CN108639308A - A kind of wing mechanism for assembling-disassembling for Fixed Wing AirVehicle - Google Patents
A kind of wing mechanism for assembling-disassembling for Fixed Wing AirVehicle Download PDFInfo
- Publication number
- CN108639308A CN108639308A CN201810449584.9A CN201810449584A CN108639308A CN 108639308 A CN108639308 A CN 108639308A CN 201810449584 A CN201810449584 A CN 201810449584A CN 108639308 A CN108639308 A CN 108639308A
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- China
- Prior art keywords
- push rod
- block
- disassembling
- assembling
- wing
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- 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.)
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/26—Attaching the wing or tail units or stabilising surfaces
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Automatic Assembly (AREA)
Abstract
The invention discloses a kind of wing mechanism for assembling-disassembling for Fixed Wing AirVehicle, including handle, push rod, mounting blocks, block, spring, baffle ring；The handle is connected to the rear end of push rod；Mounting hole is equipped in the mounting blocks；The push rod passes through the mounting hole of mounting blocks, and push rod front end is connected with block；The push rod is equipped with card slot；The baffle ring is arranged on card slot；The spring pocket is located on push rod in mounting hole；Spring one end is limited by mounting hole bottom, and the other end is limited by baffle ring；The spring has push rod motive force backward so that block rear end is bonded with mounting blocks front end；The wing mechanism for assembling-disassembling of the present invention, need not additionally increase the dismounting that wing can be completed in tool, simple in structure, easy to operate, can realize fast assembling-disassembling.
Description
Technical field
The invention belongs to vehicle technology field, especially a kind of wing mechanism for assembling-disassembling for Fixed Wing AirVehicle.
Background technology
Unmanned plane has important due to the advantages that its is small, cost-effective, fight survival ability is strong in Future Air Combat
Effect.It is widely used with fixed-wing unmanned plane, traditional dismounting mode relies on before the cumbersome disadvantage of tool, assembly makes flight
Prepare and follow-up maintenance work is extremely complex.It voluntarily replaces, repair for ease of user, numerous manufacturers will be quick without tool
Dismounting design is introduced into aircraft platforms design.But quick-disassembly structure realization method is complicated in the prior art, in order to realize Quick Release
Demand often sacrifices the bonding strength between component, cannot achieve the connection of high intensity, is easily damaged in use.
Invention content
Technical problem solved by the invention is to provide one kind, to solve the problems, such as that wing dismounting is complicated.
Realize that the technical solution of the object of the invention is：
A kind of wing mechanism for assembling-disassembling for Fixed Wing AirVehicle, including handle, push rod, mounting blocks, block, spring, gear
Circle；
The handle is connected to the rear end of push rod；Mounting hole is equipped in the mounting blocks；The push rod passes through mounting blocks
Mounting hole, push rod front end are connected with block；The push rod is equipped with card slot；The baffle ring is arranged on card slot；The spring pocket
On push rod, and in mounting hole；Spring one end is limited by mounting hole bottom, and the other end is limited by baffle ring；Institute
Spring is stated to push rod with motive force backward so that block rear end is bonded with mounting blocks front end.
Compared with prior art, the present invention its remarkable advantage：
(1) wing mechanism for assembling-disassembling of the invention need not additionally increase the dismounting that wing can be completed in tool, structure letter
It is single, it is easy to operate, it can realize fast assembling-disassembling.
(2) wing mechanism for assembling-disassembling of the invention, fixed block rear end are equipped with baffle, need not be incited somebody to action by fasteners such as bolt etc.
Fixed block is fixed with the mounting groove on sleeve, time saving and energy saving.
(3) mounting blocks front end is equipped with cross recess, block rear end is equipped with flat recess, is effectively limited, accurate positioning, together
When under the action of the spring, ensure that the effective of block and mounting blocks locks,
(4) handle is connected with push rod using shaft, and handle can be freely sagging after rotation, reduces the occupied space of handle.
Present invention is further described in detail below in conjunction with the accompanying drawings.
Description of the drawings
Fig. 1 is the overall explosive view of the wing mechanism for assembling-disassembling for Fixed Wing AirVehicle.
Fig. 2 is wing scheme of installation.
Fig. 3 is the specific scheme of installation that wing inserts the wing.
Fig. 4 (a-c) is the mechanism for assembling-disassembling fundamental diagram of the present invention
Specific implementation mode
In order to illustrate technical scheme of the present invention and technical purpose, below in conjunction with the accompanying drawings and specific embodiment is the present invention
It is further to introduce.
