CN206580483U - Gas suspension supporting mechanism - Google Patents
Gas suspension supporting mechanism Download PDFInfo
- Publication number
- CN206580483U CN206580483U CN201621306559.8U CN201621306559U CN206580483U CN 206580483 U CN206580483 U CN 206580483U CN 201621306559 U CN201621306559 U CN 201621306559U CN 206580483 U CN206580483 U CN 206580483U
- Authority
- CN
- China
- Prior art keywords
- support member
- support
- supporting mechanism
- gas suspension
- base
- 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.)
- Expired - Fee Related
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- 239000000725 suspension Substances 0.000 title claims abstract description 41
- 239000000463 material Substances 0.000 claims abstract description 11
- 230000015572 biosynthetic process Effects 0.000 claims abstract description 8
- 230000001360 synchronised effect Effects 0.000 claims description 9
- 238000000926 separation method Methods 0.000 claims description 7
- 238000010276 construction Methods 0.000 abstract description 6
- 230000000694 effects Effects 0.000 description 7
- 238000001914 filtration Methods 0.000 description 7
- 230000005540 biological transmission Effects 0.000 description 3
- 230000001174 ascending effect Effects 0.000 description 2
- 230000005484 gravity Effects 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 238000002955 isolation Methods 0.000 description 2
- 238000010521 absorption reaction Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000030279 gene silencing Effects 0.000 description 1
- 230000003319 supportive effect Effects 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B44—DECORATIVE ARTS
- B44C—PRODUCING DECORATIVE EFFECTS; MOSAICS; TARSIA WORK; PAPERHANGING
- B44C5/00—Processes for producing special ornamental bodies
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B66—HOISTING; LIFTING; HAULING
- B66F—HOISTING, LIFTING, HAULING OR PUSHING, NOT OTHERWISE PROVIDED FOR, e.g. DEVICES WHICH APPLY A LIFTING OR PUSHING FORCE DIRECTLY TO THE SURFACE OF A LOAD
- B66F3/00—Devices, e.g. jacks, adapted for uninterrupted lifting of loads
- B66F3/24—Devices, e.g. jacks, adapted for uninterrupted lifting of loads fluid-pressure operated
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B66—HOISTING; LIFTING; HAULING
- B66F—HOISTING, LIFTING, HAULING OR PUSHING, NOT OTHERWISE PROVIDED FOR, e.g. DEVICES WHICH APPLY A LIFTING OR PUSHING FORCE DIRECTLY TO THE SURFACE OF A LOAD
- B66F3/00—Devices, e.g. jacks, adapted for uninterrupted lifting of loads
- B66F3/24—Devices, e.g. jacks, adapted for uninterrupted lifting of loads fluid-pressure operated
- B66F3/25—Constructional features
-
- 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
- F04D29/002—Details, component parts, or accessories 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
- F04D29/005—Decorative aspects, i.e. features which have no effect on the functioning of the pump
-
- 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
- F04D29/403—Casings; Connections of working fluid especially adapted for elastic fluid pumps
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B66—HOISTING; LIFTING; HAULING
- B66F—HOISTING, LIFTING, HAULING OR PUSHING, NOT OTHERWISE PROVIDED FOR, e.g. DEVICES WHICH APPLY A LIFTING OR PUSHING FORCE DIRECTLY TO THE SURFACE OF A LOAD
- B66F2700/00—Lifting apparatus
- B66F2700/07—Lifting devices actuated by the driving force of water
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Life Sciences & Earth Sciences (AREA)
- Geology (AREA)
- Structural Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Seats For Vehicles (AREA)
- Toys (AREA)
- Air-Flow Control Members (AREA)
Abstract
The utility model discloses a kind of gas suspension supporting mechanism, including support base, turbine assembly, conducting element and support member；The bottom of support base is provided with air inlet and its open top；Turbine assembly is in support base and positioned at the top of air inlet, and turbine assembly is used to form air-flow from lower to upper；Conducting element is in hollow structure and both ends open, and conducting element is in support base and positioned at the top of turbine assembly；Support member is sealed in hollow structure and top, and the top of support member is used to support other objects, and support member is movably sheathed between conducting element and support base, and with one close to the first position of support base and the second place away from support base；The air-flow of turbine assembly formation acts on support member after being oriented to through conducting element, so that support member is moved from first position to the second place.The gas suspension supporting mechanism uses manpower and material resources sparingly without manually operated, more convenient operation, with less volume, occupied little space, and simple in construction, cost reduction.
