CN207157486U - Unmanned plane wing rapid dismounting apparatus - Google Patents
Unmanned plane wing rapid dismounting apparatus Download PDFInfo
- Publication number
- CN207157486U CN207157486U CN201720976278.1U CN201720976278U CN207157486U CN 207157486 U CN207157486 U CN 207157486U CN 201720976278 U CN201720976278 U CN 201720976278U CN 207157486 U CN207157486 U CN 207157486U
- Authority
- CN
- China
- Prior art keywords
- wing
- hole
- sliding pin
- unmanned plane
- lock
- 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.)
- Active
Links
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
A kind of unmanned plane wing rapid dismounting apparatus, including fuselage and wing, also include being used for the rapid dismounting apparatus for dismounting wing, the rapid dismounting apparatus includes lock sliding pin, the lock frame being slidably connected with lock sliding pin, with the buckle in lock the sliding pin setting and wing that are used cooperatively and being arranged on lock sliding pin bottom and latching the spring between frame, the wing fixed seat for fixing wing is provided with the fuselage, it is provided with the wing fixed seat for accommodating and fixing the pit of lock sliding pin, the lock sliding pin top is provided with button, interconnected first through hole and the second through hole are provided with the lock sliding pin, the buckle is used cooperatively with first through hole and the second through hole.The unmanned plane wing rapid dismounting apparatus can complete the dismounting or installation of wing by pressing button, and simple to operate, practicality is high.
Description
Technical field
This is related to a kind of rapid dismounting apparatus using new, more particularly to a kind of unmanned plane wing rapid dismounting apparatus.
Background technology
Unmanned plane field in China's is quickly grown in recent years, and the unmanned plane yield in China occupies first place in the world.Existing part nobody
The fuselage and airfoil member of machine take big quantity space still by the way of being fixedly connected during packaging, transport and collection,
And it is easily damaged, transport is got up very inconvenient.Some unmanned planes use insertion airfoil, i.e. wing is installed to pluggablely
On fuselage, and it is screwed, but the position of screw is more hidden, is not easy to dismount.Unmanned plane wing and fuselage also
Connected mode adopt be screwed, mode these fixed form reliabilities that rubber band is fixed it is bad, damage easy to aging, dismounting
It is cumbersome, part is more, thereby result in relatively low in outer operating efficiency.
Authorization Notice No. is that CN205854479 U Chinese patent discloses a kind of unmanned plane wing device for quickly disassembling, including
Wing and fuselage, are fixed with wing anterior cannula, wing rear sleeve and wing tubular girder on wing, described wing anterior cannula,
Wing rear sleeve and wing tubular girder are inserted in set hole corresponding to fuselage respectively, are also passed through between described wing and fuselage
Clamp button of the spring mechanism is connected.Although what this device for quickly disassembling can be quickly is arranged on wing on fuselage, requiring
When wing is stably connected with into upper, clamp button of the spring needs enough stiffness factors, but just needs very big power just in dismounting
Wing can be disassembled, using simultaneously inconvenient.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane wing rapid dismounting apparatus, and its advantage is can to reduce nobody
The space that machine takes during packaging, transport and collection, and can single-handedly be completed when dismounting wing, disassembly process is simple
It is convenient.
Above-mentioned technical purpose of the present utility model technical scheme is that：
A kind of unmanned plane wing rapid dismounting apparatus, including fuselage and wing, and for dismounting the fast assembling-disassembling of wing
Device, the rapid dismounting apparatus include lock sliding pin, the lock frame being slidably connected with lock sliding pin, made with lock sliding pin cooperation
Buckle and it is arranged on lock sliding pin bottom and latches the spring between frame, is provided with for fixing wing on the fuselage
Wing fixed seat, it is provided with the wing fixed seat for accommodating and the pit of fixed lock sliding pin, the lock sliding pin top
End is provided with button, and interconnected first through hole and the second through hole are provided with the lock sliding pin, and the buckle and first are led to
Hole and the second through hole are used cooperatively, and buckle is arranged on wing.
