CN107618652B - Unmanned aerial vehicle flap quick-release structure and jacking device - Google Patents
Unmanned aerial vehicle flap quick-release structure and jacking device Download PDFInfo
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- CN107618652B CN107618652B CN201710812752.1A CN201710812752A CN107618652B CN 107618652 B CN107618652 B CN 107618652B CN 201710812752 A CN201710812752 A CN 201710812752A CN 107618652 B CN107618652 B CN 107618652B
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- vehicle flap
- driving device
- jacking
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Abstract
The invention discloses an unmanned aerial vehicle flap quick-release structure and a jacking device, wherein the jacking device comprises a jacking mechanism, a manual driving device and a remote control driving device, wherein the manual driving device and the remote control driving device are used for driving the jacking mechanism to conduct jacking action, and the jacking mechanism is respectively connected with the manual driving device and the remote control driving device. This unmanned aerial vehicle flap quick detach structure includes unmanned aerial vehicle flap and jack-up device, jack-up device is located the unmanned aerial vehicle flap inboard. The unmanned aerial vehicle flap quick-release device realizes quick disassembly and aerial disassembly of the unmanned aerial vehicle flap through the jacking mechanism, the manual driving device and the remote control driving device in the jacking device.
Description
Technical Field
The invention relates to the technical field of aircrafts, in particular to an unmanned aerial vehicle flap quick-release structure and a jacking device.
Background
The unmanned aerial vehicle flap is as part in the unmanned aerial vehicle shell, has the guard action to fuselage internals. Wherein, the inside of the flap is generally provided with a circuit board and other equipment devices of the unmanned plane, or is provided with a parachute for emergency application and the like. Whether for equipment maintenance and replacement or emergency purposes, the flap needs to be opened quickly in time. However, at present, the unmanned aerial vehicle flap has the inconvenient dismouting, the unable scheduling problem of opening in the air.
Disclosure of Invention
Aiming at the problems, the invention provides the unmanned aerial vehicle flap quick-release structure and the jacking device, which can be opened quickly and manually and can be opened quickly and remotely.
The invention adopts the technical proposal for solving the technical problems that:
the jacking device comprises a jacking mechanism, a manual driving device and a remote control driving device, wherein the manual driving device and the remote control driving device are used for driving the jacking mechanism to conduct jacking action, and the jacking mechanism is respectively connected with the manual driving device and the remote control driving device.
As a further improvement of the scheme, the jacking mechanism comprises a base plate, a jacking block and a rotating arm, wherein the jacking block and the rotating arm are arranged on the base plate in a free rotation mode, the jacking block is connected with the rotating arm through a connecting element, and the rotating arm is respectively connected with the manual driving device and the remote control driving device.
As a further improvement of the above, the top block is provided with a boss.
As a further development of the above solution, the connecting element is an elastic element.
As a further improvement of the above solution, the manual driving device comprises a push rod fixedly connected with the rotating arm.
As a further improvement of the above scheme, the remote control driving device comprises a driving arm capable of driving the rotating arm to rotate, a control system for driving the driving arm to rotate, and a signal receiving system for receiving signals.
The utility model provides an unmanned aerial vehicle flap quick-release structure, includes unmanned aerial vehicle flap and the jack-up device of arbitrary one of the above-mentioned, the jack-up device is located the unmanned aerial vehicle flap inboard.
As a further improvement of the scheme, a butt joint block which is in butt joint with the top block is arranged on the inner side of the unmanned aerial vehicle cover.
As a further improvement of the above scheme, the butt joint block is provided with an opening for the boss to pass through.
As a further improvement of the scheme, the manual driving device comprises a push rod fixedly connected with the rotating arm, a through hole is formed in the unmanned aerial vehicle opening cover, and the push rod extends to the outer side of the unmanned aerial vehicle opening cover through the through hole.
The beneficial effects of the invention are as follows: the unmanned aerial vehicle flap quick-release device realizes quick disassembly and aerial disassembly of the unmanned aerial vehicle flap through the jacking mechanism, the manual driving device and the remote control driving device in the jacking device.
Drawings
In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the drawings that are required to be used in the description of the embodiments will be briefly described below. It is evident that the drawings described are only some embodiments of the invention, but not all embodiments, and that a person skilled in the art can obtain other designs and drawings from these drawings without inventive effort:
FIG. 1 is a schematic diagram of a preferred embodiment of the present invention;
FIG. 2 is an enlarged view of a portion of FIG. 1 at A;
FIG. 3 is a schematic view showing the internal structures of the manual driving device, the remote control driving device and the jack-up mechanism according to the preferred embodiment of the present invention;
fig. 4 is a schematic structural view of an abutment according to a preferred embodiment of the present invention.
Detailed Description
The conception, specific structure, and technical effects produced by the present invention will be clearly and completely described below with reference to the embodiments and the drawings to fully understand the objects, features, and effects of the present invention. It is apparent that the described embodiments are only some embodiments of the present invention, but not all embodiments, and that other embodiments obtained by those skilled in the art without inventive effort are within the scope of the present invention based on the embodiments of the present invention.
Referring to fig. 1 to 4, the unmanned aerial vehicle flap quick-release structure and the jacking device of the invention can be opened quickly and manually and can be opened quickly and remotely. The jacking device comprises a jacking mechanism 2, a manual driving device 3 and a remote control driving device 4, wherein the manual driving device 3 is used for driving the jacking mechanism 2 to perform jacking action, and the jacking mechanism 2 is respectively connected with the manual driving device 3 and the remote control driving device 4. This unmanned aerial vehicle flap quick-release structure includes unmanned aerial vehicle flap 1 and jack-up device, jack-up device is located unmanned aerial vehicle flap 1 inboard, but jack-up device jack-up unmanned aerial vehicle flap 1. This unmanned aerial vehicle flap quick discharge device passes through jack-up mechanism 2, manual drive device 3 and remote control drive device 4, realizes unmanned aerial vehicle flap's quick dismantlement and aerial dismantlement.
