CN106628213A - Quick disassembling device for mission loads of unmanned aerial vehicle - Google Patents
Quick disassembling device for mission loads of unmanned aerial vehicle Download PDFInfo
- Publication number
- CN106628213A CN106628213A CN201710110425.1A CN201710110425A CN106628213A CN 106628213 A CN106628213 A CN 106628213A CN 201710110425 A CN201710110425 A CN 201710110425A CN 106628213 A CN106628213 A CN 106628213A
- Authority
- CN
- China
- Prior art keywords
- hanging
- shaped hanging
- unmanned plane
- hanging groove
- load plate
- 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
- 238000005452 bending Methods 0.000 claims abstract description 5
- 239000003292 glue Substances 0.000 claims description 5
- 230000037431 insertion Effects 0.000 claims 1
- 238000003780 insertion Methods 0.000 claims 1
- 239000007787 solid Substances 0.000 claims 1
- 230000000903 blocking effect Effects 0.000 abstract 1
- 240000002853 Nelumbo nucifera Species 0.000 description 1
- 235000006508 Nelumbo nucifera Nutrition 0.000 description 1
- 235000006510 Nelumbo pentapetala Nutrition 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000000116 mitigating effect Effects 0.000 description 1
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
- B64D47/00—Equipment not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Load-Engaging Elements For Cranes (AREA)
Abstract
The invention discloses a quick disassembling device for mission loads of an unmanned aerial vehicle. The quick disassembling device is hung under the unmanned aerial vehicle by three hanging points and comprises a loading plate for fixing the mission loads, wherein two front U-shaped hanging grooves with backward openings are arranged at the front part of the loading plate, and a rear U-shaped hanging groove with a backward opening is arranged at the rear part of the loading plate; a locking hook for locking the loading plate and the hanging points is arranged under the rear U-shaped hanging groove; the front end of the locking hook is in pin joint at the lower bottom surface of the loading plate, and the rear end of the locking hook is provided with a bending hook for blocking the hanging points from sliding out of the rear U-shaped hanging groove; one end of a locking spring is fixed on the loading plate and the other end of the locking spring is fixed on the locking hook; the locking hook is poked by a force in the tension direction of the locking spring, the hanging points are inserted into the three U-shaped hanging grooves, then the locking hook is loosened, the locking spring is reset to drive the locking hook to return, and the hanging point at the rear part is locked in the rear U-shaped hanging groove by the bending hook. The quick disassembling device disclosed by the invention has the advantages that the mission loads can be quickly disassembled according to the needs, and the fixing is firm, so that the risk of falling of the mission loads when in flying of the unmanned aerial vehicle is reduced.
Description
Technical field
The invention belongs to technical field of aircraft design, and in particular to a kind of device for quickly disassembling of unmanned plane mission payload.
Background technology
With the fast development of unmanned air vehicle technique, increasing unmanned plane is applied to industry-by-industry and performs task, and
Carry equipment is also that unmanned plane performs the requisite instrument of task.The mission payload of traditional unmanned plane using screw and nobody
Machine is directly fixed, and dismounting is also pretty troublesome when needing to change loading device, and is possible to damage equipment, due to loading device with
Shi Keneng is changed, so the glue that typically will not screw is strengthened fixing, spiral shell may be caused because of aircraft vibrations in flight course
Silk loosens and causes danger, and causes unnecessary economic loss, or even jeopardizes personal safety.
The content of the invention
The present invention be directed to mission payload dismounting is inconvenient, and there is a problem of potential safety hazard, and research and design one kind can
Fast quick-detach, a kind of device for quickly disassembling of safe and reliable unmanned plane mission payload.
