CN107618652A - A kind of unmanned plane lid quick-release structure and jacking system - Google Patents
A kind of unmanned plane lid quick-release structure and jacking system Download PDFInfo
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- CN107618652A CN107618652A CN201710812752.1A CN201710812752A CN107618652A CN 107618652 A CN107618652 A CN 107618652A CN 201710812752 A CN201710812752 A CN 201710812752A CN 107618652 A CN107618652 A CN 107618652A
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- unmanned plane
- driving device
- jacking
- plane lid
- jacking system
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- 238000003032 molecular docking Methods 0.000 claims description 7
- 239000000758 substrate Substances 0.000 claims description 5
- 238000010276 construction Methods 0.000 abstract description 2
- 238000009434 installation Methods 0.000 abstract description 2
- 238000005516 engineering process Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
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Abstract
The invention discloses a kind of unmanned plane lid quick-release structure and jacking system, this jacking system includes jacking mechanism, for driving the jacking mechanism to make the manual driving device and romote-controlled driving device of jack-up action, and the jacking mechanism is connected with manual driving device and romote-controlled driving device respectively.This unmanned plane lid quick-release structure includes unmanned plane lid and jacking system, and the jacking system is located on the inside of unmanned plane lid.This unmanned plane lid Quick-disassembling device passes through the jacking mechanism in jacking system, manual driving device and romote-controlled driving device, realize the fast quick-detach of unmanned plane lid and aerial dismounting, the present invention is simple in construction, easy for installation, very convenient can quickly open lid.
Description
Technical field
The present invention relates to vehicle technology field, more particularly, to a kind of unmanned plane lid quick-release structure and jacking system.
Background technology
Unmanned plane lid has protective effect as the part in unmanned plane shell to fuselage interior part.Wherein, lid
Inner side is typically provided with the circuit board and remaining apparatus of unmanned plane, or be provided with the parachute of some emergencies etc..Nothing
By the purpose for being in order at overhaul of the equipments replacing, or emergent purpose, it is required for lid quickly to open in time.However, at present, nothing
The problems such as dismounting inconvenience, can not open in the air be present in man-machine lid.
The content of the invention
In view of the above-mentioned problems, the invention provides a kind of unmanned plane lid quick-release structure and jacking system, it can not only be fast
Fast manual unlocking, moreover it is possible to which quick remote control is opened.
The present invention is that technical scheme is used by solving its technical problem：
A kind of jacking system, including jacking mechanism, for drive the jacking mechanism make jack-up action manual actuation dress
Put and romote-controlled driving device, the jacking mechanism are connected with manual driving device and romote-controlled driving device respectively.
As the further improvement of such scheme, the jacking mechanism includes substrate and is rotatably arranged at base
Jacking block and turning arm on plate, the jacking block are connected by connecting element with turning arm, turning arm respectively with manual driving device
Connected with romote-controlled driving device.
As the further improvement of such scheme, the jacking block is provided with lug boss.
As the further improvement of such scheme, the connecting element is flexible member.
As the further improvement of such scheme, the manual driving device includes the push rod being fixedly connected with turning arm.
As the further improvement of such scheme, the romote-controlled driving device includes the drive that the turning arm can be driven to rotate
The control system and the signal for receiving signal that swing arm, the driving actuating arm rotate receive system.
A kind of unmanned plane lid quick-release structure, including unmanned plane lid and the jacking system described in any of the above-described, institute
Jacking system is stated to be located on the inside of unmanned plane lid.
As the further improvement of such scheme, the docking block docked with jacking block is provided with the inside of the unmanned plane lid.
As the further improvement of such scheme, the docking block offers the opening passed through for lug boss.
As the further improvement of such scheme, the manual driving device includes the push rod being fixedly connected with turning arm,
Through hole is offered in the unmanned plane lid, the push rod via through holes are extended on the outside of unmanned plane lid.
The beneficial effects of the invention are as follows：This unmanned plane lid Quick-disassembling device by the jacking mechanism in jacking system, manually
Drive device and romote-controlled driving device, the fast quick-detach of unmanned plane lid and aerial dismounting being realized, the present invention is simple in construction,
It is easy for installation, very convenient it can quickly open lid.
Brief description of the drawings
Technical scheme in order to illustrate the embodiments of the present invention more clearly, make required in being described below to embodiment
Accompanying drawing is briefly described.Obviously, described accompanying drawing is the part of the embodiment of the present invention, rather than is all implemented
Example, on the premise of not paying creative work, other that can also be obtained according to these accompanying drawings are set those skilled in the art
Meter scheme and accompanying drawing：
Fig. 1 is the structural representation of present pre-ferred embodiments；
Fig. 2 is the partial enlarged drawing at A in Fig. 1；
Fig. 3 is manual driving device, romote-controlled driving device and jacking mechanism internal structure in present pre-ferred embodiments
Structural representation；
Fig. 4 is the structural representation that block is docked in present pre-ferred embodiments.