Referring to fig. 2 and 3, the jack-up mechanism 2 includes a base plate 21, and a jack-up block 22 and a rotating arm 23 rotatably disposed on the base plate 21, wherein the jack-up block 22 is connected to the rotating arm 23 through a connecting element 24, preferably, the connecting element 24 is an elastic element, further, the connecting element 24 is preferably a spring, and the rotating arm 23 is connected to the manual driving device 3 and the remote control driving device 4, respectively.
The ejector block 22 can be arranged to abut against the inner side of the unmanned aerial vehicle cover 1 and is driven by the rotating arm 23 to eject the unmanned aerial vehicle cover 1. In addition, a docking block 5 docking with the top block 22 may also be provided on the inside of the unmanned aerial vehicle flap 1. Specifically, the top block 22 includes a boss 221, and the docking block 5 is provided with an opening 51 through which the boss 221 passes. In operation, the rotary arm 23 is driven by the manual driving device 3 and the remote control driving device 4 to rotate, and the connection element 24 drives the top block 22 to rotate, and the protruding portion 221 of the top block 22 rotates in the opening 51 of the butt joint block 5 and abuts against the upper wall surface of the opening 51, so as to jack up the unmanned aerial vehicle cover 1.
Further, referring to fig. 2 to 4, the manual driving device 3 includes a push rod fixedly connected with the rotating arm 23, the unmanned aerial vehicle cover 1 is provided with a through hole, and the push rod extends to the outside of the unmanned aerial vehicle cover 1 through the through hole. In this embodiment, the push rod and the connecting element 24 are located on the same side of the rotation center of the rotating arm 23. The setting of push rod and through-hole is so that operating personnel jack-up from unmanned aerial vehicle flap 1 outside, and operating personnel is manual from through-hole department with push rod inboard propelling movement, and the push rod drives swinging boom 23 and rotates to accomplish the jack-up work.
Further, referring to fig. 2 to 4, the remote control driving device 4 includes a driving arm 41 capable of driving the rotation arm 23 to rotate, a control system for driving the driving arm 41 to rotate, and a signal receiving system for receiving a signal. In this embodiment, the driving arm 41 is located below the rotation arm 23 and on one side of the rotation center of the rotation arm 23, and the connecting element 24 is located on the other side of the rotation center of the rotation arm 23. The signal receiving system is used for receiving an instruction sent by the remote control device and informing the control system, the control system starts the driving arm 41, and the driving arm 41 drives the rotating arm 23 to rotate, so that jacking work is completed.
This unmanned aerial vehicle flap quick discharge device passes through jack-up mechanism 2, manual drive device 3 and remote control drive device 4, realizes unmanned aerial vehicle flap's quick dismantlement and aerial dismantlement. The jacking device includes a jacking mechanism 2, a manual drive device 3, and a remote control drive device 4, which are independent jacking devices and can be mounted on other components to jack up the object.
The foregoing embodiments are further illustrative of the present invention, but it should not be construed that the scope of the subject matter of the present invention is limited to the foregoing embodiments, and all techniques implemented based on the foregoing are within the scope of the present invention.
Claims (8)
1. The utility model provides a jack-up device which characterized in that: the lifting mechanism (2) comprises a base plate (21), and a lifting block (22) and a rotating arm (23) which are rotatably arranged on the base plate (21), wherein the lifting block (22) is connected with the rotating arm (23) through a connecting element (24), and the rotating arm (23) is connected with the manual driving device (3) and the remote control driving device (4) respectively; the remote control driving device (4) comprises a driving arm (41) capable of driving the rotating arm (23) to rotate, a control system for driving the driving arm (41) to rotate and a signal receiving system for receiving signals.
2. A jacking device as claimed in claim 1, wherein: the top block (22) is provided with a boss (221).
3. A jacking device as claimed in claim 2, wherein: the connecting element (24) is an elastic element.
4. A jacking device as claimed in claim 1, wherein: the manual driving device (3) comprises a push rod fixedly connected with the rotary arm (23).
5. An unmanned aerial vehicle flap quick detach structure, its characterized in that: comprising an unmanned aerial vehicle flap (1) and a jacking device according to any one of claims 1 to 4, which jacking device is located inside the unmanned aerial vehicle flap (1).
6. The unmanned aerial vehicle flap quick release structure of claim 5, wherein: the inside of the unmanned aerial vehicle flap (1) is provided with a butt joint block (5) which is in butt joint with the top block (22).
7. The unmanned aerial vehicle flap quick release structure of claim 6, wherein: the butt joint block (5) is provided with an opening (51) for the protrusion part (221) to pass through.
8. The unmanned aerial vehicle flap quick release structure of claim 5, wherein: the manual driving device (3) comprises a push rod fixedly connected with the rotating arm (23), a through hole is formed in the unmanned aerial vehicle cover (1), and the push rod extends to the outer side of the unmanned aerial vehicle cover (1) through the through hole.
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 |
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| Publication Number | Publication Date |
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| CN107618652A CN107618652A (en) | 2018-01-23 |
| CN107618652B true CN107618652B (en) | 2024-04-02 |
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| 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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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 |
|---|---|
| CN107618652A (en) | 2018-01-23 |
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