The technical solution adopted for the present invention to solve the technical problems is：
A kind of device for quickly disassembling of unmanned plane mission payload, it is characterised in that the device for quickly disassembling is hung over by three hanging points
The lower section of unmanned plane, the front portion of the unmanned plane has two symmetrically arranged hanging points, and rear portion arranges a hanging point, the Quick Release
Device includes the load plate for pinned task load, and the front portion of the load plate has two aft-opening front U-shaped hanging grooves,
Rear portion have one it is aft-opening after U-shaped hanging groove, afterwards before U-shaped hanging groove and two U-shaped hanging groove respectively be fixed on unmanned plane
Three hanging points correspondence；The lower section of U-shaped hanging groove has and is used for the latch hook of load plate and hanging point locking after described, the latch hook
In the bottom surface of the load plate, rear end has for stopping the crotch that hanging point is skidded off from rear U-shaped hanging groove, a locking front end pin joint
Spring one end is fixed in load plate, and the other end is fixed on latch hook, and to latch hook, one dials the power of locking spring draw direction
Unlocking hook, hanging point is inserted after three U-shaped hanging grooves from rear, unclamps latch hook, and locking spring reset strap moveable lock hook return, crotch will
The hanging point at rear portion is locked in rear U-shaped hanging groove.
Further, the locking spring is fixed on the middle part of latch hook, afterwards the front of U-shaped hanging groove.
Further, the hanging point is the bolt for being threaded in unmanned plane bottom, and is fixed with screw glue, is linked into U-shaped
Load plate is hung over by unmanned plane lower section by nut after hanging groove.
Further, there are multiple lightening holes in the load plate.
Further, the front portion of the load plate has the carry leg of bending downwards, and front U-shaped hanging groove is arranged on described in two
The lower end of the carry leg.
The beneficial effect of device for quickly disassembling of the unmanned plane mission payload of the present invention is：
1st, mission payload of the invention is fixed on the bottom surface of load plate, only need to push latch hook aside, U-shaped hanging groove after exposing, will
Three hanging points are inserted respectively in corresponding U-shaped hanging groove, then unclamp latch hook, latch hook is acted on next time in pulling back for locking spring
Position, hanging point is fixed in U-shaped hanging groove without deviating from, convenient to operation, can realize as needed quickly changeing task
Load.
2 hanging points being fixedly connected with unmanned plane can be permanently affixed on unmanned plane, fixed by screw glue, prevent spiral shell
Silk loosens and causes load to drop and cause unnecessary economic loss and danger.
3rd, screw and nut need not be unscrewed, without worrying that small part is lost during outdoor replacing loading device.
The 4th, multiple lightening holes are set in load plate, are designed using hollow out, while ensureing to facilitate installed load equipment,
Mitigate the flying weight of unmanned plane.
Description of the drawings
With reference to the accompanying drawings and detailed description the present invention is further detailed explanation.
Fig. 1 is the device for quickly disassembling stereogram of the unmanned plane mission payload of the embodiment of the present invention；
Fig. 2 is the device for quickly disassembling upward view of the unmanned plane mission payload of the embodiment of the present invention.
Wherein：1st, load plate, 11, lightening hole, 12, carry leg, 2, front U-shaped hanging groove, 3, rear U-shaped hanging groove, 4, latch hook, 41,
Crotch, 5, locking spring.
Specific embodiment
In conjunction with the accompanying drawings, the present invention is further detailed explanation.These accompanying drawings are simplified schematic diagram, only with
The basic structure of the illustration explanation present invention, therefore it only shows the composition relevant with the present invention.
A kind of device for quickly disassembling of unmanned plane mission payload as depicted in figs. 1 and 2, by three hanging points unmanned plane is hung over
Lower section, the front portion of unmanned plane has two symmetrically arranged hanging points, and rear portion arranges a hanging point, and so-called hanging point is to be threadedly secured in
The bolt of unmanned plane bottom, the nut of bolt and a part of stud are stretched out in the lower section of unmanned plane.
The device for quickly disassembling of the present embodiment includes the load plate 1 for pinned task loading device, and mission payload is fixed on load
On the bottom surface of lotus plate 1, multiple screwed holes can be set in load plate 1, mission payload is bolted on into load plate 1
On, then with screw glue fixation, bolt is not loosened.Can also be fixed on by other reliable fixed forms
In load plate 1.