Description
Technical field
The utility model is related to a kind of liftable supporter, more particularly to a kind of gas suspension simple in construction, easy to operate
Supporting mechanism.
Background technology
The existing lifting platform or lowering or hoisting gear for praising object is all often to use gear push rod structure, and it generally includes bottom
Seat, support, fall way, bracket, transmission mechanism and operating mechanism, bracket are located at the upper end of fall way, and transmission mechanism includes mutually nibbling
Gear, the rack of conjunction, operating mechanism are provided with gear, and rack is fixed on fall way, are driven by the operation operating mechanism
Fall way is lifted, but existing such lifting device structure is all more complicated, cost is higher, and operation is very inconvenient, wastes big
Measure labour.
Therefore, it is necessary to a kind of gas suspension supporting mechanism simple in construction, easy to operate be provided, to overcome above-mentioned existing skill
Deficiency in the presence of art.
Utility model content
The purpose of this utility model is to provide a kind of gas suspension supporting mechanism simple in construction, easy to operate.
To achieve the above object, the technical solution of the utility model is：A kind of gas suspension supporting mechanism is provided, it includes branch
Support seat, turbine assembly, conducting element and support member；The bottom of the support base is provided with air inlet and its open top；Turbine assembly
In the support base and positioned at the top of the air inlet, the turbine assembly is used to form air-flow from lower to upper；Institute
Conducting element is stated in hollow structure and both ends open, the conducting element is in the support base and positioned at the upper of the turbine assembly
Side；The support member is sealed in hollow structure and top, and the top of the support member is used to support other objects, the support member
Movably it is sheathed between the conducting element and the support base, and with one close to the first position of the support base and one
The second place away from the support base；The air-flow of the turbine assembly formation acts on the branch after being oriented to through the conducting element
Support member, so that the support member is moved from the first position to the second place.
It is preferred that the top of the support member is provided with the supporting part for being used for carrying supported object part.
It is preferred that when the support member is in the second place, the support base is convexedly stretched at the top of the support member
Top.
It is preferred that location structure is provided between the support member and the support base, with the second place
The support member is positioned.
It is preferred that the location structure includes being convexly equipped in the first flange of the outer wall of the support member and is convexly equipped in the branch
The second flange of the inwall of seat is supportted, when the support member is in the second place, first flange and second flange
It is inconsistent.
It is preferred that being provided with the guiding extended along the moving direction of the support member between the support member and the support base
Structure, to be oriented to the mobile of the support member.
It is preferred that the guide frame includes the fin and groove that are engaged, the fin is located at the support member, described
One of support base, the groove is located at the other of the support member, described support base.
It is preferred that offering venthole on the support member.
It is preferred that the inner surface at the top of the support member is provided with separation layer.
It is preferred that the gas suspension supporting mechanism also includes the separator in the support base, the support member can
Movably it is located between the conducting element and the separator.
It is preferred that the separator is integrally formed with the conducting element by flexible material.
It is preferred that the gas suspension supporting mechanism also includes in the mounting seat in the support base, the mounting seat
Provided with mounting hole that is corresponding with the shape of the turbine assembly and connecting the air inlet, the turbine assembly is embedded at described
In mounting hole.
It is preferred that the mounting seat is molded using flexible material.
It is preferred that the support base includes base and is connected to the support frame of the base, the top tool of support frame as described above
There is the opening, the air inlet is located at the base.
It is preferred that the base is also provided with drive mechanism, the drive mechanism is used to drive support frame as described above, the branch
Support member is relative to the base synchronous rotary.
Compared with prior art, be provided with due to gas suspension supporting mechanism of the present utility model, in its support base is in hollow knot
The conducting element of structure and both ends open, conducting element is located at the top of turbine assembly, and the turbine assembly is located at the top of air inlet, is used for
Air-flow from lower to upper is formed, support member is sealed in hollow structure and top, and support member is movably sheathed on conducting element and branch
Support seat between, turbine assembly formation air-flow be oriented to through conducting element after act on support member so that support member from first position to
The second place is moved, so that support member is raised, when turbine assembly is stopped, support member is moved to first under gravity
Position, by the flexible of support member, makes the object of its top carrying can be with ascending, descending, without manually operated, more convenient operation, section
About manpower and materials, and after support member is moved down, gas suspension supporting mechanism has less volume, occupies little space, while the gas is outstanding
The simple in construction of over draft support mechanism, cost reduction.
