CN205864143U - A kind of super high speed motor - Google Patents
A kind of super high speed motor Download PDFInfo
- Publication number
- CN205864143U CN205864143U CN201620452845.9U CN201620452845U CN205864143U CN 205864143 U CN205864143 U CN 205864143U CN 201620452845 U CN201620452845 U CN 201620452845U CN 205864143 U CN205864143 U CN 205864143U
- Authority
- CN
- China
- Prior art keywords
- decorative pattern
- slot type
- bearing
- high speed
- super high
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn - After Issue
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C17/00—Sliding-contact bearings for exclusively rotary movement
- F16C17/02—Sliding-contact bearings for exclusively rotary movement for radial load only
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D25/00—Pumping installations or systems
- F04D25/02—Units comprising pumps and their driving means
- F04D25/08—Units comprising pumps and their driving means the working fluid being air, e.g. for ventilation
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
- F02B37/04—Engines with exhaust drive and other drive of pumps, e.g. with exhaust-driven pump and mechanically-driven second pump
- F02B37/10—Engines with exhaust drive and other drive of pumps, e.g. with exhaust-driven pump and mechanically-driven second pump at least one pump being alternatively or simultaneously driven by exhaust and other drive, e.g. by pressurised fluid from a reservoir or an engine-driven pump
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C17/00—Sliding-contact bearings for exclusively rotary movement
- F16C17/04—Sliding-contact bearings for exclusively rotary movement for axial load only
- F16C17/042—Sliding-contact bearings for exclusively rotary movement for axial load only with flexible leaves to create hydrodynamic wedge, e.g. axial foil bearings
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K7/00—Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
- H02K7/18—Structural association of electric generators with mechanical driving motors, e.g. with turbines
- H02K7/1807—Rotary generators
- H02K7/1823—Rotary generators structurally associated with turbines or similar engines
- H02K7/183—Rotary generators structurally associated with turbines or similar engines wherein the turbine is a wind turbine
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
- F01D15/10—Adaptations for driving, or combinations with, electric generators
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B41/00—Engines characterised by special means for improving conversion of heat or pressure energy into mechanical power
- F02B41/02—Engines with prolonged expansion
- F02B41/10—Engines with prolonged expansion in exhaust turbines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/06—Arrangements of bearings; Lubricating
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/12—Cooling of plants
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/05—Shafts or bearings, or assemblies thereof, specially adapted for elastic fluid pumps
- F04D29/056—Bearings
- F04D29/057—Bearings hydrostatic; hydrodynamic
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/52—Casings; Connections of working fluid for axial pumps
- F04D29/522—Casings; Connections of working fluid for axial pumps especially adapted for elastic fluid pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/58—Cooling; Heating; Diminishing heat transfer
- F04D29/582—Cooling; Heating; Diminishing heat transfer specially adapted for elastic fluid pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C17/00—Sliding-contact bearings for exclusively rotary movement
- F16C17/02—Sliding-contact bearings for exclusively rotary movement for radial load only
- F16C17/026—Sliding-contact bearings for exclusively rotary movement for radial load only with helical grooves in the bearing surface to generate hydrodynamic pressure, e.g. herringbone grooves
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C17/00—Sliding-contact bearings for exclusively rotary movement
- F16C17/04—Sliding-contact bearings for exclusively rotary movement for axial load only
- F16C17/08—Sliding-contact bearings for exclusively rotary movement for axial load only for supporting the end face of a shaft or other member, e.g. footstep bearings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C17/00—Sliding-contact bearings for exclusively rotary movement
- F16C17/10—Sliding-contact bearings for exclusively rotary movement for both radial and axial load
- F16C17/102—Sliding-contact bearings for exclusively rotary movement for both radial and axial load with grooves in the bearing surface to generate hydrodynamic pressure
- F16C17/107—Sliding-contact bearings for exclusively rotary movement for both radial and axial load with grooves in the bearing surface to generate hydrodynamic pressure with at least one surface for radial load and at least one surface for axial load
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C17/00—Sliding-contact bearings for exclusively rotary movement
- F16C17/26—Systems consisting of a plurality of sliding-contact bearings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C32/00—Bearings not otherwise provided for
- F16C32/06—Bearings not otherwise provided for with moving member supported by a fluid cushion formed, at least to a large extent, otherwise than by movement of the shaft, e.g. hydrostatic air-cushion bearings
- F16C32/0603—Bearings not otherwise provided for with moving member supported by a fluid cushion formed, at least to a large extent, otherwise than by movement of the shaft, e.g. hydrostatic air-cushion bearings supported by a gas cushion, e.g. an air cushion
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/02—Parts of sliding-contact bearings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/02—Parts of sliding-contact bearings
- F16C33/04—Brasses; Bushes; Linings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/02—Parts of sliding-contact bearings
- F16C33/04—Brasses; Bushes; Linings
- F16C33/06—Sliding surface mainly made of metal
- F16C33/10—Construction relative to lubrication
- F16C33/1005—Construction relative to lubrication with gas, e.g. air, as lubricant
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C37/00—Cooling of bearings
- F16C37/002—Cooling of bearings of fluid bearings
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K5/00—Casings; Enclosures; Supports
- H02K5/04—Casings or enclosures characterised by the shape, form or construction thereof
- H02K5/16—Means for supporting bearings, e.g. insulating supports or means for fitting bearings in the bearing-shields
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K5/00—Casings; Enclosures; Supports
- H02K5/04—Casings or enclosures characterised by the shape, form or construction thereof
- H02K5/16—Means for supporting bearings, e.g. insulating supports or means for fitting bearings in the bearing-shields
- H02K5/161—Means for supporting bearings, e.g. insulating supports or means for fitting bearings in the bearing-shields radially supporting the rotary shaft at both ends of the rotor
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K5/00—Casings; Enclosures; Supports
- H02K5/04—Casings or enclosures characterised by the shape, form or construction thereof
- H02K5/16—Means for supporting bearings, e.g. insulating supports or means for fitting bearings in the bearing-shields
- H02K5/163—Means for supporting bearings, e.g. insulating supports or means for fitting bearings in the bearing-shields radially supporting the rotary shaft at only one end of the rotor
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K7/00—Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
- H02K7/18—Structural association of electric generators with mechanical driving motors, e.g. with turbines
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K9/00—Arrangements for cooling or ventilating
- H02K9/02—Arrangements for cooling or ventilating by ambient air flowing through the machine
- H02K9/04—Arrangements for cooling or ventilating by ambient air flowing through the machine having means for generating a flow of cooling medium
- H02K9/06—Arrangements for cooling or ventilating by ambient air flowing through the machine having means for generating a flow of cooling medium with fans or impellers driven by the machine shaft
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C17/00—Sliding-contact bearings for exclusively rotary movement
- F16C17/02—Sliding-contact bearings for exclusively rotary movement for radial load only
- F16C17/028—Sliding-contact bearings for exclusively rotary movement for radial load only with fixed wedges to generate hydrodynamic pressure, e.g. multi-lobe bearings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2360/00—Engines or pumps
- F16C2360/23—Gas turbine engines
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Power Engineering (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Sustainable Energy (AREA)
- Thermal Sciences (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
- Motor Or Generator Frames (AREA)
- Supercharger (AREA)
- Support Of The Bearing (AREA)
- Slot Machines And Peripheral Devices (AREA)
Abstract
The utility model discloses a kind of super high speed motor, it includes electric machine casing, rotor, stator, 2 journal bearings, 1 thrust bearing and interior axle and outer shaft, described journal bearing is slot type kinetic pressure gas journal bearing, described thrust bearing is hybrid kinetic pressure gas thrust bearing, described rotor is set in the middle part of interior axle, 2 journal bearings are respectively sleeved on the outer shaft being positioned at the left and right end of rotor, and described thrust bearing is set on the outer shaft of right-hand member and is positioned at the outer side of right-hand member journal bearing.This utility model may be implemented in the ultrahigh speed steady running under air supporting state, for equal-wattage requirement, the volume of motor can be made to be substantially reduced realization miniaturization.
Description
Technical field
This utility model relates to a kind of super high speed motor, belongs to high-accuracy field of mechanical technique.