Pass through above-mentioned technical proposal, latch on the buckle insertion fuselage on wing and can be achieved in the second through hole on sliding pin
Fixation to wing, the i.e. removable assembly and disassembly of button is pressed, very simply, convenient, fast.And it is provided with and is used on fuselage
The pit of lock sliding pin is accommodated, space can be saved.
The utility model is further arranged to：Described wing fixed seat one end is fixedly installed guide rod, is provided with wing
The pilot tunnel being used cooperatively with guide rod.
Pass through above-mentioned technical proposal, guide rod stretches out in pilot tunnel the fixation that can be realized to wing, and guide rod can be to machine
The wing is played a supporting role, and makes wing more stable.
The utility model is further arranged to：The diameter of second through hole is slightly larger than the diameter on buckle head.
Pass through above-mentioned technical proposal, the second through-hole diameter, which is more than buckle head diameter, can facilitate buckle to insert buckle sliding pin
It is interior.
The utility model is further arranged to：Buckle head maximum gauge is more than first through hole diameter.
Pass through above-mentioned technical proposal, first through hole are used to that buckle can be connect, and first through hole diameter, which is less than buckle head, can make card
Button and first through hole clamping.
The utility model is further arranged to：The lock frame bottom is provided with for pacifying spring-loaded boss.
Pass through above-mentioned technical proposal, boss can play fixation to spring, prevent spring from being come off from lock frame.
The utility model is further arranged to：The lock frame top is provided with the breach for wearing button, described recessed
The groove for accommodating button is provided with the correspondence position of hole.
Pass through above-mentioned technical proposal, the breach on lock frame top can be such that button is slided up and down on lock frame, on pit
Groove play a part of accommodate button so that lock sliding pin insertion groove in when button can normally slide.
The utility model is further arranged to：The both sides of the lock frame are bonded with cover plate.
Pass through above-mentioned technical proposal, cover plate can play protection and fixation to lock sliding pin, prevent from latching in sliding pin
Portion's part is rocked, and cover plate is Nian Jie with fuselage, and lock sliding pin can be fixed on fuselage.
The utility model is further arranged to：Third through-hole is provided with the cover plate, third through-hole diameter and second are led to
Bore dia is identical.
Pass through above-mentioned technical proposal, third through-hole diameter is identical with the second through hole, can make buckle through cover plate insertion lock
Detain in sliding pin, cover plate is not influenceed the normal use of device for quickly disassembling while fixed lock sliding pin.
In summary, the utility model has the advantages that：
One：The wing rapid dismounting apparatus latches sliding pin by buckle clamping and wing is fixed, and buckle sliding pin
Top is provided with button, by pressing button wing can be controlled to dismantle or install, simple to operate quick, and can subtract
The space that small unmanned plane takes during packaging, transport and collection.
Two：Due to being additionally provided with guide rod on fuselage, the pilot tunnel coordinated with it is provided with wing, guide rod and pilot tunnel are arranged on
Wing rapid dismounting apparatus opposite side, can play a supporting role to wing, make wing structure more stable, and guide rod is with leading
The direct grafting in hole, convenient dismounting.
Brief description of the drawings
Fig. 1 is unmanned plane wing junction structural representation；
Fig. 2 is Fig. 1 A portions enlarged diagram；
Fig. 3 is the explosive view of rapid dismounting apparatus；
Fig. 4 is the front view of lock sliding pin.
In figure, 1, unmanned plane；11st, fuselage；111st, wing fixed seat；1111st, guide rod；1112nd, groove；1113rd, pit；
12nd, wing；2nd, rapid dismounting apparatus；21st, sliding pin is latched；211st, button；212nd, latch；2121st, first through hole；2122nd, second
Through hole；2123rd, first boss；22nd, frame is latched；221st, breach；222nd, second boss；23rd, spring；24th, cover plate；241st, threeway
Hole；25th, buckle.
Embodiment
A kind of unmanned plane wing rapid dismounting apparatus, it is shown referring to Figures 1 and 2, including unmanned plane 1, fuselage 11, wing 12
And for dismounting the rapid dismounting apparatus 2 of wing 12.