Brief description of the drawings
Fig. 1 is the structural representation of the utility model gas suspension supporting mechanism.
Fig. 2 is the structural representation of another angles of Fig. 1.
Fig. 3 is Fig. 1 exploded view.
Fig. 4 is Fig. 1 sectional view.
Fig. 5 is conducting element and the structural representation of another angle of separator in Fig. 3.
Fig. 6 is Fig. 5 sectional view.
Fig. 7 is the structural representation of another angle of turbine assembly in Fig. 3.
Fig. 8 is the structural representation of the another angles of Fig. 7.
Fig. 9 is the sectional view of mounting seat in Fig. 3.
Figure 10 is Fig. 1 another view.
Figure 11 is Figure 10 sectional view.
Embodiment
Element numbers similar in embodiment of the present utility model, accompanying drawing, which are described, with reference now to accompanying drawing represents similar member
Part.
First with reference to shown in Fig. 1-4, gas suspension supporting mechanism 1 provided by the utility model, including support base 10, whirlpool
Wheel assembly 20, conducting element 30 and support member 40.Wherein, the bottom of support base 10 is provided with air inlet 121 and its open top；Whirlpool
Wheel assembly 20 is in support base 10 and positioned at the top of air inlet 121, and turbine assembly 20 is used to form air-flow from lower to upper；
Conducting element 30 is in hollow structure and both ends open, and conducting element 30 is led in support base 10 and positioned at the top of turbine assembly 20
Stream part 30 is used to be oriented to the air-flow that turbine assembly 20 is produced；Support member 40 is sealed in hollow structure and top, support member
40 top is used to support other objects, and support member 40 is movably sheathed between conducting element 30 and support base 10, and support
Part 40 has one close to the first position of support base 10 and the second place away from support base 10；The gas of the formation of turbine assembly 20
Support member 40 is acted on after the guiding for flowing through conducting element 30, so that support member 40 is moved from first position to the second place.
With continued reference to shown in Fig. 1-4, the top of the support member 40 can also set supporting part 41, and supporting part 41 has
One bottom wall 411 and the side wall 412 upwardly extended along the bottom wall 411, the supporting part 41 is to carry supported object part and can prevent
Object slides to side.Wherein, supporting part 41 can be integrally formed with support member 40, can also be fixed on or be detachably connected in addition
In the top of support member 40.The shape of supporting part 41 can be adapted with the shape of supported object part, also can be with supported object part
Shape is different, and this is well known to those skilled in the art.
In a kind of preferred embodiment of the present utility model, supporting part 41 is integrally formed with support member 40, and the bottom of supporting part 41
Wall 411 is the top of support member 40, and seal support part 40 is carried out by the bottom wall 411 of supporting part 41, and side wall 412 is along the bottom wall
411 upwardly extend and curved structure, certainly, the shape of side wall 412 are not limited to arc.
When support member 40 is in first position, the bottom of extensible member 40 contacts at the bottom of conducting element 30 (after referring to
State), the supporting part 41 that supporting part 41 is under the position of relatively close support frame 13, this state can hold object, work as support member
40 when being risen to the second place for being relatively distant from support frame 13 by first position, and supporting part 41 is at higher position (see figure
11), so that the object on supporting part 41 is transplanted on into higher position, and the higher position can be constantly in.
Further, the ratio between conducting element 30, extensible member 40, support frame 13 can be arranged as required to, so as to stretch
When contracting part 40 is in first position, its bottom contacts at the bottom of conducting element 30, and the supporting part 41 at the top of it is just carried on
The top (see Fig. 4) of support frame 1, to increase supportive.
Understandably, the form and dimension of supporting part 41 can be also arranged as required to, so that support member 40 is in first
When putting, supporting part 41 can be in retraction support frame 13, and this has no effect on the realization of technical solutions of the utility model.