The front portion of load plate 1 has two aft-opening front U-shaped hanging grooves 2, and rear portion is aft-opening rear U-shaped with one
Hanging groove 3, afterwards U-shaped hanging groove 2 is corresponding with three hanging points being fixed on unmanned plane respectively before U-shaped hanging groove 3 and two；U-shaped hanging groove 3 afterwards
Lower section have and be used for the latch hook 4 of load plate 1 and hanging point locking, the front end pin joint of latch hook 4 load plate 1 bottom surface, after
End has for stopping the crotch 41 that hanging point is skidded off from rear U-shaped hanging groove 3, and the one end of a locking spring 5 is fixed in load plate 1, separately
One end is fixed on latch hook 4, and to latch hook, 4 one make the power of the draw direction of locking spring 5 push latch hook 4 aside, and hanging point is inserted from rear
After entering three U-shaped hanging grooves, latch hook 4, the return of 5 reset strap moveable lock hook of locking spring 4, after crotch 41 is locked in the hanging point at rear portion are unclamped
In U-shaped hanging groove 3.
In order to avoid the stud of hanging point, locking spring 5 is fixed on the middle part of latch hook 4, afterwards the front of U-shaped hanging groove 3.
For the flying weight of mitigation unmanned plane as little as possible, the lightening hole 11 of multiple hollow outs is set in load plate 1,
While guaranteeing to carry installation mission payload equipment, weight is reduced as far as possible.
In the present embodiment, the front portion of load plate 1 has the carry leg 12 of bending downwards, and U-shaped hanging groove 2 is arranged on carry before two
The lower end of leg 12.
Specifically, latch hook 4 is pushed aside first, three hanging points are inserted respectively corresponding U-shaped hanging groove by U-shaped hanging groove 3 after exposing
It is interior, latch hook 4 is then unclamped, the return of latch hook 4 under the effect of pulling back of locking spring 5, crotch 41 is fixed on hanging point in U-shaped hanging groove
Without deviating from；When needing to change loading device, only latch hook 4 need to be pushed aside, three hanging points is deviate from from three U-shaped hanging grooves
Unload.
It should be appreciated that specific embodiment described above is only used for explaining the present invention, it is not intended to limit the present invention.By
Among the obvious change extended out of spirit or variation of the present invention are still in protection scope of the present invention.
Claims (5)
1. a kind of device for quickly disassembling of unmanned plane mission payload, it is characterised in that the device for quickly disassembling hangs over nothing by three hanging points
Man-machine lower section, the front portion of the unmanned plane has two symmetrically arranged hanging points, and rear portion arranges a hanging point, the fast dismounting
Put including the load plate (1) for pinned task load, the front portion of the load plate (1) is aft-opening front U-shaped with two
Hanging groove (2), rear portion have one it is aft-opening after U-shaped hanging groove (3), afterwards U-shaped hanging groove (2) is distinguished before U-shaped hanging groove (3) and two
It is corresponding with three hanging points being fixed on unmanned plane；The lower section of U-shaped hanging groove (3) has and is used for load plate (1) and extension after described
The latch hook (4) of point locking, in the bottom surface of the load plate (1), rear end has and is used for stopping for the front end pin joint of the latch hook (4)
The crotch (41) that hanging point is skidded off from rear U-shaped hanging groove (3) a, locking spring (5) one end is fixed in load plate (1), and the other end is solid
It is scheduled on latch hook (4), to latch hook, (4) one make the power of locking spring (5) draw direction push latch hook (4) aside, by hanging point from rear
After three U-shaped hanging grooves of insertion, latch hook (4) is unclamped, locking spring (5) reset strap moveable lock hook (4) return, crotch (41) is by rear portion
U-shaped hanging groove (3) is interior after hanging point is locked in.
