CN108327914A - A kind of fast disassembly type motor cabinet - Google Patents
A kind of fast disassembly type motor cabinet Download PDFInfo
- Publication number
- CN108327914A CN108327914A CN201810278378.6A CN201810278378A CN108327914A CN 108327914 A CN108327914 A CN 108327914A CN 201810278378 A CN201810278378 A CN 201810278378A CN 108327914 A CN108327914 A CN 108327914A
- Authority
- CN
- China
- Prior art keywords
- motor
- nacelle
- level
- boss
- connector
- 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.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D29/00—Power-plant nacelles, fairings or cowlings
- B64D29/06—Attaching of nacelles, fairings or cowlings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/13—Propulsion using external fans or propellers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K5/00—Casings; Enclosures; Supports
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Power Engineering (AREA)
- Details Of Aerials (AREA)
Abstract
The present invention proposes a kind of fast disassembly type motor cabinet, including：Motor contact, radome fairing, blade, motor, nacelle connector and motor nacelle；Motor contact is fixedly connected with motor, and motor contact is fixedly connected with radome fairing, and nacelle connector is fixedly connected with motor nacelle；Blade is mounted on motor；Motor contact includes motor first order boss, motor second level boss and motor third level boss；Nacelle connector includes nacelle first order boss, nacelle second level concave station and nacelle third level boss；Nacelle second level concave station is concave-convex mating structure with motor third level boss；Motor second level boss and nacelle third level boss consistency of thickness, this motor cabinet realizes the fast assembling-disassembling of motor with simple mechanical structure and is securely loaded, the modular assembly of unmanned plane motor part may be implemented, save carry unmanned plane go out operation when vanning space, decrease the time before unmanned machine operation.
Description
Technical field
The invention belongs to unmanned plane accessory technical field, especially a kind of fast disassembly type motor cabinet.
Background technology
At this stage, unmanned plane industry development is rapid, and application of the unmanned plane in all trades and professions is also more wide.It is answered in industry
It is one of the key condition that unmanned plane product can be promoted well in the process, having higher portability.Each component of unmanned plane
Fast-detachable modular also become one of an important factor for each unmanned plane manufacturer will consider in the design process.
Invention content
To solve the above-mentioned problems, the present invention provides a kind of fast disassembly type motor cabinets.
Specific technical solution is as follows：
A kind of fast disassembly type motor cabinet, including：Motor contact, radome fairing, blade, motor, nacelle connector and motor are short
Cabin；
The motor contact is fixedly connected with motor, and the motor contact is fixedly connected with radome fairing, the nacelle
Connector is fixedly connected with motor nacelle；
The blade is mounted on motor；
The motor contact includes motor first order boss, motor second level boss and motor third level boss；
The nacelle connector includes nacelle first order boss, nacelle second level concave station and nacelle third level boss；
Nacelle second level concave station is concave-convex mating structure with motor third level boss；
Motor second level boss and nacelle third level boss consistency of thickness.
Preferably, further include locking device.
Preferably, the locking device includes mechanical locking device and magnet locking device.
Preferably, the connection type of the motor contact and motor connects for screw.
Preferably, the connection type of the motor contact and radome fairing is screw connection or cementing.
Preferably, the nacelle connector and the connection type of motor nacelle are that screw is connect or cementing.
Preferably, the material of the radome fairing, motor contact and nacelle connector is aluminium alloy, steel, polyethylene, poly- breast
It is one or more in acid, UV resins, cork wood.
Compared with the existing technology, a kind of fast disassembly type motor cabinet of the present invention has the advantage that：
A kind of fast disassembly type motor cabinet proposed by the present invention, this motor cabinet realize the fast of motor with simple mechanical structure
Speed is dismounted and is securely loaded, and the modular assembly of unmanned plane motor part may be implemented, and is saved and is carried the outgoing operation of unmanned plane
When vanning space, decrease the time before unmanned machine operation.
Description of the drawings
Fig. 1 is overall structure diagram when a kind of fast disassembly type motor cabinet proposed by the present invention uses mechanical interlocking；
Fig. 2 is overall structure diagram when a kind of fast disassembly type motor cabinet proposed by the present invention is locked using magnetic；
Fig. 3 is the partial schematic diagram of connector when a kind of fast disassembly type motor cabinet proposed by the present invention uses mechanical interlocking；
Fig. 4 is the partial schematic diagram of connector when a kind of fast disassembly type motor cabinet proposed by the present invention is locked using magnetic；
Fig. 5 is a kind of motor contact schematic diagram of fast disassembly type motor cabinet proposed by the present invention；
Fig. 6 is a kind of nacelle connector schematic diagram of fast disassembly type motor cabinet proposed by the present invention.