Wing fixed seat 111 is provided with fuselage 11, the one end of wing fixed seat 111 is fixedly installed guide rod 1111, wing
12 offer pilot tunnel, and the pilot tunnel on wing 12 is arranged in by guide rod 1111, wing 12 can be connected on fuselage 11, led simultaneously
Bar 1111 also has supporting role to wing 12.Pit 1113 is additionally provided with the free end of wing fixed seat 111, above-mentioned is quick
Attaching/detaching apparatus 2 is fixedly installed in pit 1113.
Shown in reference picture 3 and Fig. 4, rapid dismounting apparatus 2 includes lock sliding pin 21, lock frame 22, buckle 25 and installation
In the lock bottom of sliding pin 21 and the spring 23 between frame 22 is latched, lock sliding pin 21 includes button 211, and one end of button 211 is worn
Cross the groove 1112 being arranged in wing fixed seat 111, and protrude the upper surface of wing fixed seat 111, button 211 it is another
End has been wholely set lock 212, and the through hole 2122 of first through hole 2121 and second is provided with lock 212, first through hole 2121 with
Second through hole 2122 connects, and first through hole 2121 connects in semicircle and rectangle combined shaped, rectangle one end with the second through hole 2122,
Afterbody of half circular diameter slightly larger than buckle 25 but the maximum gauge less than the head of buckle 25, to ensure buckle 25 can be stuck in into lock
The inner side of sliding pin 21 is detained, the diameter of the second through hole 2122 is slightly larger than the maximum gauge on the head of buckle 25, to facilitate buckle 25 to pass through,
The bottom of lock sliding pin 21 is provided with the boss 2123 for installing spring 23.Lock sliding pin 21 periphery is provided with lock frame 22,
Jagged 221 are opened up so that button 211 passes through on lock frame 22, are provided with the inside of lock frame bottom for installing spring 23
Boss 222, lock frame 22 play support guide effect to lock sliding pin 21.Cover plate 24 is bonded with the both sides of lock frame 221, is covered
Third through-hole 241 is provided with plate 24, the diameter of third through-hole 241 is identical with the diameter of the second through hole 2122, when pressing button 211
When, the axis of third through-hole 241 overlaps with the axis of the second through hole 2122.Wing quick-release arrangement 2 is embedded in wing fixed seat
In pit 1113 on 111, and it is be bonded with wing fixed seat 111, and one end of button 211, which passes through, is arranged on wing fixed seat
Groove 1112 on 111, and protrude the upper surface of wing fixed seat 111.Buckle 25 is threaded on wing 12, buckle 25
Overall " T " shape, the afterbody of buckle 25 is provided with screw thread, and head design is into arc dome-shaped, to facilitate insertion lock sliding pin 21.
When needing wing 12 being arranged on fuselage 11, the guide rod 1111 in wing fixed seat 111 is inserted into wing 12
On pilot tunnel, then push wing 12 to wing fixed seat 111 along guide rod 1111, when wing 12 is close to wing fixed seat 111,
Button 211 is pressed, the buckle 25 allowed on wing 12 inserts lock sliding pin 21, release button 211, allows lock sliding pin 21 to exist
Reset in the presence of spring 23, so wing 12 is fixed on fuselage 11 by wing rapid dismounting apparatus 2.Needing machine
When the wing 12 is pulled down from fuselage 11, button 211 is pressed, wing 12 is outwards extracted along guide rod 1111.
The unmanned plane wing rapid dismounting apparatus can control wing to dismantle or install, side simple to operate by pressing button
Just it is quick, and the space that unmanned plane takes during packaging, transport and collection can be reduced, there is very high practicality.
This specific embodiment is only that it is not to limitation of the present utility model, ability to explanation of the present utility model
Field technique personnel can make the modification of no creative contribution to the present embodiment as needed after this specification is read, but
As long as all protected in right of the present utility model by Patent Law.