Embodiment
Carried out below with reference to the design of embodiment and accompanying drawing to the present invention, concrete structure and caused technique effect clear
Chu, it is fully described by, to be completely understood by the purpose of the present invention, feature and effect.Obviously, described embodiment is this hair
Bright part of the embodiment, rather than whole embodiments, based on embodiments of the invention, those skilled in the art is not paying
The other embodiment obtained on the premise of creative work, belongs to the scope of protection of the invention.
Referring to figs. 1 to Fig. 4, a kind of unmanned plane lid quick-release structure of the invention and jacking system, it can not only fast hand
It is dynamic to open, moreover it is possible to which that quick remote control is opened.Wherein, this jacking system includes jacking mechanism 2, for driving the jacking mechanism 2 to make
The manual driving device 3 and romote-controlled driving device 4 of jack-up action, the jacking mechanism 2 respectively with manual driving device 3 and distant
Control drive device 4 connects.This unmanned plane lid quick-release structure includes unmanned plane lid 1 and jacking system, the jacking system
Positioned at the inner side of unmanned plane lid 1, the jacking system can jack up unmanned plane lid 1.This unmanned plane lid Quick-disassembling device passes through top
Mechanism 2, manual driving device 3 and romote-controlled driving device 4 are played, realizes the fast quick-detach of unmanned plane lid and aerial dismounting.
Wherein, reference picture 2 and Fig. 3, the jacking mechanism 2 include substrate 21 and are rotatably arranged at substrate 21
On jacking block 22 and turning arm 23, the jacking block 22 is connected by connecting element 24 with turning arm 23, it is preferred that the connection member
Part 24 is flexible member, further, the connecting element 24 be preferably spring, turning arm 23 respectively with manual driving device 3
Connected with romote-controlled driving device 4.
The jacking block 22 can be set to support in the inner side of unmanned plane lid 1, and be driven by turning arm 23, by unmanned plane hole
Open on the top of lid 1.In addition, the inner side of unmanned plane lid 1 can also be provided with the docking block 5 docked with jacking block 22.Specifically, it is described
Jacking block 22 includes lug boss 221, and the docking block 5 offers the opening 51 passed through for lug boss 221.During operation, turning arm 23
Rotated under the drive of manual driving device 3 and romote-controlled driving device 4, and drive jacking block 22 to rotate by connecting element 24, pushed up
The lug boss 221 of block 22 is rotated and supported on the upper wall surface of opening 51 in the opening 51 of docking block 5, so as to jack up unmanned plane
Lid 1.
Further, for reference picture 2 to Fig. 4, the manual driving device 3 includes the push rod being fixedly connected with turning arm 23, institute
State and through hole is offered in unmanned plane lid 1, the push rod via through holes extend to the outside of unmanned plane lid 1.It is described in the present embodiment
Push rod is located at the same side of the pivot of turning arm 23 with connecting element 24.The push rod and through hole are situated so as to operator
Member opens from the outside of unmanned plane lid 1 top, and operating personnel manually inwards promote push rod from through hole, and push rod drives turning arm 23
Rotate, so as to complete to jack up work.
Further, for reference picture 2 to Fig. 4, the romote-controlled driving device 4 includes the driving that the turning arm 23 can be driven to rotate
The control system and the signal for receiving signal that arm 41, the driving actuating arm 41 rotate receive system.In the present embodiment,
The actuating arm 41 is located at the lower section of turning arm 23 and is located at positioned at the side of the pivot of turning arm 23, the connecting element 24
The opposite side of the pivot of turning arm 23.Wherein, signal receives system for receiving the instruction that remote control is sent, and notifies to control
System processed, control system start actuating arm 41, and actuating arm 41 drives turning arm 23 to rotate, so as to complete to jack up work.
This unmanned plane lid Quick-disassembling device is realized by jacking mechanism 2, manual driving device 3 and romote-controlled driving device 4
The fast quick-detach of unmanned plane lid and aerial dismounting.In addition, jacking system include jacking mechanism 2, manual driving device 3 and
Romote-controlled driving device 4, it can be installed in miscellaneous part as independent jacking device and open object top.
Described above-described embodiment is that the above of the present invention is further described, but this should not be interpreted as into this hair
The scope of bright above-mentioned theme is only limitted to above-described embodiment, all models that the present invention is belonged to based on the technology that the above is realized
Enclose.
Claims (10)
- A kind of 1. jacking system, it is characterised in that：Moved including jacking mechanism (2), for driving the jacking mechanism (2) to make to jack up The manual driving device (3) and romote-controlled driving device (4) of work, the jacking mechanism (2) respectively with manual driving device (3) and Romote-controlled driving device (4) connects.
- A kind of 2. jacking system according to claim 1, it is characterised in that：The jacking mechanism (2) includes substrate (21) And jacking block (22) and turning arm (23) on substrate (21) are rotatably arranged at, the jacking block (22) is by connecting member Part (24) is connected with turning arm (23), and turning arm (23) is connected with manual driving device (3) and romote-controlled driving device (4) respectively.