In conjunction with Fig. 1, a kind of wing mechanism for assembling-disassembling for Fixed Wing AirVehicle of the invention, including handle 1, push rod 2, peace
Fill block 3, block 4, spring 6, baffle ring 7；
The handle 1 is connected to the rear end of push rod 2；Mounting hole 31 is equipped among the mounting blocks 3；The push rod 2 passes through
The mounting hole 31 of mounting blocks 3,2 front end of push rod are connected with block 4；The push rod 2 is equipped with card slot 21；The setting of the baffle ring 7 exists
On card slot 21；The spring 6 is sleeved on push rod 2, and in mounting hole 31；6 one end of spring is limited by 31 bottom of mounting hole,
The other end is limited by baffle ring 7；The spring 7 has push rod 2 motive force backward so that 4 rear end of block and installation
3 front end of block is bonded.
Preferably, it is rectangular rectangular block, the cross sectional dimensions of block 4 that the mounting blocks 3, block 4, which are cross section,
It is less than or identical as 3 cross sectional dimensions of mounting blocks.
Further, 3 front end of the mounting blocks is equipped with cross recess；4 rear end of the block is equipped with a word protrusion 41, a word
Raised 41 length directions are consistent with 4 width direction of block；Reset condition, it is recessed that a word protrusion 41 of block 4 is caught in 3 cross of mounting blocks
In the transverse concave groove 33 of slot；After push rod 2 rotates 90 °, the longitudinal direction that a word protrusion 41 of block 4 is caught in 3 cross recess of mounting blocks is recessed
In slot 34.
Further, the handle 1 is connected to 2 rear end of push rod by shaft 5.
Further, the length direction of the transverse concave groove 33 for being axially parallel to cross recess of the shaft 5,2 turns of push rod
After 90 ° dynamic, the length direction of the longitudinal fluting 34 for being axially parallel to cross recess of shaft 5 so that handle 1 can freely be fallen downwards
Under, reduce 1 occupied space of handle.
Further, 3 rear end of the mounting blocks is additionally provided with baffle 32, is limited to the installation site of mounting blocks 3.
In use, first the slotting wing 91 of wing 9 is inserted into fuselage slot 10, as shown in Fig. 2, being specially to insert the wing 91 to be inserted into cabin
In slot between plate 11 and casing 8, as shown in Figure 3；It is equipped with the mounting groove 81 of mounting blocks 3 on wing 91 and casing 8, installs
81 size of slot is slightly larger than 4 cross sectional dimensions of block so that when rotating push-rod 2, mounting blocks 3 will not rotate together；Then this is sent out
The mounting blocks 3 of bright mechanism for assembling-disassembling 100 are inserted into mounting groove 81, push handle 1 that push rod 2 (such as Fig. 4 (a)), spring 6 is pushed to be pressurized
The word protrusion 41 of contracting, block 4 is detached with the transverse concave groove 33 of 3 cross recess of mounting blocks；Rotating handles 90 ° (such as Fig. 4 (b)),
Block 4 follows push rod 2 to rotate together, and 4 length direction of block is vertical with 81 width direction of mounting groove at this time；After unclamping handle 1, bullet
Spring 6 pushes push rod 2 to move backward, and block 4 moves backward with push rod 2, and the word protrusion 41 of block 4 is located in mounting groove 81, and
It is caught in the longitudinal fluting 34 of 3 cross recess of mounting blocks (such as Fig. 4 (c))；Push rod 2 is avoided to be freely rotated；In block 4 and baffle 32
Common position-limiting action under, the slotting wing 91 of wing 9 is fixed with casing 8, handle 1 is freely sagging at this time.When dismantling wing 9, push away
Dynamic push rod 2 reversely rotates 90 °, and mechanism for assembling-disassembling 100 is taken out from mounting groove 8, the slotting wing is detached with 91 casings 8, removes wing 9
.
The wing mechanism for assembling-disassembling of the present invention, need not additionally increase the dismounting that wing can be completed in tool, simple in structure, behaviour
Facilitate, can realize fast assembling-disassembling.
Claims (6)
1. a kind of wing mechanism for assembling-disassembling for Fixed Wing AirVehicle, which is characterized in that including handle (1), push rod (2), installation
Block (3), block (4), spring (6), baffle ring (7)；
The handle (1) is connected to the rear end of push rod (2)；The mounting blocks (3) are equipped with mounting hole (31)；The push rod (2) is worn
The mounting hole (31) of mounting blocks (3) is crossed, push rod front end is connected with block (4)；The push rod (2) is equipped with card slot (21)；It is described
Baffle ring (7) is arranged on card slot (21)；The spring (6) is sleeved on push rod (2), and in mounting hole (31)；Spring (6) one
End is limited by mounting hole (31) bottom, and the other end is limited by baffle ring (7)；The spring (7) to push rod (2) have to
Motive force afterwards so that block (4) rear end is bonded with mounting blocks (3) front end.
2. a kind of wing mechanism for assembling-disassembling for Fixed Wing AirVehicle according to claim 1, which is characterized in that the peace
Dress block (3), block (4) are that cross section is rectangular rectangular block.