Claims (8)
1. a kind of unmanned plane wing rapid dismounting apparatus, including fuselage (11) and wing (12), it is characterized in that：Also include being used for tearing open
The rapid dismounting apparatus (2) of the installation wing (12), the rapid dismounting apparatus (2) include lock sliding pin (21), with latching sliding pin
(21) the lock frame being slidably connected（22）And lock sliding pin (21) is used cooperatively and is arranged on wing（12）On buckle (25) with
And it is arranged on lock sliding pin (21) bottom and lock frame（22）Between spring (23), be provided with the fuselage (11) for solid
Determine the wing fixed seat (111) of wing (12), be provided with the wing fixed seat (111) for accommodating and fixing lock sliding pin
(21) pit (1113), described lock sliding pin (21) top are provided with button (211), phase are provided with the lock sliding pin (21)
Intercommunicated first through hole (2121) and the second through hole (2122), the buckle (25) and first through hole (2121) and the second through hole
(2122) it is used cooperatively.
2. a kind of unmanned plane wing rapid dismounting apparatus according to claim 1, it is characterized in that：The wing fixed seat
(111) one end is fixedly installed guide rod (1111), and the pilot tunnel being used cooperatively with guide rod (1111) is provided with wing (12).
3. a kind of unmanned plane wing rapid dismounting apparatus according to claim 1, it is characterized in that：Second through hole
(2122) diameter is more than the diameter on buckle (25) head.
4. a kind of unmanned plane wing rapid dismounting apparatus according to claim 1, it is characterized in that：Buckle (25) head
Maximum gauge is more than first through hole (2121) diameter.
5. a kind of unmanned plane wing rapid dismounting apparatus according to claim 1, it is characterized in that：The lock frame（22）Bottom
End is provided with the boss for installing spring (23).
6. a kind of unmanned plane wing rapid dismounting apparatus according to claim 1, it is characterized in that：The lock frame（22）Top
End is provided with for wearing the breach (221) of button (211), be provided with pit (1113) correspondence position for accommodate by
The groove (1112) of button (211).
7. a kind of unmanned plane wing rapid dismounting apparatus according to claim 1, it is characterized in that：It is described to latch frame（22）
Both sides be bonded with cover plate (24).
8. a kind of unmanned plane wing rapid dismounting apparatus according to claim 7, it is characterized in that：Set on the cover plate (24)
Third through-hole (241) is equipped with, third through-hole (241) diameter is identical with the second through hole (2122) diameter.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720976278.1U CN207157486U (en) | 2017-08-05 | 2017-08-05 | Unmanned plane wing rapid dismounting apparatus |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720976278.1U CN207157486U (en) | 2017-08-05 | 2017-08-05 | Unmanned plane wing rapid dismounting apparatus |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207157486U true CN207157486U (en) | 2018-03-30 |
Family
ID=61716144
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720976278.1U Active CN207157486U (en) | 2017-08-05 | 2017-08-05 | Unmanned plane wing rapid dismounting apparatus |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207157486U (en) |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108639308A (en) * | 2018-05-11 | 2018-10-12 | 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 |
| CN109927878A (en) * | 2019-04-25 | 2019-06-25 | 西安航空学院 | Diamond wing mounting structure and aircraft with the mounting structure |
| CN110466750A (en) * | 2019-08-19 | 2019-11-19 | 西北工业大学 | A kind of Portable vertical landing scouting monitoring unmanned plane |
| WO2021078162A1 (en) * | 2019-10-21 | 2021-04-29 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle |
| CN114013625A (en) * | 2021-11-17 | 2022-02-08 | 中山福昆航空科技有限公司 | Can dismantle fixed wing unmanned aerial vehicle |
| CN114379765A (en) * | 2021-12-30 | 2022-04-22 | 中电科芜湖通用航空产业技术研究院有限公司 | Unmanned aerial vehicle's front wing and unmanned aerial vehicle |
| EP4253227A1 (en) * | 2022-03-28 | 2023-10-04 | Shanghai Autoflight Co., Ltd. | Quick-release wing structure and an unmanned aerial vehicle using the same |