- A kind of 3. jacking system according to claim 2, it is characterised in that：The jacking block (22) is provided with lug boss (221)。
- A kind of 4. jacking system according to claim 2, it is characterised in that：The connecting element (24) is flexible member.
- A kind of 5. jacking system according to claim 1, it is characterised in that：The manual driving device (3) includes and rotation The push rod that pivoted arm (23) is fixedly connected.
- A kind of 6. jacking system according to claim 1, it is characterised in that：The romote-controlled driving device (4) includes can band The actuating arm (41) of dynamic turning arm (23) rotation, drive the control system of actuating arm (41) rotation and for receiving The signal of signal receives system.
- A kind of 7. unmanned plane lid quick-release structure, it is characterised in that：Including unmanned plane lid (1) and such as claim 1 to 6 times Jacking system described in one, the jacking system are located on the inside of unmanned plane lid (1).
- A kind of 8. unmanned plane lid quick-release structure according to claim 7, it is characterised in that：The unmanned plane lid (1) Inner side is provided with the docking block (5) docked with jacking block (22).
- A kind of 9. unmanned plane lid quick-release structure according to claim 8, it is characterised in that：The docking block (5) opens up There is the opening (51) passed through for lug boss (221).
- A kind of 10. unmanned plane lid quick-release structure according to claim 7, it is characterised in that：The manual driving device (3) include the push rod being fixedly connected with turning arm (23), offer through hole on the unmanned plane lid (1), the push rod is through logical Hole is extended on the outside of unmanned plane lid (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710812752.1A CN107618652B (en) | 2017-09-11 | 2017-09-11 | Unmanned aerial vehicle flap quick-release structure and jacking device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710812752.1A CN107618652B (en) | 2017-09-11 | 2017-09-11 | Unmanned aerial vehicle flap quick-release structure and jacking device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107618652A true CN107618652A (en) | 2018-01-23 |
| CN107618652B CN107618652B (en) | 2024-04-02 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710812752.1A Active CN107618652B (en) | 2017-09-11 | 2017-09-11 | Unmanned aerial vehicle flap quick-release structure and jacking device |
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| CN (1) | CN107618652B (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CA2491245A1 (en) * | 2003-12-19 | 2005-06-19 | Etienne Lacroix Tous Artifices S.A. | Movement control device for a closing element for vehicles |
| CN202642092U (en) * | 2012-07-02 | 2013-01-02 | 江西洪都航空工业集团有限责任公司 | Improved rainproof quick-release port cover |
| CN105947173A (en) * | 2016-06-23 | 2016-09-21 | 西安爱生技术集团公司 | Automatic opening and closing mechanism of lower opening cover of unmanned aerial vehicle |
| CN106218856A (en) * | 2016-09-23 | 2016-12-14 | 江西洪都航空工业集团有限责任公司 | A kind of airplane hatch cover opener |
| CN206125397U (en) * | 2016-09-23 | 2017-04-26 | 江西洪都航空工业集团有限责任公司 | Can throw flap |
| CN207360561U (en) * | 2017-09-11 | 2018-05-15 | 珠海天晴航空航天科技有限公司 | A kind of unmanned plane lid quick-release structure and jacking system |
-
2017
- 2017-09-11 CN CN201710812752.1A patent/CN107618652B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CA2491245A1 (en) * | 2003-12-19 | 2005-06-19 | Etienne Lacroix Tous Artifices S.A. | Movement control device for a closing element for vehicles |
| CN202642092U (en) * | 2012-07-02 | 2013-01-02 | 江西洪都航空工业集团有限责任公司 | Improved rainproof quick-release port cover |
| CN105947173A (en) * | 2016-06-23 | 2016-09-21 | 西安爱生技术集团公司 | Automatic opening and closing mechanism of lower opening cover of unmanned aerial vehicle |
| CN106218856A (en) * | 2016-09-23 | 2016-12-14 | 江西洪都航空工业集团有限责任公司 | A kind of airplane hatch cover opener |
| CN206125397U (en) * | 2016-09-23 | 2017-04-26 | 江西洪都航空工业集团有限责任公司 | Can throw flap |
| CN207360561U (en) * | 2017-09-11 | 2018-05-15 | 珠海天晴航空航天科技有限公司 | A kind of unmanned plane lid quick-release structure and jacking system |
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| Publication number | Publication date |
|---|---|
| CN107618652B (en) | 2024-04-02 |
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Address after: Room 102, floor 1, 3 workshop, No. 6898, Zhuhai Avenue, Hongqi Town, Jinwan District, Zhuhai City, Guangdong Province Applicant after: ZHUHAI TIANQING AEROSPACE TECHNOLOGY Co.,Ltd. Address before: 519000 Guangdong Province, Zhuhai city planning exhibition hall on the third floor of the aviation city Jinwan District 312-30 room Applicant before: ZHUHAI TIANQING AEROSPACE TECHNOLOGY Co.,Ltd. |
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