2. the device for quickly disassembling of unmanned plane mission payload according to claim 1, it is characterised in that the locking spring (5)
It is fixed on the middle part of latch hook (4) and the front of rear U-shaped hanging groove (3).
3. the device for quickly disassembling of unmanned plane mission payload according to claim 1, it is characterised in that the hanging point is that screw thread connects
The bolt of unmanned plane bottom is connected on, and is fixed with screw glue, be linked into after U-shaped hanging groove and load plate (1) is hung over by nobody by nut
Machine lower section.
4. the device for quickly disassembling of unmanned plane mission payload according to claim 1, it is characterised in that on the load plate (1)
With multiple lightening holes (11).
5. the device for quickly disassembling of unmanned plane mission payload according to claim 1, it is characterised in that the load plate (1)
Front portion has the carry leg (12) of bending downwards, and front U-shaped hanging groove (2) is arranged on the lower end of the carry leg (12) described in two.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710110425.1A CN106628213A (en) | 2017-02-28 | 2017-02-28 | Quick disassembling device for mission loads of unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710110425.1A CN106628213A (en) | 2017-02-28 | 2017-02-28 | Quick disassembling device for mission loads of unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106628213A true CN106628213A (en) | 2017-05-10 |
Family
ID=58847643
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710110425.1A Pending CN106628213A (en) | 2017-02-28 | 2017-02-28 | Quick disassembling device for mission loads of unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106628213A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108557093A (en) * | 2018-02-06 | 2018-09-21 | 贵州电网有限责任公司 | A kind of multi-rotor unmanned aerial vehicle cruising inspection system Rapid replacing device |
Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB617238A (en) * | 1944-09-19 | 1949-02-03 | Frank George Manson | Improvements in or relating to instantaneous release hook connectors |
| US4102520A (en) * | 1976-03-22 | 1978-07-25 | R. Alkan & Cie | Dual-purpose ejector for aircraft load jettisoning mechanism |
| JPH0826197A (en) * | 1994-07-19 | 1996-01-30 | Ishikawajima Harima Heavy Ind Co Ltd | Rack structure for space |
| CN2506540Y (en) * | 2001-11-07 | 2002-08-21 | 哈尔滨飞机工业(集团)有限责任公司 | External hanging device for helicopter |
| JP2012007623A (en) * | 2010-06-22 | 2012-01-12 | Takigen Mfg Co Ltd | Instrument fixing device |
| CN204021256U (en) * | 2014-06-10 | 2014-12-17 | 中孚航空科技（天津）有限公司 | Depopulated helicopter modularization task hanger |
| CN104691769A (en) * | 2015-03-17 | 2015-06-10 | 南京航空航天大学 | Novel unmanned aerial vehicle airborne pod hanging frame |
| CN205652363U (en) * | 2016-05-04 | 2016-10-19 | 上海钛灵盾无人机技术有限公司 | Fast tying of unmanned aerial vehicle water tank constructs |
| CN106043732A (en) * | 2016-07-15 | 2016-10-26 | 天峋（常州）智能科技有限公司 | Small unmanned aerial vehicle catapulting hook |
| CN206502036U (en) * | 2017-02-28 | 2017-09-19 | 天峋（常州）智能科技有限公司 | A kind of device for quickly disassembling of unmanned plane mission payload |
-
2017
- 2017-02-28 CN CN201710110425.1A patent/CN106628213A/en active Pending
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB617238A (en) * | 1944-09-19 | 1949-02-03 | Frank George Manson | Improvements in or relating to instantaneous release hook connectors |
| US4102520A (en) * | 1976-03-22 | 1978-07-25 | R. Alkan & Cie | Dual-purpose ejector for aircraft load jettisoning mechanism |