Reference sign：
1 motor contact, 2 radome fairing, 3 blade, 4 motor, 5 nacelle connector, 6 mechanical locking device
7 motor nacelle, 8 magnet locking device, 11 motor first order boss, 12 motor second level boss
13 motor third level boss, 51 nacelle first order boss, 52 nacelle second level concave station
53 nacelle third level boss
Specific implementation mode
Below in conjunction with the specific implementation mode technical solution that present invention be described in more detail.It should be appreciated that being described herein as
Specific implementation mode be only used to explain the present invention, be not intended to limit the present invention.
In the description of the present invention, it is to be understood that, term "center", " longitudinal direction ", " transverse direction ", "upper", "lower",
The orientation or positional relationship of the instructions such as "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outside" is
It is based on the orientation or positional relationship shown in the drawings, is merely for convenience of description of the present invention and simplification of the description, rather than instruction or dark
Show that signified device or element there must be specific side, with specific azimuth configuration and operation, therefore should not be understood as to this
The limitation of invention.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " installation ", " phase
Even ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or be integrally connected；It can
Can also be electrical connection to be mechanical connection；Can be directly connected to, can also indirectly connected through an intermediary, Ke Yishi
Connection inside two elements.For the ordinary skill in the art, above-mentioned term can be understood by concrete condition
Concrete meaning in the present invention.
The present invention will be described in detail below with reference to the accompanying drawings and embodiments.
Fig. 1 is overall structure diagram when a kind of fast disassembly type motor cabinet proposed by the present invention uses mechanical interlocking, including：
Motor contact 1, radome fairing 2, blade 3, motor 4, nacelle connector 5, mechanical locking device 6 and motor nacelle 7；The motor
Connector 1 is fixedly connected with motor 4 by screw, as shown in figure 3, the axial direction of the motor contact 1 has 4 circular holes, screw
Motor contact 1 can be fixedly connected with motor 4 across circular hole, the motor contact 1 is fixedly connected with radome fairing 2, tool
Body connection type include screw connection and it is cementing, the nacelle connector 5 is fixedly connected with motor nacelle 7, specific connection type
It is connected including screw or cementing；The blade 3 is mounted on motor 4, and motor 4 drives blade 3 to rotate, as shown in figure 5, the electricity
Machine connector 1 includes motor first order boss 11, motor second level boss 12 and motor third level boss 13；As shown in fig. 6, institute
It includes nacelle first order boss 51, nacelle second level concave station 52 and nacelle third level boss 53 to state nacelle connector 5；The nacelle
Second level concave station 52 is concave-convex mating structure with motor third level boss 13, and motor third level boss 13 can be in the nacelle second level
It is slided in the slideway of concave station 52, finally fits like a glove and dock with nacelle second level concave station 52；Motor second level boss 12 with
53 consistency of thickness of nacelle third level boss, nacelle third level boss 53 can play the role of limit, and motor contact 1 can only edge
A direction rotation (counterclockwise or clockwise), this direction turns to identical with motor 4.When motor 4 rotates extremely along this direction
When extreme position, the limit hole on limit hole and nacelle first order boss 51 on motor first order boss 11 is in concentric position
It sets, is at this time inserted into mechanical locking device 6, mechanical locking device 6 plays the role of limit at this time, mechanical locking device at this time
6 be check lock lever.
Fig. 2 is overall structure diagram when a kind of fast disassembly type motor cabinet proposed by the present invention is locked using magnetic, including：
Motor contact 1, radome fairing 2, blade 3, motor 4, nacelle connector 5, magnet locking device 8 and motor nacelle 7；The motor
Connector 1 is fixedly connected with motor 4 by screw, as shown in figure 4, the axial direction of the motor contact 1 has 4 circular holes, screw
Motor contact 1 can be fixedly connected with motor 4 across circular hole, the motor contact 1 is fixedly connected with radome fairing 2, tool
Body connection type include screw connection and it is cementing, the nacelle connector 5 is fixedly connected with motor nacelle 7, specific connection type
It is connected including screw or cementing；The blade 3 is mounted on motor 4, and motor 4 drives blade 3 to rotate, as shown in figure 5, the electricity
Machine connector 1 includes motor first order boss 11, motor second level boss 12 and motor third level boss 13；As shown in fig. 6, institute
It includes nacelle first order boss 51, nacelle second level concave station 52 and nacelle third level boss 53 to state nacelle connector 5；The nacelle
Second level concave station 52 is concave-convex mating structure with motor third level boss 13, and motor third level boss 13 can be in the nacelle second level
It is slided in the slideway of concave station 52, finally fits like a glove and dock with nacelle second level concave station 52；Motor second level boss 12 with
53 consistency of thickness of nacelle third level boss, nacelle third level boss 53 can play the role of limit, and motor contact 1 can only edge
A direction rotation (counterclockwise or clockwise), this direction turns to identical with motor 4.When motor 4 rotates extremely along this direction
When extreme position, the magnet on motor third level boss 13 should be in same position with the magnet on nacelle first order boss 51, lead to
It crosses magnet to attract and be fixed together, magnet locking device 8 at this time is magnet.
The material of the radome fairing 2, motor contact 1 and nacelle connector 5 be aluminium alloy, steel, polyethylene, polylactic acid,
It is one or more in UV resins, cork wood.
Motor nacelle 7 act as connecting in motor and wing structure or airframe structure, while being able to maintain that pneumatic
Shape.The radome fairing 2 wraps up motor 4 to maintain good aerodynamic configuration.
The present invention is a kind of fast disassembly type motor cabinet, and this motor cabinet realizes quickly tearing open for motor with simple mechanical structure
It dress and is securely loaded, the modular assembly of unmanned plane motor part may be implemented, save when carrying the outgoing operation of unmanned plane
Vanning space, decreases the time before unmanned machine operation.
The fast disassembly type motor cabinet is by mainly comprising the following steps：Motor contact 1, radome fairing 2, blade 3, motor
4, nacelle connector 5, locking device, motor nacelle 7 form.The nacelle connector 5 is connect with motor nacelle 7, the motor
Connector 1 is connect with motor 4, and blade 3 is equipped on the motor 4, and the locking device is used for that motor contact 1 is auxiliarily fixed
With the relative position of nacelle connector 5, the radome fairing 2 wraps up motor 4 to maintain good aerodynamic configuration.
How the connection between narration nacelle connector 5 and motor contact 1 and locking device lock in detail below.
The nacelle connector 5 and motor contact 1 are segmented into the structure being made of three-level concave and convex platform, the electricity of motor contact 1
53 thickness having the same of nacelle third level boss of machine second level boss 12 and nacelle connector 5.Wherein on nacelle connector 5
Nacelle second level concave station 52 corresponded with the motor third level boss 13 on motor contact 1, shape is complementary, and nacelle connects
The space that the nacelle second level concave station 52 of fitting 5 is vacated inside annulus, can make motor contact 1 along electrical axis side
To when being inserted into nacelle connector 5, can be relatively rotated by axis of electrical axis.Due to the 5 nacelle third level of nacelle connector
The position-limiting action of boss 53, motor contact 1 can only rotate (counterclockwise or clockwise) along a direction, this direction and motor
4 steerings are identical.When motor 4 is rotated along this direction to extreme position, the limit hole and nacelle on motor first order boss 11
Limit hole on level-one boss 51 is in concentric position, is at this time inserted into check lock lever, check lock lever plays the role of limit at this time.
(when using magnetic mode, magnet when extreme position on motor third level boss 13 should on nacelle first order boss 51
Magnet is in same position)
This design is advantageous in that, when motor 4 rotates, motor contact 1 can be driven to be limited towards nacelle connector 5
Position direction rotation, even if without locking device its in the operating condition if can make at motor contact 1 and nacelle connector 5
In a kind of state for the more turning the more tight, good fixation can be reached, but in view of there are certain vibrations in rotation process for motor 4
And its relative position may change when unmanned plane during flying attitudes vibration, therefore retaining mechanism is set in situation convenient for disassembly and assembly
Under auxiliary stopper is carried out to it.
The locking device can be mechanical interlocking 6, also can lock 8 by magnetic.
The motor contact 1 can connect for screw with the connection type of radome fairing 2, be cementing.
The motor contact 1 is connected by screw with motor 4.
The nacelle connector 5 can be connect and be glued for screw with the connection type of motor nacelle 7.
The material of the radome fairing 2, motor contact 1 and nacelle connector 5 can be aluminium alloy, steel, polyethylene, poly- breast
Acid, UV resins, cork wood etc..
In conclusion a kind of fast disassembly type motor cabinet proposed by the present invention, this motor cabinet are realized with simple mechanical structure
It the fast assembling-disassembling of motor and is securely loaded, the modular assembly of unmanned plane motor part may be implemented, saves and carry nobody
Machine go out operation when vanning space, decrease the time before unmanned machine operation.
Above embodiment is the preferred embodiment of the present invention, is not intended to limit the patent protection model of the present invention
It encloses.Those skilled in the art belonging to any present invention, in the premise for not departing from spirit and scope disclosed in this invention
Under, the transformation of the equivalent structure and equivalent steps that done to present disclosure each falls within claimed the scope of the claims
Within.
Claims (7)
1. a kind of fast disassembly type motor cabinet, which is characterized in that including：Motor contact (1), radome fairing (2), blade (3), motor
(4), nacelle connector (5) and motor nacelle (7)；
The motor contact (1) is fixedly connected with motor (4), and the motor contact (1) is fixedly connected with radome fairing (2),
The nacelle connector (5) is fixedly connected with motor nacelle (7)；
The blade (3) is mounted on motor (4)；
The motor contact (1) includes that motor first order boss (11), motor second level boss (12) and the motor third level are convex
Platform (13)；
The nacelle connector (5) includes that nacelle first order boss (51), nacelle second level concave station (52) and the nacelle third level are convex
Platform (53)；
Nacelle second level concave station (52) is concave-convex mating structure with motor third level boss (13)；
Motor second level boss (12) and nacelle third level boss (53) consistency of thickness.
2. a kind of fast disassembly type motor cabinet according to claim 1, which is characterized in that further include locking device.
3. a kind of fast disassembly type motor cabinet according to claim 2, which is characterized in that the locking device includes mechanical interlocking
Device (6) and magnet locking device (8).
4. a kind of fast disassembly type motor cabinet according to claim 1, which is characterized in that the motor contact (1) and motor
(4) connection type connects for screw.
5. a kind of fast disassembly type motor cabinet according to claim 1, which is characterized in that the motor contact (1) and rectification
The connection type for covering (2) is screw connection or cementing.
6. a kind of fast disassembly type motor cabinet according to claim 1, which is characterized in that the nacelle connector (5) and motor
The connection type of nacelle (7) is screw connection or cementing.
7. a kind of fast disassembly type motor cabinet according to claim 1, which is characterized in that the radome fairing (2), motor contact
(1) and the material of nacelle connector (5) is one or more in aluminium alloy, steel, polyethylene, polylactic acid, UV resins, cork wood.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810278378.6A CN108327914A (en) | 2018-03-31 | 2018-03-31 | A kind of fast disassembly type motor cabinet |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810278378.6A CN108327914A (en) | 2018-03-31 | 2018-03-31 | A kind of fast disassembly type motor cabinet |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108327914A true CN108327914A (en) | 2018-07-27 |
Family
ID=62931946
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810278378.6A Pending CN108327914A (en) | 2018-03-31 | 2018-03-31 | A kind of fast disassembly type motor cabinet |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108327914A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109353512A (en) * | 2018-11-20 | 2019-02-19 | 飞智控（天津）科技有限公司 | Space-saving type logistics unmanned plane horn |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2772342A1 (en) * | 1997-12-16 | 1999-06-18 | Aerospatiale | PROPELLER ASSEMBLY WITH BLOWER HOODS PROVIDED WITH HOLDING AND POSITIONING SAFETY DEVICES, FOR AIRCRAFT |
| CN101784444A (en) * | 2007-08-20 | 2010-07-21 | 埃尔塞乐公司 | Jet engine nacelle equipped with a system for mechanically inhibiting a thrust reverser |
| CN106005453A (en) * | 2016-06-17 | 2016-10-12 | 长光卫星技术有限公司 | Unmanned aerial vehicle nacelle retracting mechanism and assembly method |
| CN106379544A (en) * | 2016-11-29 | 2017-02-08 | 北京奇正数元科技股份有限公司 | Modularized and detachable type power nacelle of unmanned aerial vehicle |
| CN208683114U (en) * | 2018-03-31 | 2019-04-02 | 灵翼飞航（天津）科技有限公司 | A kind of fast disassembly type motor cabinet |
-
2018
- 2018-03-31 CN CN201810278378.6A patent/CN108327914A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2772342A1 (en) * | 1997-12-16 | 1999-06-18 | Aerospatiale | PROPELLER ASSEMBLY WITH BLOWER HOODS PROVIDED WITH HOLDING AND POSITIONING SAFETY DEVICES, FOR AIRCRAFT |
| CN101784444A (en) * | 2007-08-20 | 2010-07-21 | 埃尔塞乐公司 | Jet engine nacelle equipped with a system for mechanically inhibiting a thrust reverser |
| CN106005453A (en) * | 2016-06-17 | 2016-10-12 | 长光卫星技术有限公司 | Unmanned aerial vehicle nacelle retracting mechanism and assembly method |
| CN106379544A (en) * | 2016-11-29 | 2017-02-08 | 北京奇正数元科技股份有限公司 | Modularized and detachable type power nacelle of unmanned aerial vehicle |
| CN208683114U (en) * | 2018-03-31 | 2019-04-02 | 灵翼飞航（天津）科技有限公司 | A kind of fast disassembly type motor cabinet |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109353512A (en) * | 2018-11-20 | 2019-02-19 | 飞智控（天津）科技有限公司 | Space-saving type logistics unmanned plane horn |
| CN109353512B (en) * | 2018-11-20 | 2024-09-06 | 一飞智控(天津)科技有限公司 | Space saving type logistics unmanned aerial vehicle arm |
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