Further, one layer of separation layer (not shown) is additionally provided with the inner surface at the top of support member 40, this practicality is new
In type, the separation layer is on the inner surface of the bottom 411 of supporting part 41, and the separation layer is made of flexible material, so, when
Airflow function is when the top of the support member 40, and produced vibrations and noise absorb by the separation layer, can reduce support machine
The noise of structure 1.
With continued reference to shown in Fig. 1-3, the support base 10 includes base 11, connecting seat 12 and support frame 13, wherein, connection
Seat 12 is pivotably coupled on base 11 and (referred to aftermentioned), and the correspondence of support frame 13 is fixed on connecting seat 12, and support frame 13 is in
Hollow structure and its top have the opening.In the utility model, air inlet 121 is located at the bottom of connecting seat 12, and connection
The top of seat 12 connects the hollow structure of support frame 13, and turbine assembly 20 is arranged on the top of connecting seat 12, so that gas can
Enter from air inlet 121 and air-flow from lower to upper is formed in the presence of turbine assembly 20.
Preferably, the top and bottom of connecting seat 12 are designed in hollow out, so that gas can pass through, but not as
Limit, can also set the air inlet of other forms.
With reference to shown in Fig. 3-4, filtration members 14 and support member 15 are additionally provided with shell body 10.Wherein, filtration members 14 are located at company
The top of joint chair 12, support member 15 is arranged on connecting seat 12 and pressure holding is in the top of filtration members 14, and support member 15 is in hollow out
Structure (see Fig. 3), turbine assembly 20 is installed on the support member 15.So, the gas entered through air inlet 121 is first by filtration members
After 14 are filtered, then air-flow from bottom to top formed by the effect of turbine assembly 20；Meanwhile, filtration members 14 also to
The noise of the direction of base 11 transmission has isolation, absorption, so as to reduce noise produced when supporting mechanism 1 works.
In the utility model, filtration members 14 are made of flexible material, for example, be made using sound-absorbing sponge, but not with this
It is limited.
Referring now to Fig. 7-8, turbine assembly 20 includes impeller chimney 21, the impeller 22 in impeller chimney 21 and is connected to
The motor (non-label) of impeller 22, is rotated by motor driven impeller 22, so as to form air-flow from lower to upper.The turbine assembly
20 other structures and operation principle are well known to those skilled in the art, and will not be repeated here.
With reference to shown in Fig. 3-4,7-9, gas suspension supporting mechanism 1 of the present utility model also includes a mounting seat 50, and it is installed
In the top of support member 15, for installing turbine assembly 20.Specifically, the mounting seat 50 is provided with the shape with turbine assembly 20
Corresponding mounting hole 51, and the lower end of mounting seat 50 offers the through hole (non-label) of connection mounting hole 51, in mounting seat 50
Also it is convexly equipped with supporting part 52.The mounting seat 50 is located at the top of support member 15, and its outer wall contacts at the inwall of support frame 13, turbine
Component 20 is embedded in mounting hole 51, meanwhile, conducting element 30 is arranged in the outside of turbine assembly 20, and its bottom contacts at branch
On support part 52, as shown in Figure 4.
Preferably, the mounting seat 50 is integrally formed using flexible material, is molded for example with sound-absorbing sponge, therefore the installation
Seat 50 can absorb turbine assembly 20 operationally produced vibration and noise, further reduction gas suspension supporting mechanism 1
Noise.
Referring again to shown in Fig. 3-4, gas suspension supporting mechanism 1 of the present utility model also includes separator 60, separator 60
Shape it is corresponding with the shape of support frame 13, its inwall for being close to support frame 13 is set, and separator 60 and conducting element 30
Between there is certain interval, the gap is more than the thickness of support member 40, and support member 40 is movably disposed in conducting element 30 with isolating
Between part 60.Separator 60 is used to absorb, isolates the noise produced when turbine assembly 20 works, so that the gas suspension supports machine
Structure 1 has less noise.
With reference to above description, gas suspension supporting mechanism 1 of the present utility model, bottom is provided with the filtering of erasure effect well
Part 14 and mounting seat 50, the inner surface at the top of support member 40 are provided with separator 60 provided with separation layer, sidepiece, by top, bottom
The sound-absorbing structure that portion, sidepiece are set, makes the surrounding of gas suspension supporting mechanism 1 be respectively provided with good erasure effect, so that the gas
Suspension support mechanism 1 has minimum noise.