Background technology
High-speed electric expreess locomotive typically refers to the rotating speed motor more than 10000r/min, and they have the advantage that one is owing to turning
Speed is high, so power of motor density is high, and the motor that volume is common much smaller than power, can effectively save material;Two is can
Being connected with prime mover, eliminate traditional reducing gear, transmission efficiency is high, and noise is little;Three is due to high-speed electric expreess locomotive rotary inertia
It is little, so dynamic response is fast.But along with high-speed electric expreess locomotive power grade and rotation speed requirements are improved constantly, common mechanical ball axle
Hold the use requirement that can not meet Large-power High-Speed motor.And air-bearing is little with its frictional dissipation, high-temperature stability good,
Reliability is high, it is little to vibrate, need not lubricating oil, not by series of advantages such as rotating shaft size limitation, be increasingly becoming industrial quarters
The focus paid close attention to academia, has been applied to Aeronautics and Astronautics field.
Air-bearing used by current existing high-speed electric expreess locomotive mainly has: tilting bush formula, slot type and paillon foil formula three kinds, although can
Tile style of inclining air-bearing has self-regulation performance, can in less air film interstice coverage trouble free service, to thermal deformation, elastic deformation
Etc. insensitive, and machining accuracy such as is easily guaranteed at the advantage, but its bearing bush structure is more complicated, and mounting process is complicated, from discomfort
Close industrial applications;Although paillon foil formula kinetic pressure gas journal bearing has elastic bearing, can bearing is made to obtain certain holding accordingly
Loading capability and the ability of mitigation impact shock, but owing to foil bearing is generally adopted by tinsel, not only material manufactures skill
There is also some difficult problems in art and technology, and the damping value of bearing can not large increase, cause the rigidity of bearing
Not, the critical speed of bearing is relatively low, and when running up, easy unstability is the most stuck;Although slot type kinetic pressure gas journal bearing
Having preferable stability, at high speeds, its static bearing capacity is big compared with the bearing of other form, but current slot type action pneumatic
Body journal bearing has high rigidity, and impact resistance is the best and load-carrying ability is the biggest, it is impossible to realize the height under bigger load
Speed operating.Because current air-bearing technology there is also above-mentioned variety of problems, so that existing high-speed electric expreess locomotive there is also and asks as follows
Topic: 1, rotating speed is the most limited, can only realize the rotating speed of the highest 50,000 turns at present;2, can not longtime running: produce because running up
Heat can not effectively be derived, so that stream time can not be the longest;3, the stability run up is the best, so that actual motion
Efficiency does not reaches ideal goal;4, structure is the most complicated, and volume is bigger, it is impossible to meet current miniaturization requirement.
Utility model content
The problems referred to above existed for prior art, the purpose of this utility model be to provide a kind of can the superelevation of stable operation
Speed motor.
For achieving the above object, the technical solution adopted in the utility model is as follows:
A kind of super high speed motor, including electric machine casing, rotor, stator, 2 journal bearings, 1 thrust bearing and interior axle and
Outer shaft;It is characterized in that: described journal bearing is slot type kinetic pressure gas journal bearing, including bearing outside and bearing inner sleeve;Institute
Stating thrust bearing is hybrid kinetic pressure gas thrust bearing, including two side panels and be folded in the mid-game between two side panels,
Foil-type elastic component it is equipped with between each side panel and mid-game;Described rotor is set in the middle part of interior axle, and 2 journal bearings are respectively
Being set on the outer shaft being positioned at the left and right end of rotor, described thrust bearing is set on the outer shaft of right-hand member and is positioned at right-hand member radial axle
The outer side held.
As a kind of embodiment, described super high speed motor also includes left radial axle bearing sleeve and left bearing room end cap, institute
Stating left bearing room end cap to be connected with left radial axle bearing sleeve, described left radial axle bearing sleeve is connected with electric machine casing.
As a kind of embodiment, described super high speed motor also includes right radial axle bearing sleeve, right bearing room end cap, heat radiation
Fan and blower-casting, described blower-casting is connected with right bearing room end cap, described right bearing room end cap and right journal bearing
Set is connected, and described right radial axle bearing sleeve is connected with electric machine casing, and described radiator fan is set in and is positioned at right bearing room end cap
And on the interior axle between blower-casting.
Preferably, offering some open slots in the inwall week side of electric machine casing, the end face at electric machine casing is opened
Being provided with some passages, described open slot is connected with passage, is beneficial to importing and the derivation of gas, on the one hand realizes quickly
Heat radiation aerofluxus, another side realizes bearing indoor are carried out air supply.
Preferably, some steam vents are offered in all sides of left bearing room end cap, in the outer face of blower-casting
On offer some air inlets.
Preferably, the outer circumference surface of described bearing inner sleeve and both ends of the surface are respectively provided with the slot type decorative pattern of regular shape.
As further preferred scheme, the slot type decorative pattern of the end face of described bearing inner sleeve and the slot type decorative pattern of other end
Form specular, and the radial profile of the slot type decorative pattern of the axial profile line of the slot type decorative pattern of outer circumference surface and both ends of the surface
It is respectively formed one_to_one corresponding and mutually joins.
As further preferred scheme, the axial high bit line and two in the slot type decorative pattern of the outer circumference surface of described bearing inner sleeve
The high bit line of radial direction in the slot type decorative pattern of end face is homogeneously corresponding and mutually joins before end face peripheral chamfer;The groove of outer circumference surface
Axial neutrality line in formula decorative pattern is the most corresponding with the radial direction neutrality line in the slot type decorative pattern of both ends of the surface and in end face peripheral chamfer
Front mutually handing-over;Axial low-bit line in the slot type decorative pattern of outer circumference surface is equal with the radial direction low-bit line in the slot type decorative pattern of both ends of the surface
Corresponding and mutually join before end face peripheral chamfer.
Preferably, the fit clearance between described bearing inner sleeve and bearing outside is 0.003~0.008mm.
Preferably, the two ends at described bearing outside are provided with stop ring.
Preferably, the both ends of the surface of described mid-game are equipped with the slot type decorative pattern of regular shape, and the slot type of end face
Decorative pattern forms specular with the slot type decorative pattern of other end.
Preferably, the outer circumference surface in described mid-game also is provided with slot type decorative pattern, and the slot type decorative pattern of outer circumference surface
Shape identical with the shape of the slot type decorative pattern of both ends of the surface, and the axial profile line of the slot type decorative pattern of outer circumference surface and both ends of the surface
The radial profile of slot type decorative pattern be respectively formed one_to_one corresponding and mutually join.
Groove as further preferred scheme, the axial high bit line in the slot type decorative pattern of the outer circumference surface of mid-game and both ends of the surface
The high bit line of radial direction in formula decorative pattern is homogeneously corresponding and mutually joins before end face peripheral chamfer;In the slot type decorative pattern of outer circumference surface
Axial neutrality line the most corresponding with the radial direction neutrality line in the slot type decorative pattern of both ends of the surface and mutually hand over before end face peripheral chamfer
Connect;Axial low-bit line in the slot type decorative pattern of outer circumference surface is the most corresponding with the radial direction low-bit line in the slot type decorative pattern of both ends of the surface,
And mutually join before end face peripheral chamfer.
As further preferred scheme, the cooperation face of the foil-type elastic component matched with mid-game is provided with wear-resistant coating.
As further preferred scheme, described foil-type elastic component is 0.003~0.008mm with the fit clearance of mid-game.
As further preferred scheme, at least one end of described foil-type elastic component is fixed on the inner face of corresponding side panel.
As further preferred scheme, the foil-type elastic component on each side panel is multiple, and uniform along the inner face of side panel
Distribution.
As further preferred scheme, the foil-type elastic component being fixed on a side panel be fixed on another side panel
Foil-type elastic component forms specular.
As further preferred scheme, the inner face at side panel is provided with the draw-in groove for fixing foil-type elastic component.
As a kind of embodiment, described foil-type elastic component is made up of ripple paper tinsel peace paper tinsel, the arc convex of described ripple paper tinsel
Top fits with flat paper tinsel.
As another embodiment, described foil-type elastic component is made up of ripple paper tinsel peace paper tinsel, between the ripple arch of described ripple paper tinsel
Transition base fits with flat paper tinsel.
As another embodiment, described foil-type elastic component is made up of two flat paper tinsels.
Above-mentioned slot type decorative pattern is impeller shape.
Above-mentioned foil-type elastic component is preferably through Surface heat-treatent.
Preferably, described rotor includes rotor base, magnet steel and magnet steel protection set, and described rotor base is set in
On interior axle, described magnetic steel sleeve is located at the central part of rotor base, and described magnet steel protection set is set on magnet steel.
Preferably, described stator includes that iron core and winding, described iron core are held within the motor above rotor
On the inwall of housing, described winding is arranged on iron core.
Preferably, described iron core includes by some punchings stacked stator lasmination formed up and down and is fixed on stator
The end clamp plate of lamination both sides.
As further preferred scheme, described punching is annular, is interval with the perforation of multiple cup-shaped at ring part, described
The rim of a cup portion of perforation closes, the bottom opening of cup foot.
Preferably, described winding is the star-like connection of three-phase, and centrage is not brought up, and only draws tri-terminations of A, B, C.
As further preferred scheme, every phase winding is 2 coils, and each coil is formed by enamel covered wire continuous coiling.
Compared with prior art, this utility model has the advantages that
Because of motor provided by the utility model, be the lubricant using gas as bearing, the most not only have pollution-free,
Friction loss is low, use the plurality of advantages such as time length, applied widely, energy-conserving and environment-protective, and uses described structure, radiating effect
Good, it is ensured that long-time steady operation;Especially, the ultrahigh speed under air supporting state can be realized because of the air bearing of described structure
Steady running (after tested, up to 100,000~450, the limit speed of 000rpm), therefore for equal-wattage requirement, this reality
It is substantially reduced realization miniaturization with the novel volume making motor, there is the advantage such as little, easy to use that takes up room, micro-to promoting
The development of type new and high technology has important value, has significance progress relative to prior art.
Accompanying drawing explanation
Fig. 1 is the cross-sectional view of a kind of super high speed motor that embodiment 1 provides;
Fig. 2 is the left view perspective view of the local segmentation of the slot type kinetic pressure gas journal bearing that embodiment 1 provides;
Fig. 3 is the A partial enlarged drawing in Fig. 2;
Fig. 4 is that the right side of the local segmentation of the slot type kinetic pressure gas journal bearing that embodiment 1 provides regards perspective view;
Fig. 5 is the B partial enlarged drawing in Fig. 4;
Fig. 6 is the cross-sectional view of the hybrid kinetic pressure gas thrust bearing that embodiment 1 provides;
Fig. 7 a is the left view of mid-game described in embodiment 1;
Fig. 7 b is the right view of mid-game described in embodiment 1;
Fig. 8 a is the right view of the left hand plate being fixed with foil-type elastic component described in embodiment 1;
Fig. 8 b is the left view of the right side dish being fixed with foil-type elastic component described in embodiment 1;
Fig. 9 is the cross section structure schematic diagram of the foil-type elastic component that embodiment 1 provides;
Figure 10 is the perspective view of the foil-type elastic component that embodiment 1 provides;
Figure 11 a is the left view perspective view of a kind of hybrid kinetic pressure gas thrust bearing that embodiment 2 provides;
Figure 11 b is that the right side of the hybrid kinetic pressure gas thrust bearing that embodiment 2 provides regards perspective view;
Figure 12 is the local segmentation perspective view of the hybrid kinetic pressure gas thrust bearing that embodiment 2 provides;
Figure 13 is the left view perspective view of mid-game described in embodiment 2;
Figure 14 is the C partial enlarged drawing in Figure 13;
Figure 15 is that the right side of mid-game described in embodiment 2 regards perspective view;
Figure 16 is the D partial enlarged drawing in Figure 15;
Figure 17 is the rotor structure schematic diagram that embodiment 3 is provided;
Figure 18 is the core structure schematic diagram that embodiment 4 is provided;
Figure 19 is the structural representation of punching described in embodiment 4;
Figure 20 is the winding construction schematic diagram that embodiment 4 is provided;
Figure 21 is the perspective view of the electric machine casing that embodiment 5 is provided;
Figure 22 is the E partial enlarged drawing in Figure 21;
Figure 23 is that the right side of a kind of super high speed motor that embodiment 5 provides regards perspective view.
In figure, label is schematically as follows:
1, electric machine casing;11, open slot;12, passage;2, rotor;21, rotor base;22, magnet steel;23, magnet steel protection
Set;3, stator;31, iron core;311, punching;3111, cup-shaped perforation;3111a, rim of a cup portion;3111b, cup foot;312, stator stack
Sheet;313, end clamp plate;32, winding;4, slot type kinetic pressure gas journal bearing;4a, left end journal bearing;4b, right-hand member journal bearing;
41, bearing outside;42, bearing inner sleeve;43, slot type decorative pattern;431, the slot type decorative pattern of outer circumference surface;4311, axial high bit line;
4312, axial neutrality line;4313, axial low-bit line;432, the slot type decorative pattern of left side;4321, the highest bit line;4322, footpath
To neutrality line;4323, radially low-bit line;433, the slot type decorative pattern of right side;4331, the highest bit line;4332, position in radial direction
Line;4333, radially low-bit line;44, stop ring;5, hybrid kinetic pressure gas thrust bearing;51, side panel;511, left hand plate;512, right
Side panel;513, draw-in groove;52, mid-game;521, the slot type decorative pattern of left side;5211, the highest bit line;5212, radially neutrality line;
5213, radially low-bit line;522, the slot type decorative pattern of right side;5221, the highest bit line;5222, radially neutrality line;5223, footpath
To low-bit line;523, the slot type decorative pattern of outer circumference surface;5231, axial high bit line;5232, axial neutrality line;5233, axial low level
Line;53, foil-type elastic component;53a, the foil-type elastic component being fixed in left hand plate;53b, the foil-type being fixed on the dish of right side are elastic
Part;531, ripple paper tinsel;5311, arc convex;5312, transition base between ripple arch;532, flat paper tinsel;6, interior axle;7, outer shaft;8a, Zuo Jing
To bearing holder (housing, cover);8b, right radial axle bearing sleeve;9a, left bearing room end cap;9a1, steam vent;9b, right bearing room end cap;10, radiation air
Fan;101, blower-casting;102, air inlet.
Detailed description of the invention
Below in conjunction with the accompanying drawings and the technical solution of the utility model is described in detail by embodiment.
Embodiment 1
As shown in Figure 1: a kind of super high speed motor that the present embodiment provides, including electric machine casing 1, rotor 2, stator 3,2
4,1 thrust bearing 5 of journal bearing and interior axle 6 and outer shaft 7;Described journal bearing 4 is slot type kinetic pressure gas journal bearing, bag
Include bearing outside 41 and bearing inner sleeve 42;Described thrust bearing 5 is hybrid kinetic pressure gas thrust bearing, including two side panels 51
And the mid-game 52 being folded between two side panels, between each side panel 51 and mid-game 52, it is equipped with foil-type elastic component 53;Institute
Stating rotor 2 and be set in the middle part of interior axle 6,2 journal bearings 4 are respectively sleeved on the outer shaft 7 being positioned at the left and right end of rotor 2, described
Thrust bearing 5 is set on the outer shaft 7 of right-hand member and is positioned at the outer side of right-hand member journal bearing 4b.
Described super high speed motor also includes left radial axle bearing sleeve 8a, left bearing room end cap 9a, right radial axle bearing sleeve 8b, the right side
Bearing chamber end cap 9b, radiator fan 10 and blower-casting 101, described left bearing room end cap 9a is connected with left radial axle bearing sleeve 8a
Connecing, described left radial axle bearing sleeve 8a is connected with electric machine casing 1, and described blower-casting 101 is connected with right bearing room end cap 9b,
Described right bearing room end cap 9b is connected with right radial axle bearing sleeve 8b, and described right radial axle bearing sleeve 8b is connected with electric machine casing 1,
Described radiator fan 10 is set on the interior axle 6 between right bearing room end cap 9b and blower-casting 101.
In conjunction with shown in Fig. 2 to Fig. 5: outer circumference surface and the left and right end face of described bearing inner sleeve 42 are respectively provided with regular shape
Slot type decorative pattern 43 (such as 431 in figure, 432 and 433, the slot type decorative pattern in the present embodiment is impeller shape), and left side
Slot type decorative pattern 432 forms specular with the slot type decorative pattern 433 of right side.It is positioned at the slot type flower of the outer circumference surface of bearing inner sleeve 42
The axial profile line of stricture of vagina 431 is respectively formed one_to_one corresponding also with the radial profile of the slot type decorative pattern (432 and 433) of left and right end face
Mutually handing-over, it may be assumed that the axial high bit line 4311 in the slot type decorative pattern 431 of outer circumference surface and the slot type decorative pattern (432 of left and right end face
With 433) in the high bit line of radial direction (4321 and 4331) the most corresponding and mutually join before end face peripheral chamfer;Outer circumference surface
Slot type decorative pattern 431 in axial neutrality line 4312 and the radial direction neutrality line in the slot type decorative pattern (432 and 433) of left and right end face
(4322 and 4332) are the most corresponding and mutually join before end face peripheral chamfer;Axial in the slot type decorative pattern 431 of outer circumference surface
Low-bit line 4313 is the most corresponding with the radial direction low-bit line (4323 and 4333) in the slot type decorative pattern of left and right end face (432 and 433),
And mutually join before end face peripheral chamfer.
Slot type decorative pattern (431,432 and of regular shape it are respectively provided with by the outer circumference surface and both ends of the surface making bearing inner sleeve 42
433), the slot type decorative pattern 432 of left side and the slot type decorative pattern 433 of right side form the slot type decorative pattern of specular and outer circumference surface
The axial profile line of 431 is respectively formed one_to_one corresponding phase with the radial profile of the slot type decorative pattern (432 and 433) of left and right end face
Handing-over mutually, it is ensured that produced by the slot type decorative pattern (432 and 433) of the impeller shape of both ends of the surface, pressurization gas is from axle center radially
Carrying in the recess channels constantly formed toward the slot type decorative pattern 431 of outer circumference surface, running up axle so that forming higher support
Hold required air film, and air film is i.e. as the lubricant of kinetic pressure gas journal bearing, is thus advantageous to realize described slot type dynamic pressure
The gas lubricated journal bearing 4 high speed steady running under air supporting state.
It addition, when being respectively provided with stop ring 44 at the two ends of bearing outside 41, may be implemented under the drive of high speed gyroaxis,
Making to be produced from sealing function between the both ends of the surface of bearing inner sleeve 42 and stop ring 44, the action pneumatic physical ability making slot type decorative pattern continuously generate is complete
Well in the airtight whole fit clearance being saved in bearing, fully ensure that the lubrication of the kinetic pressure gas journal bearing run up needs
Want.
Fit clearance between described bearing outside 41 and bearing inner sleeve 42 is preferably 0.003~0.008mm, with the most really
Protect the reliability and stability that bearing runs up.
As shown in Figure 6: the hybrid kinetic pressure gas thrust bearing of one 5 that the present embodiment provides, including: two side panels 51,
Between two side panels 51, it is folded with mid-game 52, between each side panel 51 and mid-game 52, is provided with foil-type elastic component 53;In described
The left side of dish 52 is provided with the slot type decorative pattern 521 of regular shape, and right side is provided with the slot type decorative pattern 522 of regular shape.
Visible in conjunction with Fig. 7 a and Fig. 7 b: the slot type decorative pattern 521 of the left side of described mid-game 52 and the slot type decorative pattern of right side
The footpath of specular, the radial profile of the slot type decorative pattern 521 of left side and the slot type decorative pattern 522 of right side is formed between 522
One_to_one corresponding is formed to contour line.
Described slot type decorative pattern 521 is identical with the shape of 522, is impeller shape in the present embodiment.
Visible further combined with Fig. 8 a and Fig. 8 b: described foil-type elastic component 53 is fixed on the inner face of corresponding side panel 51
(shown in the left hand plate 511 and Fig. 8 b being fixed with foil-type elastic component 53a shown in such as Fig. 8 a, it is fixed with foil-type elastic component 53b
Right side dish 512), and the foil-type elastic component 53a being fixed in left hand plate 511 and the foil-type being fixed on the dish 512 of right side elastic
Part 53b forms specular.Foil-type elastic component on each side panel can be multiple (shown in figure are 4), and along side panel
Inner face be uniformly distributed.
By arranging foil-type elastic component 53 between side panel 51 and mid-game 52, the left and right end face in mid-game 52 arranges rule
The slot type decorative pattern (521 and 522) of shape, and make the slot type decorative pattern 521 of left side form mirror image with the slot type decorative pattern 522 of right side
Symmetry, thus obtained the rigidity characteristic of the high limit rotating speed not only with slot type kinetic pressure gas thrust bearing, but also there is paillon foil formula
The high impact-resistance of kinetic pressure gas thrust bearing and the hybrid kinetic pressure gas thrust bearing of the flexible characteristic of load-carrying ability;Cause
For defining wedge shape space between foil-type elastic component 53 and mid-game 52, when mid-game 52 rotates, gas is because of the viscous effect of himself
It is driven and is compressed in wedge shape space, thus axial hydrodynamic power can be made to been significantly enhanced, relative to existing simple paper tinsel
Chip kinetic pressure gas thrust bearing, can have the limit speed being multiplied under same load;Simultaneously as add foil-type
Elastic component 53, under its elastic reaction, the ability that also can make the load-carrying ability of bearing, impact resistance and suppression axle whirling motion is notable
Improve, relative to existing simple slot type kinetic pressure gas thrust bearing, can have the shock resistance being multiplied under same rotational speed
Ability and load-carrying ability.
Shown in Fig. 6 and Fig. 9, Figure 10: described foil-type elastic component 53 is made up of ripple paper tinsel 531 peace paper tinsel 532, described ripple
The top of the arc convex 5311 of paper tinsel 531 fits with flat paper tinsel 532, and between the ripple arch of described ripple paper tinsel 531, transition base 5312 is with right
The inner face answering side panel 51 fits.
For reducing the mid-game 52 the run up abrasion to foil-type elastic component 53 further, to extend the use longevity of bearing
Life, preferably arranges wear-resistant coating (not shown) on the cooperation face of the foil-type elastic component 53 matched with mid-game 52.
Embodiment 2
In conjunction with Figure 11 a, 11b, shown in 12 to 16 visible, the hybrid kinetic pressure gas thrust bearing of one that the present embodiment provides
With differing only in of embodiment 1:
Outer circumference surface in described mid-game 52 also is provided with slot type decorative pattern 523, and the shape of the slot type decorative pattern 523 of outer circumference surface
Identical with the shape of the slot type decorative pattern of left and right end face (521 and 522) (in the present embodiment, being impeller shape), and excircle
The axial profile line of the slot type decorative pattern 523 in face is respectively formed with the radial profile of the slot type decorative pattern (521 and 522) of left and right end face
One_to_one corresponding also mutually joins;That is:
Axial high bit line 5231 in the slot type decorative pattern 523 of outer circumference surface and the radial direction in the slot type decorative pattern 521 of left side
High bit line 5211 is the most corresponding and mutually joins before end face peripheral chamfer;In axial direction in the slot type decorative pattern 523 of outer circumference surface
Bit line 5232 the most corresponding with the radial direction neutrality line 5212 in the slot type decorative pattern 521 of left side and before end face peripheral chamfer phase
Handing-over mutually;Axial low-bit line 5233 in the slot type decorative pattern 523 of outer circumference surface is low with the radial direction in the slot type decorative pattern 521 of left side
Bit line 5213 is the most corresponding and mutually joins (as shown in figure 14) before end face peripheral chamfer;
Axial high bit line 5231 in the slot type decorative pattern 523 of outer circumference surface and the radial direction in the slot type decorative pattern 522 of right side
High bit line 5221 is the most corresponding and mutually joins before end face peripheral chamfer;In axial direction in the slot type decorative pattern 523 of outer circumference surface
Bit line 5232 the most corresponding with the radial direction neutrality line 5222 in the slot type decorative pattern 522 of right side and before end face peripheral chamfer phase
Handing-over mutually;Axial low-bit line 5233 in the slot type decorative pattern 523 of outer circumference surface is low with the radial direction in the slot type decorative pattern 522 of right side
Bit line 5223 is the most corresponding and mutually joins (as shown in figure 16) before end face peripheral chamfer.