| JPH0826197A (en) * | 1994-07-19 | 1996-01-30 | Ishikawajima Harima Heavy Ind Co Ltd | Rack structure for space |
| CN2506540Y (en) * | 2001-11-07 | 2002-08-21 | 哈尔滨飞机工业(集团)有限责任公司 | External hanging device for helicopter |
| JP2012007623A (en) * | 2010-06-22 | 2012-01-12 | Takigen Mfg Co Ltd | Instrument fixing device |
| CN204021256U (en) * | 2014-06-10 | 2014-12-17 | 中孚航空科技（天津）有限公司 | Depopulated helicopter modularization task hanger |
| CN104691769A (en) * | 2015-03-17 | 2015-06-10 | 南京航空航天大学 | Novel unmanned aerial vehicle airborne pod hanging frame |
| CN205652363U (en) * | 2016-05-04 | 2016-10-19 | 上海钛灵盾无人机技术有限公司 | Fast tying of unmanned aerial vehicle water tank constructs |
| CN106043732A (en) * | 2016-07-15 | 2016-10-26 | 天峋（常州）智能科技有限公司 | Small unmanned aerial vehicle catapulting hook |
| CN206502036U (en) * | 2017-02-28 | 2017-09-19 | 天峋（常州）智能科技有限公司 | A kind of device for quickly disassembling of unmanned plane mission payload |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108557093A (en) * | 2018-02-06 | 2018-09-21 | 贵州电网有限责任公司 | A kind of multi-rotor unmanned aerial vehicle cruising inspection system Rapid replacing device |
| CN108557093B (en) * | 2018-02-06 | 2024-02-27 | 贵州电网有限责任公司 | Quick reloading device of multi-rotor unmanned aerial vehicle inspection system |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US4068878A (en) | Container lift coupling | |
| RU2422332C2 (en) | Aircraft engine mounting device | |
| CN106256687B (en) | Rope suspensions device | |
| EP3175686B1 (en) | Locking device for rackable electronic equipment | |
| AU2014268120B2 (en) | Improvements in karabiners | |
| CA2720971C (en) | Fastening system and method for fastening an element of airplane interior equipment | |
| US20150239559A1 (en) | Apparatus and Method of Attachment of a Payload | |
| CA2690269C (en) | Pivoting equipment carrier in combination with a modified luggage rack | |
| US3801051A (en) | Tow plate | |
| CN103477007A (en) | Locking device with mechanical detection of closure and opening | |
| CN106628213A (en) | Quick disassembling device for mission loads of unmanned aerial vehicle | |
| US20080232924A1 (en) | Nut System and Aircraft Engine Mounting Structure Comprising Same | |
| CN206502036U (en) | A kind of device for quickly disassembling of unmanned plane mission payload | |
| CN207814138U (en) | A kind of spring locking pin | |
| CN101709734A (en) | C-type locking pull-plug device | |
| CN110803285A (en) | Landing disengaging lock and automatic unlocking method | |
| US9150309B2 (en) | Fastening system for hanging mountable overhead containers | |
| CN211543892U (en) | Landing disengaging lock | |
| CN210037232U (en) | Portable static adjusting equipment for hydraulic brake control unit | |
| RU2680228C1 (en) | Multi-functional beam holder | |
| US20160137300A1 (en) | Aircraft interior module support system including shared fittings | |
| CN209729770U (en) | A kind of air switch blocking device | |
| US20120102719A1 (en) | Attachment interface device for attaching mobile equipment to an aircraft structure | |
| US20130032684A1 (en) | Fastening system for suspended overhead storage bins | |
| CN205713578U (en) | A kind of lid quick-release lock structure |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20230111 Address after: Room 2211, 22nd Floor, Block D, Zhizhen Building, No. 7 Zhichun Road, Haidian District, Beijing 100088 Applicant after: TIANXUN INNOVATION (BEIJING) TECHNOLOGY CO.,LTD. Address before: Building A1, Zhongke entrepreneurship center, Changzhou science and Education City, No.18, middle Changwu Road, Changzhou City, Jiangsu Province, 213000 Applicant before: VOLITATION (CHANGZHOU) INTELLIGENT TECHNOLOGY CO.,LTD. |
|
| TA01 | Transfer of patent application right |