With reference to shown in Fig. 3-6, separator 60 is connected with the bottom of conducting element 30, and gap between the two is formed for support
The passage that part 40 is moved up and down, the top of conducting element 30 is protruded out outside separator 60；When support member 40 is in first position,
Its bottom contacts at the bottom being connected of separator 60 and conducting element 30.
Further, shape of the bottom junctions provided with one with the bottom of support member 40 of separator 60 and conducting element 30
The corresponding neck of shape, thickness, when support member 40 is in first position, its bottom is sticked in the neck and contacts at the neck
Bottom surface.In the utility model, it is in step-like supporting part 31 that the bottom of conducting element 30, which has one, positioned at the lower section of supporting part 31
Gap between conducting element 30 and separator 60 forms neck 32, as shown in Figure 6.Meanwhile, the bottom of support member 40 is provided with one
The convex shoulder 42 corresponding with supporting part 31, when support member 40 is in first position, its convex shoulder 42 is contacted on the supporting part 31,
And the bottom of support member 40 is sticked in neck 32, as shown in Figure 4.
As shown in figure 3, the bottom of the outer wall of separator 60 is provided with breach 61, the inwall of support frame 13 is provided with and the breach
61 corresponding lug boss (not shown), when installing separator 60 and conducting element 30, make separator 60 be close to support frame 13
The correspondence of breach 61 on inwall, and separator 60 is sticked in the lug boss on support frame 13, realizes the positioning to separator 60, peace
After dress, the bottom of conducting element 30 and separator 60 is contacted on the supporting part 52 of mounting seat 50.
More specifically, separator 60 is integrally formed with conducting element 30, and utilize flexible material (such as sound-absorbing sponge) one
Separator 60 and conducting element 30 are molded, so that both of which has good silencing function, turbine assembly 20 can be absorbed well
The noise produced during work.
Extend with reference to being provided with shown in Fig. 3-5,11, between support member 40 and separator 60 along the short transverse of support frame 13
Guide frame, to be oriented to the mobile of support member 40；And provided with location structure between support member 40 and support frame 13,
To be positioned to the support member 40 in the second place.
In the utility model, guide frame be between support member 40 and separator 60 and cooperate groove with it is convex
Rib, fin is located at another in support member 40, separator 60 located at one of the support member 40, separator 60, the groove
One, and groove, fin are along the glide direction extension of support member 40.Certainly, guide frame is not limited to groove and fin, also
It could be arranged to other structures.
More specifically, offering the groove 62 extended along its short transverse on the inwall of separator 60.Accordingly, support member
The fin 43 corresponding with groove 62 is convexly equipped with 40 outer wall, the length of the fin 43 is less than the height of support member 40.Support
After part 40 is installed, the correspondence of fin 43 is sticked in groove 62, so as to be oriented to for sliding up and down for support member 40, such as Fig. 3-5
It is shown.
Understandably, guide frame can also be arranged between support member 40 and support frame 13.
As shown in figure 11, location structure includes the first flange and the second flange located at support frame 13 located at support member 40
131, wherein, the first flange convexedly stretches in the periphery of support member 40, and the second flange 131 is convexly equipped with the inwall of support frame 13, works as support
When part 40 slides up to the second place, the first flange contacts at the second flange 131, so as to prevent support member 40 from support frame 13
It is upper to depart from.
Preferably, first flange is the end (see Figure 11) of above-mentioned fin 43, when support member 40 slides up to
During the second place, the end of fin 43 contacts at the second flange 131, realizes the positioning of support member 40.
Certainly, location structure can also be located between support member 40 and separator 60.
Referring now to shown in Figure 10-11, venthole 44 is offered with also extending through on the side wall 412 of the support member 40, when
Support member 40 be in the second place when, venthole 44 is exposed to support frame 13, so, turbine assembly 20 formation airflow function in
After support member 40 is moved it up, the inwall of support member 40 has guide effect to the air-flow, so that the air-flow is via branch
Gap between support member 40, conducting element 30 is down moved, and is finally flowed out via venthole 44.
Further in conjunction with shown in Fig. 4,11, drive mechanism 70 is additionally provided with base 11, the drive mechanism 70 is used for drive connection
Seat 12, support frame 13 rotate relative to base 11.And the synchronous rotary therewith of support member 40 is driven by support frame 13, make carrying
Rotated with the object on support member 40.
Specifically, drive mechanism 70 include motor 71 on the connecting seat 12 and on base 11 and with the motor 71
The fluted disc 72 being engaged, the rotation by motor 71 relative to fluted disc 72, so that the connecting seat 12 being connected with motor 71 is therewith
Synchronous axial system, drives the support frame 13 being attached to synchronous axial system therewith, due to support frame 13 and separator by connecting seat 12
It is positioned between 60, guide frame is provided between separator 60 and support member 40, therefore, isolation is driven by support frame 13
Part 60, the synchronous axial system of support member 40, so that the object at the top of support member 40 is rotated with.
It is lower with reference to shown in Fig. 1-11, the different use states to the utility model gas suspension supporting mechanism 1 are illustrated.
As Figure 1-4, when gas suspension supporting mechanism 1 is in the first use state, support member 40 is in relatively close branch
The first position of support 13, its bottom is sticked in the neck 32 between conducting element 30 and separator 80 Nei and contacts at neck 32
Bottom surface, and convex shoulder 42 contacted on supporting part 31, can place object on supporting part 41.
When turbine assembly 20 works, turbine assembly 20 makes to enter the gas of air formation from lower to upper in support frame 13
Stream, the air-flow acts on the top (bottom wall 411 for acting on supporting part 41) of support member 40 after the guiding of conducting element 30, from
And support member 40 is moved up in the presence of air-flow, the object on supporting part 41 rises therewith, by supporting part 41
Object is transplanted on higher position；When support member 40 is moved to the second place for being relatively distant from support frame 13, first thereon is convex
Edge and the second flange 131 on support frame 13 are inconsistent, so as to prevent support member 40 from departing from support frame 13.In turbine assembly 20 not
On the premise of being stopped, support member 40 is constantly in the second place, object is constantly in higher position, such as Figure 10-11 institutes
Show.
When drive mechanism 70 is run, motor 71 is rotated relative to fluted disc 72, and then makes the connecting seat 12 of installation motor 71
Concomitant rotation, connecting seat 12 drives support frame 13 relative to the synchronous rotary of base 11, due between support frame 13 and separator 60
It is positioned, and provided with the guide frame vertically extended between separator 60 and support member 40, therefore, support frame 13 drives
Separator 60, conducting element 30, support member 40 synchronous rotary therewith, thus drive the object synchronous rotary on support member 40.
When turbine assembly 20 is stopped, support member 40 loses the effect of air-flow, so that under in the presence of its gravity
First position is down to, its bottom is sticked in the neck 32 between conducting element 30 and separator 60 Nei and contacts at neck 32 again
Bottom surface, reduce the volume of the supporting mechanism 1, occupy little space, as shown in Fig. 1-2,4.
Due to gas suspension supporting mechanism 1 of the present utility model, it is in hollow structure and both ends open to be provided with its support base 10
Conducting element 30, conducting element 30 be located at turbine assembly 20 top, the turbine assembly 20 be located at air inlet top, for being formed
Air-flow from lower to upper, support member 40 is sealed in hollow structure and top, support member 40 be movably sheathed on conducting element 30 with
Between support base 10, the air-flow of the formation of turbine assembly 20 acts on support member 40 after being oriented to through conducting element 30, so that support member 40
Moved from first position to the second place, so that support member 40 is raised, when turbine assembly 20 is stopped, support member 40 is in weight
First position is moved under power effect, by the flexible of support member 40, makes the object of its top carrying can be with ascending, descending, without hand
After dynamic operation, more convenient operation is used manpower and material resources sparingly, and support member 40 is moved down, gas suspension supporting mechanism 1 has less body
Product, occupies little space, while the simple in construction of the gas suspension supporting mechanism 1, cost reduction.
Above disclosed is only preferred embodiment of the present utility model, can not limit this practicality with this certainly new
The interest field of type, therefore the equivalent variations made according to present utility model application the scope of the claims, still belong to the utility model and are covered
Scope.