When the outer circumference surface in described mid-game 52 also is provided with slot type decorative pattern, and make the shape of the slot type decorative pattern 523 of outer circumference surface
Shape is identical with the shape of the slot type decorative pattern of left and right end face (521 and 522), and the axial wheel of the slot type decorative pattern 523 of outer circumference surface
When the radial profile of the slot type decorative pattern (521 and 522) of profile and left and right end face is respectively formed one_to_one corresponding and mutually joins, can
Make pressurization gas produced by the slot type decorative pattern (521 and 522) of inner disc both ends of the surface from axle center the most constantly toward outer circumference surface
The recess channels that formed of slot type decorative pattern 523 in carry run up the air film needed for bearing so that forming higher support, and gas
Film is i.e. as the lubricant of kinetic pressure gas thrust bearing, thus can be further assured that described hybrid kinetic pressure gas thrust bearing
High speed steady running under air supporting state, is further ensured that for realizing the high limit rotating speed offer of motor.
The inner face of side panel 51 is provided with the draw-in groove 513 (as shown in figure 12) for fixing foil-type elastic component 53.
Described foil-type elastic component 53 is preferably 0.003~0.008mm, to further ensure that with the fit clearance of mid-game 52
The reliability and stability that bearing runs up.
In order to preferably meet the performance requirement that runs up, described foil-type elastic component 53 preferably through surface heat at
Reason.
It is further to note that: the composition structure of foil-type elastic component 53 described in the utility model is not limited to above-mentioned enforcement
Described in example, it is also possible to use ripple paper tinsel peace paper tinsel composition, but between the ripple of described ripple paper tinsel arch, transition base fits with flat paper tinsel, or
Person, directly uses two flat paper tinsel compositions, or uses other existing structure.
Embodiment 3
Shown in Fig. 1 and Figure 17: described rotor 2 include rotor base 21, magnet steel 22 and magnet steel protection set 23, described turn
Sub-base 21 is set on interior axle 6, and described magnet steel 22 is set in the central part of rotor base 21, and described magnet steel protection set 23 is sheathed
On magnet steel 22, more preferably to meet ultrahigh speed rotation.
Embodiment 4
Shown in Fig. 1 and Figure 18: described stator 3 includes that iron core 31 and winding 32, described iron core 31 are held within turning
On the inwall of the electric machine casing 1 above son 2, described winding 32 is arranged on iron core 31;Described iron core 31 includes by some punchings
About the 311 stacked stator lasmination 312 formed and the end clamp plates 313 being fixed on stator lasmination 312 both sides.
As shown in figure 19: described punching 311, in annular, is interval with multiple cup-shaped perforation 3111 at ring part, described
The rim of a cup portion 3111a of perforation 3111 closes, the bottom opening of cup foot 3111b.
As shown in figure 20: described winding 32 uses the star-like connection of three-phase, and centrage is not brought up, A, B, C tri-end is only drawn
Head;Every phase winding is 2 coils, and each coil is formed by enamel covered wire continuous coiling.
Embodiment 5
Shown in Figure 21 and Figure 22: offer some open slots 11, at electric machine casing in the inwall week side of electric machine casing 1
The end face of 1 offers some passages 12, and described open slot 11 is connected with passage 12, is beneficial to the importing of gas and leads
Going out, on the one hand realize quick heat radiating aerofluxus, another side realizes bearing indoor are carried out air supply.
It addition, offer some steam vent 9a1 in all sides of left bearing room end cap 9a, in the outer face of blower-casting 101
On offer some air inlets 102 (as shown in figure 23), to realize quick heat radiating further.
After tested, the bearing that this utility model provides can reach 100,000~450 under air supporting state, the pole of 000rpm
Limit rotating speed, therefore for equal-wattage requirement, this utility model can make the volume of motor be substantially reduced realization miniaturization, to promotion
The development of miniaturization new and high technology has important value.
Finally be necessary it is pointed out here that: above content is served only for doing technical scheme described in the utility model further
Describe in detail, it is impossible to being interpreted as the restriction to this utility model protection domain, those skilled in the art is according to this utility model
Some nonessential improvement of making of foregoing and adjustment belong to protection domain of the present utility model.
Claims (22)
1. a super high speed motor, including electric machine casing, rotor, stator, 2 journal bearings, 1 thrust bearing and interior axle and outer
Axle;It is characterized in that: described journal bearing is slot type kinetic pressure gas journal bearing, including bearing outside and bearing inner sleeve;Described
Thrust bearing is hybrid kinetic pressure gas thrust bearing, including two side panels and be folded in the mid-game between two side panels,
Foil-type elastic component it is equipped with between each side panel and mid-game;Described rotor is set in the middle part of interior axle, and 2 journal bearings overlap respectively
Being provided on the outer shaft of the left and right end of rotor, described thrust bearing is set on the outer shaft of right-hand member and is positioned at right-hand member journal bearing
Outer side.
Super high speed motor the most according to claim 1, it is characterised in that: described super high speed motor also includes left radial axle
Bearing sleeve and left bearing room end cap, described left bearing room end cap is connected with left radial axle bearing sleeve, described left radial axle bearing sleeve and electricity
Casing body is connected.
Super high speed motor the most according to claim 1 and 2, it is characterised in that: described super high speed motor also includes right footpath
To bearing holder (housing, cover), right bearing room end cap, radiator fan and blower-casting, described blower-casting is connected with right bearing room end cap, institute
Stating right bearing room end cap to be connected with right radial axle bearing sleeve, described right radial axle bearing sleeve is connected with electric machine casing, described heat radiation
Fan is set on the interior axle between right bearing room end cap and blower-casting.
Super high speed motor the most according to claim 3, it is characterised in that: offer some in all sides of left bearing room end cap
Steam vent, offers some air inlets on the outer face of blower-casting.
Super high speed motor the most according to claim 1, it is characterised in that: offer some in the inwall week side of electric machine casing
Open slot, the end face at electric machine casing offers some passages, and described open slot is connected with passage.
Super high speed motor the most according to claim 1, it is characterised in that: offer some in the inwall week side of electric machine casing
Open slot, the end face at electric machine casing offers some passages, and described open slot is connected with passage.
Super high speed motor the most according to claim 1, it is characterised in that: the outer circumference surface of described bearing inner sleeve and both ends of the surface
It is respectively provided with the slot type decorative pattern of regular shape.
Super high speed motor the most according to claim 7, it is characterised in that: the slot type decorative pattern of the end face of described bearing inner sleeve
Specular is formed with the slot type decorative pattern of other end, and the axial profile line of the slot type decorative pattern of outer circumference surface and both ends of the surface
The radial profile of slot type decorative pattern is respectively formed one_to_one corresponding and mutually joins.
Super high speed motor the most according to claim 8, it is characterised in that: the slot type flower of the outer circumference surface of described bearing inner sleeve
Axial high bit line bit line high with the radial direction in the slot type decorative pattern of both ends of the surface in stricture of vagina the most corresponding and before end face peripheral chamfer phase
Handing-over mutually;Axial neutrality line in the slot type decorative pattern of outer circumference surface is the most relative with the radial direction neutrality line in the slot type decorative pattern of both ends of the surface
Should and mutually join before end face peripheral chamfer;Axial low-bit line in the slot type decorative pattern of outer circumference surface and the slot type of both ends of the surface
Radial direction low-bit line in decorative pattern is the most corresponding and mutually joins before end face peripheral chamfer.
Super high speed motor the most according to claim 1, it is characterised in that: the both ends of the surface of described mid-game are equipped with rule shape
The slot type decorative pattern of shape, and the slot type decorative pattern formation specular of the slot type decorative pattern of end face and other end.
11. super high speed motors according to claim 10, it is characterised in that: the outer circumference surface in described mid-game also is provided with groove
Formula decorative pattern, and the shape of the slot type decorative pattern of outer circumference surface is identical with the shape of the slot type decorative pattern of both ends of the surface, and outer circumference surface
The axial profile line of slot type decorative pattern is respectively formed one_to_one corresponding with the radial profile of the slot type decorative pattern of both ends of the surface and mutually joins.
12. super high speed motors according to claim 11, it is characterised in that: in the slot type decorative pattern of the outer circumference surface of mid-game
Axial high bit line bit line high with the radial direction in the slot type decorative pattern of both ends of the surface is the most corresponding and mutually hands over before end face peripheral chamfer
Connect;Axial neutrality line in the slot type decorative pattern of outer circumference surface is the most corresponding with the radial direction neutrality line in the slot type decorative pattern of both ends of the surface,
And mutually join before end face peripheral chamfer;Axial low-bit line in the slot type decorative pattern of outer circumference surface and the slot type decorative pattern of both ends of the surface
In radial direction low-bit line the most corresponding and mutually join before end face peripheral chamfer.
13. super high speed motors according to claim 1, it is characterised in that: the foil-type elastic component being fixed on a side panel
Specular is formed with the foil-type elastic component being fixed on another side panel.
14. according to the super high speed motor described in claim 1 or 13, it is characterised in that: described foil-type elastic component by ripple paper tinsel and
Flat paper tinsel forms, and the arc convex top of described ripple paper tinsel fits with flat paper tinsel.
15. according to the super high speed motor described in claim 1 or 13, it is characterised in that: described foil-type elastic component by ripple paper tinsel and
Flat paper tinsel forms, and between the ripple arch of described ripple paper tinsel, transition base fits with flat paper tinsel.
16. according to the super high speed motor described in claim 1 or 13, it is characterised in that: described foil-type elastic component is put down by two
Paper tinsel forms.
17. super high speed motors according to claim 1, it is characterised in that: described rotor includes rotor base, magnet steel and magnetic
Steel protection set, described rotor base is set on interior axle, and described magnetic steel sleeve is located at the central part of rotor base, and described magnet steel is protected
It is set on magnet steel.
18. super high speed motors according to claim 1, it is characterised in that: described stator includes iron core and winding, described ferrum
Core is held within the inwall of the electric machine casing above rotor, and described winding is arranged on iron core.
19. super high speed motors according to claim 18, it is characterised in that: described iron core includes being folded up and down by some punchings
Put the stator lasmination of formation and be fixed on the end clamp plate of stator lasmination both sides.
20. super high speed motors according to claim 19, it is characterised in that: described punching is annular, between ring part
Every being provided with the perforation of multiple cup-shaped, the rim of a cup portion of described perforation closes, the bottom opening of cup foot.
21. super high speed motors according to claim 18, it is characterised in that: described winding is the star-like connection of three-phase, center
Line is not brought up, and only draws tri-terminations of A, B, C.
22. super high speed motors according to claim 21, it is characterised in that: every phase winding is 2 coils, each coil by
Enamel covered wire continuous coiling forms.
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CNPCT/CN2015/079234 | 2015-05-19 | ||
CNPCT/CN2015/079233 | 2015-05-19 | ||
PCT/CN2015/079234 WO2016183788A1 (en) | 2015-05-19 | 2015-05-19 | Mixed-type dynamic pressure gas thrust bearing |
PCT/CN2015/079233 WO2016183787A1 (en) | 2015-05-19 | 2015-05-19 | Groove-type dynamic pressure gas radial bearing |
Publications (1)
Publication Number | Publication Date |
---|---|
CN205864143U true CN205864143U (en) | 2017-01-04 |
Family
ID=56716270
Family Applications (14)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201610334013.1A Active CN105889314B (en) | 2015-05-19 | 2016-05-18 | A kind of highway turbine booster |
CN201610327779.7A Active CN106026517B (en) | 2015-05-19 | 2016-05-18 | A kind of highway turbine generator |
CN201610329210.4A Active CN106026492B (en) | 2015-05-19 | 2016-05-18 | A kind of super high speed motor |
CN201610327807.5A Active CN105889097B (en) | 2015-05-19 | 2016-05-18 | A kind of ultrahigh speed air blower |
CN201620452770.4U Withdrawn - After Issue CN205858479U (en) | 2015-05-19 | 2016-05-18 | A kind of super high speed electric power generating turbine pressurizer |
CN201620452740.3U Active CN205858947U (en) | 2015-05-19 | 2016-05-18 | A kind of ultrahigh speed gas turbine generator |
CN201610329288.6A Active CN105889313B (en) | 2015-05-19 | 2016-05-18 | A kind of ultrahigh speed gas turbine generator |
CN201620457923.4U Active CN205858948U (en) | 2015-05-19 | 2016-05-18 | A kind of highway turbine supercharger |
CN201620450047.2U Active CN205858730U (en) | 2015-05-19 | 2016-05-18 | A kind of ultrahigh speed aerator |
CN201610327762.1A Active CN105888818B (en) | 2015-05-19 | 2016-05-18 | A kind of super high speed electric power generating turbine supercharging device |
CN201620452845.9U Withdrawn - After Issue CN205864143U (en) | 2015-05-19 | 2016-05-18 | A kind of super high speed motor |
CN201620454708.9U Withdrawn - After Issue CN205858494U (en) | 2015-05-19 | 2016-05-18 | A kind of ultrahigh speed turbojet engine |
CN201610329302.2A Active CN106014641B (en) | 2015-05-19 | 2016-05-18 | A kind of ultrahigh speed turbojet engine |
CN201620450029.4U Withdrawn - After Issue CN205864174U (en) | 2015-05-19 | 2016-05-18 | A kind of highway turbine electromotor |
Family Applications Before (10)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201610334013.1A Active CN105889314B (en) | 2015-05-19 | 2016-05-18 | A kind of highway turbine booster |
CN201610327779.7A Active CN106026517B (en) | 2015-05-19 | 2016-05-18 | A kind of highway turbine generator |
CN201610329210.4A Active CN106026492B (en) | 2015-05-19 | 2016-05-18 | A kind of super high speed motor |
CN201610327807.5A Active CN105889097B (en) | 2015-05-19 | 2016-05-18 | A kind of ultrahigh speed air blower |
CN201620452770.4U Withdrawn - After Issue CN205858479U (en) | 2015-05-19 | 2016-05-18 | A kind of super high speed electric power generating turbine pressurizer |
CN201620452740.3U Active CN205858947U (en) | 2015-05-19 | 2016-05-18 | A kind of ultrahigh speed gas turbine generator |
CN201610329288.6A Active CN105889313B (en) | 2015-05-19 | 2016-05-18 | A kind of ultrahigh speed gas turbine generator |
CN201620457923.4U Active CN205858948U (en) | 2015-05-19 | 2016-05-18 | A kind of highway turbine supercharger |
CN201620450047.2U Active CN205858730U (en) | 2015-05-19 | 2016-05-18 | A kind of ultrahigh speed aerator |
CN201610327762.1A Active CN105888818B (en) | 2015-05-19 | 2016-05-18 | A kind of super high speed electric power generating turbine supercharging device |
Family Applications After (3)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201620454708.9U Withdrawn - After Issue CN205858494U (en) | 2015-05-19 | 2016-05-18 | A kind of ultrahigh speed turbojet engine |
CN201610329302.2A Active CN106014641B (en) | 2015-05-19 | 2016-05-18 | A kind of ultrahigh speed turbojet engine |
CN201620450029.4U Withdrawn - After Issue CN205864174U (en) | 2015-05-19 | 2016-05-18 | A kind of highway turbine electromotor |
Country Status (3)
Country | Link |
---|---|
CN (14) | CN105889314B (en) |
TW (2) | TWI704751B (en) |
WO (7) | WO2016184414A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106026492A (en) * | 2015-05-19 | 2016-10-12 | 罗立峰 | Ultra-high-speed motor |
Families Citing this family (38)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106285918B (en) * | 2016-10-13 | 2019-04-02 | 福州大学 | Bi-motor turbocharging power generation device and its control method |
CN108005727B (en) * | 2016-10-27 | 2019-12-20 | 北京精密机电控制设备研究所 | Ultrahigh-speed turbine applicable to high-temperature high-back-pressure dry gas sealing structure |
CN106368804B (en) * | 2016-11-04 | 2019-02-15 | 广州汽车集团股份有限公司 | Engine booster method and system |
CN106451894A (en) * | 2016-12-05 | 2017-02-22 | 中国工程物理研究院机械制造工艺研究所 | High-speed permanent magnet motor using aerodynamic pressure foil bearings for supporting |
CN106369056B (en) * | 2016-12-05 | 2019-06-21 | 中国工程物理研究院机械制造工艺研究所 | Turbocharger |
CN108868893B (en) * | 2018-01-12 | 2024-04-02 | 刘慕华 | Rotor system and control method thereof, gas turbine generator set and control method thereof |
CN108868891B (en) * | 2018-01-12 | 2024-04-02 | 刘慕华 | Rotor system and control method thereof, gas turbine generator set and control method thereof |
CN108868890A (en) * | 2018-01-12 | 2018-11-23 | 至玥腾风科技投资集团有限公司 | A kind of tesla's turbine and control method |
CN108868911B (en) * | 2018-01-12 | 2024-03-19 | 刘慕华 | Power generation system and control method thereof |
CN108952967B (en) * | 2018-06-27 | 2020-04-03 | 中国科学院工程热物理研究所 | Turbojet engine with improved air system |
CN109193990B (en) * | 2018-10-21 | 2024-06-25 | 刘慕华 | Motor and assembly method thereof |
CN109113916A (en) * | 2018-10-24 | 2019-01-01 | 汪平 | A kind of no ponding whirling motion whirlpool leaf hydroelectric generation component |
CN109660057B (en) * | 2018-12-22 | 2024-07-12 | 拓浦柯(中国)有限公司 | Unidirectional rotation permanent magnet high-speed motor and bidirectional air bearing thereof |
CN111365285A (en) * | 2018-12-25 | 2020-07-03 | 珠海格力电器股份有限公司 | Compressors, refrigerant circulation systems and refrigeration equipment |
CN111365290A (en) * | 2018-12-25 | 2020-07-03 | 珠海格力电器股份有限公司 | Shaft seal components, compressors and refrigerant circulation systems |
CN109742898B (en) * | 2018-12-28 | 2020-11-03 | 西安航天泵业有限公司 | Integrated totally-enclosed low-temperature hydraulic power generation device |
CN109751254B (en) * | 2019-01-30 | 2021-06-25 | 青岛科技大学 | A vertical miniature air suspension centrifugal compressor |
CN109707638B (en) * | 2019-01-30 | 2021-06-25 | 青岛科技大学 | A small and micro centrifugal compressor with integrated bearing and seal |
KR20200140504A (en) * | 2019-06-07 | 2020-12-16 | 가부시키가이샤 미쯔이 이앤에스 머시너리 | Turbo charger excess power recovery device for internal combustion engine, and ship |
CN110439847B (en) * | 2019-08-30 | 2022-01-11 | 广州市昊志机电股份有限公司 | Centrifugal compressor shafting structure and centrifugal compressor |
CN110939513A (en) * | 2019-12-25 | 2020-03-31 | 至玥腾风科技集团有限公司 | A kind of rotor system and micro gas turbine |
CN111075563A (en) * | 2019-12-27 | 2020-04-28 | 至玥腾风科技集团有限公司 | Cold, heat and electricity triple supply micro gas turbine equipment |
CN111535884B (en) * | 2020-04-29 | 2022-07-08 | 北京动力机械研究所 | High-efficient expansion device of inert mixed gas bearing |
CN111987841A (en) * | 2020-09-02 | 2020-11-24 | 西北工业大学 | External lubrication self-current-limiting brushless starter generator for micro turbojet engine |
CN112636510B (en) * | 2020-11-09 | 2022-08-19 | 珠海格力电器股份有限公司 | Air supporting rotor heat radiation structure and motor |
CN112628281B (en) * | 2020-11-09 | 2022-02-22 | 珠海格力电器股份有限公司 | Air-bearing rotor system and motor |
DE102020129525A1 (en) * | 2020-11-10 | 2022-05-12 | Dr. Ing. H.C. F. Porsche Aktiengesellschaft | exhaust gas turbocharger |
CN112483415B (en) * | 2020-11-13 | 2022-08-12 | 西安航天动力研究所 | Liquid rocket engine low-temperature turbine pump based on integrated cylindrical supporting seat |
CN113007211B (en) * | 2021-02-07 | 2021-11-26 | 北京伯肯当代氢燃料电池实验室有限公司 | High-heat-dissipation-rate foil type axial thrust bearing, combined bearing and heat management method |
CN113107617A (en) * | 2021-04-29 | 2021-07-13 | 宋召挺 | Fluid turbine type supercharging power generation device |
CN113517785A (en) * | 2021-07-08 | 2021-10-19 | 中国航发湖南动力机械研究所 | Alternating current generator device of aircraft engine |
CN113809885A (en) * | 2021-09-06 | 2021-12-17 | 珠海格力电器股份有限公司 | A compressor and air conditioner and automobile with the compressor |
CN114337054B (en) * | 2021-12-10 | 2024-11-05 | 陕西航天西诺美灵电气有限公司 | A motor capable of resisting high overload axial impact load |
CN114876824B (en) * | 2022-05-23 | 2023-08-29 | 烟台东德实业有限公司 | Air cooling structure of high-speed centrifugal air compressor and expander integrated system |
CN115978092B (en) * | 2023-03-21 | 2023-06-16 | 中国空气动力研究与发展中心空天技术研究所 | Support structure of ultra-high speed micro rotor and design method of support structure |
CN116608203B (en) * | 2023-07-20 | 2023-10-03 | 山东华东风机有限公司 | Radial double-wave foil air bearing |
CN116792328B (en) * | 2023-07-26 | 2023-12-22 | 烟台东德实业有限公司 | Built-in water-cooling and air-cooling single-stage high-speed centrifugal air compressor |
CN116838723B (en) * | 2023-09-04 | 2023-11-03 | 天津飞旋科技股份有限公司 | Bearing body, foil hydrodynamic bearing and rotary machine shafting |
Family Cites Families (42)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS56141021A (en) * | 1980-04-02 | 1981-11-04 | Toyota Motor Corp | Bearing construction for turbo machinery |
KR900001291B1 (en) * | 1985-08-28 | 1990-03-05 | 이스즈지도샤 가부시끼가이샤 | Auxiliary apparatus for internal combustion engine |
JPH01290999A (en) * | 1988-05-14 | 1989-11-22 | Daikin Ind Ltd | fan device |
JPH07154010A (en) * | 1993-12-01 | 1995-06-16 | Fanuc Ltd | Turboblower for laser |
CN2191308Y (en) * | 1994-04-19 | 1995-03-08 | 崔援 | Electric fan with double blades |
US6294842B1 (en) * | 1997-12-19 | 2001-09-25 | Alliedsignal Inc. | Fog cycle for microturbine power generating system |
JP2000130176A (en) * | 1998-10-30 | 2000-05-09 | Isuzu Motors Ltd | Turbo charger with generator and motor |
JP2002039096A (en) * | 2000-07-27 | 2002-02-06 | Minebea Co Ltd | Air blower |
CN2558797Y (en) * | 2002-04-03 | 2003-07-02 | 廖英桐 | Improved dynamic bearing |
CN1209554C (en) * | 2002-09-23 | 2005-07-06 | 北京航空航天大学 | Miniature turbine jet engines |
JP4078983B2 (en) * | 2003-01-10 | 2008-04-23 | ソニー株式会社 | Bearing unit and rotary drive device having bearing unit |
GB0304320D0 (en) * | 2003-02-26 | 2003-04-02 | Bladon Jets Ltd | Gas turbine engines |
CN1283931C (en) * | 2004-03-18 | 2006-11-08 | 西安交通大学 | Mechanical bearing flat foil type thrust gas bearing of high speed surbine |
US7108488B2 (en) * | 2004-03-26 | 2006-09-19 | Honeywell International, Inc. | Turbocharger with hydrodynamic foil bearings |
US7948105B2 (en) * | 2007-02-01 | 2011-05-24 | R&D Dynamics Corporation | Turboalternator with hydrodynamic bearings |
CN201258910Y (en) * | 2008-08-11 | 2009-06-17 | 罗立峰 | Radial kinetic pressure air-float bearing |
KR101324226B1 (en) * | 2008-09-22 | 2013-11-20 | 삼성테크윈 주식회사 | Fluid charger |
JP2011047388A (en) * | 2009-08-28 | 2011-03-10 | Toshiba Home Technology Corp | Blower |
JP5497489B2 (en) * | 2010-03-08 | 2014-05-21 | 本田技研工業株式会社 | Centrifugal compressor |
CN102619616A (en) * | 2011-01-30 | 2012-08-01 | 梁天宇 | Turbine supercharger |
CN201982337U (en) * | 2011-04-07 | 2011-09-21 | 浙江同源鼓风机制造有限公司 | High-speed centrifugal blower |
CN102200136B (en) * | 2011-05-25 | 2012-09-05 | 北京虎渡能源科技有限公司 | Air-suspension air-supply-adjustable air blower directly driven by high-speed electric machine |
CN102242762B (en) * | 2011-05-27 | 2013-01-23 | 罗立峰 | Dynamic pressure gas radial ceramic bearing |
CN102278366A (en) * | 2011-05-27 | 2011-12-14 | 罗立峰 | Self-sealing dynamic-pressure gas radial ceramic bearing |
CN102192237A (en) * | 2011-06-07 | 2011-09-21 | 罗立峰 | Self-seal kinetic pressure gas radial ceramic bearing |
CN102261374B (en) * | 2011-06-15 | 2014-04-09 | 罗立峰 | Dynamic pressure gas thrust ceramic bearing |
CN102223007A (en) * | 2011-06-24 | 2011-10-19 | 罗立峰 | High-speed permanent magnet motor/generator |
KR102077148B1 (en) * | 2011-08-24 | 2020-02-14 | 보르그워너 인코퍼레이티드 | Bearing arrangement |
JP6065917B2 (en) * | 2012-10-16 | 2017-01-25 | 株式会社Ihi | Thrust bearing |
CN103089405B (en) * | 2013-01-09 | 2015-09-16 | 北京理工大学 | Rotor clutch type motor-driven power generation turbocharger |
CN103089407B (en) * | 2013-01-09 | 2015-01-14 | 北京理工大学 | Rotor clutch type motor-driven power generation turbocharger and auxiliary control circuit and control method thereof |
CN103306995B (en) * | 2013-05-30 | 2015-08-26 | 西安交通大学 | A kind of spline tooth pull bar combined rotor high speed direct-drive compressor structure |
CN103670672B (en) * | 2013-12-19 | 2016-03-02 | 湖南大学 | A kind of turbosupercharger |
CN203840113U (en) * | 2014-05-10 | 2014-09-17 | 台州市勃森工艺灯饰有限公司 | Air-discharge protective housing for decorative lighting motor |
CN204082684U (en) * | 2014-05-30 | 2015-01-07 | 鑫贺精密电子(东莞)有限公司 | A kind of radiation fan |
CN104265460B (en) * | 2014-08-20 | 2016-03-23 | 中国科学院工程热物理研究所 | Micro-aeroengine bearing fuel heat exchange cooling device |
CN105202027B (en) * | 2015-05-19 | 2017-10-20 | 罗立峰 | A kind of hybrid kinetic pressure gas thrust bearing |
CN105889314B (en) * | 2015-05-19 | 2019-01-04 | 罗立峰 | A kind of highway turbine booster |
CN104895924A (en) * | 2015-05-19 | 2015-09-09 | 罗立峰 | Hybrid aerodynamic journal bearing |
CN104895917A (en) * | 2015-05-19 | 2015-09-09 | 罗立峰 | Hybrid type dynamic-pressure gas thrust bearing |
HUE046304T2 (en) * | 2015-05-19 | 2020-02-28 | Lifeng Luo | Groove-type dynamic pressure gas radial bearing |
CN105895917A (en) * | 2016-06-17 | 2016-08-24 | 天津商业大学 | Method for preparing anode material of ion battery by utilizing retrograded starch |
-
2016
- 2016-05-18 CN CN201610334013.1A patent/CN105889314B/en active Active
- 2016-05-18 CN CN201610327779.7A patent/CN106026517B/en active Active
- 2016-05-18 CN CN201610329210.4A patent/CN106026492B/en active Active
- 2016-05-18 CN CN201610327807.5A patent/CN105889097B/en active Active
- 2016-05-18 CN CN201620452770.4U patent/CN205858479U/en not_active Withdrawn - After Issue
- 2016-05-18 CN CN201620452740.3U patent/CN205858947U/en active Active
- 2016-05-18 CN CN201610329288.6A patent/CN105889313B/en active Active
- 2016-05-18 CN CN201620457923.4U patent/CN205858948U/en active Active
- 2016-05-18 CN CN201620450047.2U patent/CN205858730U/en active Active
- 2016-05-18 CN CN201610327762.1A patent/CN105888818B/en active Active
- 2016-05-18 CN CN201620452845.9U patent/CN205864143U/en not_active Withdrawn - After Issue
- 2016-05-18 CN CN201620454708.9U patent/CN205858494U/en not_active Withdrawn - After Issue
- 2016-05-18 CN CN201610329302.2A patent/CN106014641B/en active Active
- 2016-05-18 CN CN201620450029.4U patent/CN205864174U/en not_active Withdrawn - After Issue
- 2016-05-19 TW TW105115473A patent/TWI704751B/en active
- 2016-05-19 TW TW105115472A patent/TWI694210B/en active
- 2016-05-19 WO PCT/CN2016/082711 patent/WO2016184414A1/en active Application Filing
- 2016-05-19 WO PCT/CN2016/082676 patent/WO2016184404A1/en active Application Filing
- 2016-05-19 WO PCT/CN2016/082707 patent/WO2016184410A1/en active Application Filing
- 2016-05-19 WO PCT/CN2016/082705 patent/WO2016184408A1/en active Application Filing
- 2016-05-19 WO PCT/CN2016/082713 patent/WO2016184416A1/en active Application Filing
- 2016-05-19 WO PCT/CN2016/082702 patent/WO2016184406A1/en active Application Filing
- 2016-05-19 WO PCT/CN2016/082709 patent/WO2016184412A1/en active Application Filing
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106026492A (en) * | 2015-05-19 | 2016-10-12 | 罗立峰 | Ultra-high-speed motor |
CN106026492B (en) * | 2015-05-19 | 2019-01-04 | 罗立峰 | A kind of super high speed motor |
Also Published As
Publication number | Publication date |
---|---|
CN205858948U (en) | 2017-01-04 |
CN105888818A (en) | 2016-08-24 |
TW201706516A (en) | 2017-02-16 |
CN105888818B (en) | 2019-01-04 |
CN106026492A (en) | 2016-10-12 |
CN106014641A (en) | 2016-10-12 |
CN205858730U (en) | 2017-01-04 |
CN205864174U (en) | 2017-01-04 |
CN106026517B (en) | 2019-01-04 |
CN105889097B (en) | 2019-01-04 |
TWI704751B (en) | 2020-09-11 |
WO2016184414A1 (en) | 2016-11-24 |
WO2016184408A1 (en) | 2016-11-24 |
TWI694210B (en) | 2020-05-21 |
WO2016184416A1 (en) | 2016-11-24 |
CN205858479U (en) | 2017-01-04 |
CN106026517A (en) | 2016-10-12 |
CN105889097A (en) | 2016-08-24 |
CN205858494U (en) | 2017-01-04 |
CN105889314B (en) | 2019-01-04 |
CN106026492B (en) | 2019-01-04 |
WO2016184406A1 (en) | 2016-11-24 |
CN205858947U (en) | 2017-01-04 |
CN105889313A (en) | 2016-08-24 |
WO2016184410A1 (en) | 2016-11-24 |
CN105889313B (en) | 2018-10-26 |
WO2016184404A1 (en) | 2016-11-24 |
WO2016184412A1 (en) | 2016-11-24 |
CN106014641B (en) | 2018-06-12 |
CN105889314A (en) | 2016-08-24 |
TW201706511A (en) | 2017-02-16 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN205864143U (en) | A kind of super high speed motor | |
CN205864142U (en) | A kind of little micromachine | |
CN205858770U (en) | A kind of little Minitype radiating fan | |
CN205858771U (en) | A kind of ultrahigh speed radiator fan | |
CN101604876A (en) | Fan-cooled rotor in shaft of high-speed permanent magnet motor | |
WO2021169493A1 (en) | Dynamic-pressure sliding vane bearing rotor system, motor and electric appliance | |
US3191079A (en) | Heavy dynamoelectric machine having nylon bearings | |
CN211474265U (en) | Rotor system and micro gas turbine generator set | |
CN109707638A (en) | A small and micro centrifugal compressor with integrated bearing and seal | |
CN204465193U (en) | A kind of wind power generator rotor support |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
AV01 | Patent right actively abandoned | ||
AV01 | Patent right actively abandoned | ||
AV01 | Patent right actively abandoned |
Granted publication date: 20170104 Effective date of abandoning: 20190104 |
|
AV01 | Patent right actively abandoned |
Granted publication date: 20170104 Effective date of abandoning: 20190104 |