3. a kind of wing mechanism for assembling-disassembling for Fixed Wing AirVehicle according to claim 1 or 2, which is characterized in that institute
It states mounting blocks (3) front end and is equipped with cross recess；Block (4) rear end is equipped with word protrusion (41), word protrusion (41) length
Direction is consistent with block (4) width direction；A word raised (41) for reset condition, block (4) is caught in mounting blocks (3) cross recess
Transverse concave groove (33) in；After push rod (2) rotates 90 °, a word raised (41) for block (4) is caught in mounting blocks (3) cross recess
Longitudinal fluting (34) in.
4. a kind of wing mechanism for assembling-disassembling for Fixed Wing AirVehicle according to claim 1, which is characterized in that described
Hand (1) is connected to push rod (2) rear end by shaft (5).
5. a kind of wing mechanism for assembling-disassembling for Fixed Wing AirVehicle according to claim 4, which is characterized in that described turn
The length direction of the transverse concave groove (33) for being axially parallel to cross recess of axis (5).
6. a kind of wing mechanism for assembling-disassembling for Fixed Wing AirVehicle according to claim 1, which is characterized in that the peace
Dress block (3) rear end is additionally provided with baffle (32).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810449584.9A CN108639308A (en) | 2018-05-11 | 2018-05-11 | A kind of wing mechanism for assembling-disassembling for Fixed Wing AirVehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810449584.9A CN108639308A (en) | 2018-05-11 | 2018-05-11 | A kind of wing mechanism for assembling-disassembling for Fixed Wing AirVehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108639308A true CN108639308A (en) | 2018-10-12 |
Family
ID=63754695
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810449584.9A Pending CN108639308A (en) | 2018-05-11 | 2018-05-11 | A kind of wing mechanism for assembling-disassembling for Fixed Wing AirVehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108639308A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109572991A (en) * | 2018-12-28 | 2019-04-05 | 深圳市道通智能航空技术有限公司 | A kind of unmanned vehicle and its wing components |
| CN112278240A (en) * | 2020-11-06 | 2021-01-29 | 湖南浩天翼航空技术有限公司 | Small-sized fixed wing unmanned aerial vehicle empennage quick dismounting mechanism and using method thereof |
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| EP0733761A2 (en) * | 1995-03-22 | 1996-09-25 | Pax GmbH | Wing frame |
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| CN205381306U (en) * | 2015-12-28 | 2016-07-13 | 全兴精工集团有限公司 | Electronic power -assisted steering pump of pure [electric] motor coach of new forms of energy |
| CN206528612U (en) * | 2017-01-20 | 2017-09-29 | 天津腾云智航科技有限公司 | A kind of fixed-wing unmanned plane buckle locking mechanism |
| CN107651162A (en) * | 2017-09-27 | 2018-02-02 | 西安冰果智能航空科技有限公司 | A kind of unmanned plane wing quick assembling mechanism |
| CN207157486U (en) * | 2017-08-05 | 2018-03-30 | 北京海利天梦科技有限公司 | Unmanned plane wing rapid dismounting apparatus |
| CN208377045U (en) * | 2018-05-11 | 2019-01-15 | 南京航天猎鹰飞行器技术有限公司 | A kind of wing mechanism for assembling-disassembling for Fixed Wing AirVehicle |
-
2018
- 2018-05-11 CN CN201810449584.9A patent/CN108639308A/en active Pending
Patent Citations (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB943826A (en) * | 1961-10-06 | 1963-12-04 | Koppers Gmbh Heinrich | Arrangements for introducing thermocouples and like devices into pressurised reaction chambers |
| EP0733761A2 (en) * | 1995-03-22 | 1996-09-25 | Pax GmbH | Wing frame |
| EP1249570A1 (en) * | 2001-04-12 | 2002-10-16 | bulthaup GmbH & Co. KG | Closure device |
| CN102348861A (en) * | 2009-03-11 | 2012-02-08 | 布尔加建筑业和贸易有限公司 | Lockable handle/grip system with coupling for sliding windows |
| CN102060100A (en) * | 2010-12-14 | 2011-05-18 | 上海智晟航空科技有限公司 | Aircraft fuselage-wing connecting mechanism |
| CN203623960U (en) * | 2013-12-20 | 2014-06-04 | 海鹰航空通用装备有限责任公司 | Device for connecting wings and body of small-and-medium-sized fixed-wing unmanned aerial vehicle |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109572991A (en) * | 2018-12-28 | 2019-04-05 | 深圳市道通智能航空技术有限公司 | A kind of unmanned vehicle and its wing components |
| WO2020134235A1 (en) * | 2018-12-28 | 2020-07-02 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle and wing assembly thereof |
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| CN112278240A (en) * | 2020-11-06 | 2021-01-29 | 湖南浩天翼航空技术有限公司 | Small-sized fixed wing unmanned aerial vehicle empennage quick dismounting mechanism and using method thereof |
| CN112278240B (en) * | 2020-11-06 | 2021-12-28 | 湖南浩天翼航空技术有限公司 | Small-sized fixed wing unmanned aerial vehicle empennage quick dismounting mechanism and using method thereof |
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