Claims (15)
1. a kind of gas suspension supporting mechanism, it is characterised in that including：
Support base, the bottom of the support base is provided with air inlet and its open top；
Turbine assembly, its in the support base and positioned at the top of the air inlet, the turbine assembly be used to being formed by
Under air-flow up；
Conducting element, the conducting element is in hollow structure and both ends open, and the conducting element is in the support base and positioned at institute
State the top of turbine assembly；
Support member, the support member is sealed in hollow structure and top, and the top of the support member is used to support other objects, institute
Support member is stated movably to be sheathed between the conducting element and the support base, and with one close to the first of the support base
Position and the second place away from the support base；
The air-flow of turbine assembly formation acts on the support member after being oriented to through the conducting element so that the support member by
Moved to the second place first position.
2. gas suspension supporting mechanism as claimed in claim 1, it is characterised in that the top of the support member, which is provided with, to be used to carry
The supporting part of supported object part.
3. gas suspension supporting mechanism as claimed in claim 1, it is characterised in that the support member is in the second place
When, the top of the support base is convexedly stretched at the top of the support member.
4. gas suspension supporting mechanism as claimed in claim 1, it is characterised in that set between the support member and the support base
There is location structure, to be positioned to the support member in the second place.
5. gas suspension supporting mechanism as claimed in claim 4, it is characterised in that the location structure includes being convexly equipped in the branch
First flange of the outer wall of support member and be convexly equipped in the support base inwall the second flange, the support member be in described second
During position, first flange and second flange are inconsistent.
6. gas suspension supporting mechanism as claimed in claim 1, it is characterised in that set between the support member and the support base
There is the guide frame along the moving direction extension of the support member, to be oriented to the mobile of the support member.
7. gas suspension supporting mechanism as claimed in claim 6, it is characterised in that the guide frame includes the fin being engaged
And groove, the fin is one of located at the support member, described support base, and the groove is located at the support member, described
The other of support base.
8. gas suspension supporting mechanism as claimed in claim 1, it is characterised in that offer venthole on the support member.
9. gas suspension supporting mechanism as claimed in claim 1, it is characterised in that the inner surface at the top of the support member is provided with
Separation layer.
10. gas suspension supporting mechanism as claimed in claim 1, it is characterised in that also including in the support base every
Off member, the support member is movably disposed between the conducting element and the separator.
11. gas suspension supporting mechanism as claimed in claim 10, it is characterised in that the separator passes through with the conducting element
Flexible material is integrally formed.
12. gas suspension supporting mechanism as claimed in claim 1, it is characterised in that also including the peace in the support base
Seat is filled, the mounting seat is provided with mounting hole corresponding and connecting the air inlet with the shape of the turbine assembly, described
Turbine assembly is embedded in the mounting hole.
13. gas suspension supporting mechanism as claimed in claim 12, it is characterised in that the mounting seat using flexible material into
Type.
14. gas suspension supporting mechanism as claimed in claim 1, it is characterised in that the support base includes base and is connected to
The support frame of the base, the top of support frame as described above has the opening, and the air inlet is located at the base.
15. gas suspension supporting mechanism as claimed in claim 14, it is characterised in that the base is also provided with drive mechanism,
The drive mechanism is used to drive support frame as described above, the support member relative to the base synchronous rotary.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2016108211175 | 2016-09-13 | ||
| CN201610821117 | 2016-09-13 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206580483U true CN206580483U (en) | 2017-10-24 |
Family
ID=58915024
Family Applications (6)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621305925.8U Active CN206320056U (en) | 2016-09-13 | 2016-11-30 | air suspension fan |
| CN201621306559.8U Expired - Fee Related CN206580483U (en) | 2016-09-13 | 2016-11-30 | Gas suspension supporting mechanism |
| CN201611092801.0A Active CN106698233B (en) | 2016-09-13 | 2016-11-30 | Air suspension supporting mechanism |
| CN201621305114.8U Expired - Fee Related CN206317598U (en) | 2016-09-13 | 2016-11-30 | Gas suspension goods of furniture for display rather than for use |
| CN201611087512.1A Expired - Fee Related CN106704222B (en) | 2016-09-13 | 2016-11-30 | Air suspension fan |
| CN201611086792.4A Expired - Fee Related CN106739742B (en) | 2016-09-13 | 2016-11-30 | Air suspension ornament |
Family Applications Before (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621305925.8U Active CN206320056U (en) | 2016-09-13 | 2016-11-30 | air suspension fan |
Family Applications After (4)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611092801.0A Active CN106698233B (en) | 2016-09-13 | 2016-11-30 | Air suspension supporting mechanism |
| CN201621305114.8U Expired - Fee Related CN206317598U (en) | 2016-09-13 | 2016-11-30 | Gas suspension goods of furniture for display rather than for use |
| CN201611087512.1A Expired - Fee Related CN106704222B (en) | 2016-09-13 | 2016-11-30 | Air suspension fan |
| CN201611086792.4A Expired - Fee Related CN106739742B (en) | 2016-09-13 | 2016-11-30 | Air suspension ornament |
Country Status (1)
| Country | Link |
|---|---|
| CN (6) | CN206320056U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106698233A (en) * | 2016-09-13 | 2017-05-24 | 东莞市卓奇峰智能科技有限公司 | Air suspension supporting mechanism |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107421042A (en) * | 2017-07-14 | 2017-12-01 | 席光凤 | a humidifier |
| CN107388461A (en) * | 2017-07-14 | 2017-11-24 | 席光凤 | An automatic humidity regulating humidifier |
| CN107421043A (en) * | 2017-07-14 | 2017-12-01 | 席光凤 | spray ring of humidifier |
| CN107449086A (en) * | 2017-07-14 | 2017-12-08 | 席光凤 | Rotating block for humidifier |
| CN107449089A (en) * | 2017-07-14 | 2017-12-08 | 席光凤 | A humidifier with spray ring |
Family Cites Families (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1042905C (en) * | 1991-08-14 | 1999-04-14 | 刘江河 | Spray crystal ball that can rotate and move up and down |
| CN101555977B (en) * | 2008-04-11 | 2011-06-22 | 鸿富锦精密工业（深圳）有限公司 | Support device |
| EP3190347B1 (en) * | 2009-03-04 | 2018-07-18 | Dyson Technology Limited | A fan |
| GB2468315A (en) * | 2009-03-04 | 2010-09-08 | Dyson Technology Ltd | Tilting fan |
| GB2532557B (en) * | 2012-05-16 | 2017-01-11 | Dyson Technology Ltd | A fan comprsing means for suppressing noise |
| CN204043032U (en) * | 2014-07-10 | 2014-12-24 | 张伟 | Integral type humidification electric heating fan |
| CN105179478B (en) * | 2015-07-15 | 2018-08-21 | 张修竹 | A kind of Porous gas suspension support system applied to full physical simulation |
| CN105402637A (en) * | 2015-11-12 | 2016-03-16 | 董旭 | Air suspension lamp |
| CN205344286U (en) * | 2016-01-29 | 2016-06-29 | 福建省德化县冠鸿陶瓷有限公司 | Pottery goods of furniture for display rather than for use |
| CN206320056U (en) * | 2016-09-13 | 2017-07-11 | 东莞市卓奇峰智能科技有限公司 | air suspension fan |
-
2016
- 2016-11-30 CN CN201621305925.8U patent/CN206320056U/en active Active
- 2016-11-30 CN CN201621306559.8U patent/CN206580483U/en not_active Expired - Fee Related
- 2016-11-30 CN CN201611092801.0A patent/CN106698233B/en active Active
- 2016-11-30 CN CN201621305114.8U patent/CN206317598U/en not_active Expired - Fee Related
- 2016-11-30 CN CN201611087512.1A patent/CN106704222B/en not_active Expired - Fee Related
- 2016-11-30 CN CN201611086792.4A patent/CN106739742B/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106698233A (en) * | 2016-09-13 | 2017-05-24 | 东莞市卓奇峰智能科技有限公司 | Air suspension supporting mechanism |
| CN106698233B (en) * | 2016-09-13 | 2023-09-05 | 东莞市卓奇峰智能科技有限公司 | Air suspension supporting mechanism |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106739742B (en) | 2022-05-17 |
| CN106698233B (en) | 2023-09-05 |
| CN206317598U (en) | 2017-07-11 |
| CN106704222A (en) | 2017-05-24 |
| CN106739742A (en) | 2017-05-31 |
| CN106698233A (en) | 2017-05-24 |
| CN206320056U (en) | 2017-07-11 |
| CN106704222B (en) | 2023-02-14 |
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| Date | Code | Title | Description |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20171024 |