| KR20230139100A (en) * | 2022-03-25 | 2023-10-05 | 주식회사 억세스위 | One touch type assembly for easier attaching and detaching of drone's fixed wings |
| CN114013625B (en) * | 2021-11-17 | 2024-05-31 | 中山福昆航空科技有限公司 | Can dismantle fixed wing unmanned aerial vehicle |
-
2017
- 2017-08-05 CN CN201720976278.1U patent/CN207157486U/en active Active
Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108639308A (en) * | 2018-05-11 | 2018-10-12 | 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 |
| CN109927878A (en) * | 2019-04-25 | 2019-06-25 | 西安航空学院 | Diamond wing mounting structure and aircraft with the mounting structure |
| CN109927878B (en) * | 2019-04-25 | 2024-02-02 | 西安航空学院 | Diamond wing mounting structure and aircraft with same |
| CN110466750A (en) * | 2019-08-19 | 2019-11-19 | 西北工业大学 | A kind of Portable vertical landing scouting monitoring unmanned plane |
| EP4046906A4 (en) * | 2019-10-21 | 2022-11-30 | Autel Robotics Co., Ltd. | Unmanned aerial vehicle |
| WO2021078162A1 (en) * | 2019-10-21 | 2021-04-29 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle |
| US11999465B2 (en) | 2019-10-21 | 2024-06-04 | Autel Robotics Co., Ltd. | Unmanned aerial vehicle |
| CN114013625A (en) * | 2021-11-17 | 2022-02-08 | 中山福昆航空科技有限公司 | Can dismantle fixed wing unmanned aerial vehicle |
| WO2023087602A1 (en) * | 2021-11-17 | 2023-05-25 | 中山福昆航空科技有限公司 | Detachable fixed-wing unmanned aerial vehicle |
| CN114013625B (en) * | 2021-11-17 | 2024-05-31 | 中山福昆航空科技有限公司 | Can dismantle fixed wing unmanned aerial vehicle |
| CN114379765A (en) * | 2021-12-30 | 2022-04-22 | 中电科芜湖通用航空产业技术研究院有限公司 | Unmanned aerial vehicle's front wing and unmanned aerial vehicle |
| KR20230139100A (en) * | 2022-03-25 | 2023-10-05 | 주식회사 억세스위 | One touch type assembly for easier attaching and detaching of drone's fixed wings |
| KR102654386B1 (en) | 2022-03-25 | 2024-04-04 | 주식회사 억세스위 | One touch type assembly for easier attaching and detaching of drone's fixed wings |
| EP4253227A1 (en) * | 2022-03-28 | 2023-10-04 | Shanghai Autoflight Co., Ltd. | Quick-release wing structure and an unmanned aerial vehicle using the same |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN207157486U (en) | Unmanned plane wing rapid dismounting apparatus | |
| CN202434141U (en) | Connecting and fixing structure for connecting box body and back frame of light-emitting diode (LED) display screen | |
| CN204347715U (en) | The quickly dismantled computer housing of case lid | |
| CN202486146U (en) | Bidirectional clamping structure and blood-gas analyzer | |
| CN205374971U (en) | Novel projection curtain | |
| CN209402092U (en) | A kind of new automobile wiring harness fastener | |
| CN208538055U (en) | A kind of quickly assembled and disassembled dust-proof screen component and projection device | |
| CN108058807B (en) | A kind of unmanned plane Quick Release horizontal tail bindiny mechanism | |
| CN209793617U (en) | Gearbox bearing dismounting device | |
| CN202514768U (en) | Rib and umbrella disk structure of beach umbrella | |
| CN203228510U (en) | Printer convenient for dismounting | |
| CN207506241U (en) | Garden chair | |
| CN202296543U (en) | Uncoiling device of textile machine | |
| CN101852407A (en) | Quick disassembly and assembly mechanism of ceiling lamp | |
| CN205899827U (en) | Hotel management teaching board | |
| CN211694054U (en) | Compact liquid crystal display convenient to installation | |
| CN216750592U (en) | Multifunctional interface conversion device for liquid crystal display | |
| CN218861390U (en) | Warning board convenient to use | |
| CN217633601U (en) | Damping plate supporting buckle | |
| CN203257174U (en) | End portion fixing device of tent support convenient to disassemble and assemble | |
| CN204530539U (en) | A kind of fastening devices of flexible column | |
| CN209064032U (en) | A kind of new-energy automobile high-voltage wiring harness fixed buckle parallel | |
| CN208831500U (en) | A kind of Multifunction position limiting connector convenient for assembly | |
| CN208377054U (en) | A kind of remote sensing unmanned plane being readily disassembled maintenance | |
| CN208348255U (en) | A kind of automobile buffering screw |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |