CN207931974U - A kind of device that unmanned plane horn quickly removes and installs - Google Patents

A kind of device that unmanned plane horn quickly removes and installs Download PDF

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Publication number
CN207931974U
CN207931974U CN201820339820.7U CN201820339820U CN207931974U CN 207931974 U CN207931974 U CN 207931974U CN 201820339820 U CN201820339820 U CN 201820339820U CN 207931974 U CN207931974 U CN 207931974U
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China
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horn
carbon pipe
quick release
pcb
nylon
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CN201820339820.7U
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Chinese (zh)
Inventor
刘奇
沈顺明
江尉
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Wuhan Flying Intelligent Technology Co Ltd
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Wuhan Flying Intelligent Technology Co Ltd
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Priority to CN201820339820.7U priority Critical patent/CN207931974U/en
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Abstract

The utility model discloses a kind of devices that unmanned plane horn quickly removes and installs,Including horn carbon pipe (13) and upper counterangle connector (10),The side of upper counterangle connector (10) is equipped with Quick Release horn lock core (9),Quick Release horn lock core (9) side is equipped with PCB (5) and male connector (8) in carbon pipe,The other side is equipped with female (11),Centre is equipped with epoxy partition board (6) and nylon inner lining (7),The male connector (8) is externally provided with nylon foundation (4),Nylon foundation (4),(5) PCB in carbon pipe,Epoxy partition board (6) and nylon inner lining (7) are equipped with two root long bolts,Quick Release horn lock nut (1) is set on the Quick Release horn lock core (9),Horn carbon pipe (13) is set to horn lock nut (1) and Quick Release horn lock core (9) is intermediate,The Quick Release horn lock nut (1) and Quick Release horn lock core (9) screw-thread fit.The device that the utility model unmanned plane horn quickly removes and installs can reach the quick installation effect of blindmate.

Description

A kind of device that unmanned plane horn quickly removes and installs
Technical field
The utility model belongs to multi-rotor unmanned aerial vehicle technical field, is quickly torn open more particularly, to a kind of unmanned plane horn Unload the device with installation.
Background technology
For unmanned plane compared with manned aircraft, it has small, low cost, easy to use, low to operational environment requirement, war The advantages that field survival ability is stronger.Therefore unmanned plane is grown rapidly, and corresponding unmanned plane horn is multifarious, a variety of different machines Arm configuration is all similar, and horn common currently on the market is all that simple carbon pipe is fixed or simple fold mechanism, Assembly is inconvenient, replaces difficult.
Unmanned plane Quick-dismantle component on the market is largely all utilized in the centre section even section CNC Al-alloy parts of horn Docking, is tightened with the mode of screw thread.This mode has the following defects:1. the carbon fiber pipe of each horn needs that two sections is divided to cut Cut, per more carbon fiber pipes cutting will more cutting errors, such accumulation of error can be amplified;2. liang section carbon fiber Line joint plug inside when pipe is docked by two CNC parts needs alignment in advance, is unfavorable for over-the-counter quick installation.
Patent CN206719542 discloses a kind of Quick Release horn structure for plant protection drone, including fuselage connects aluminium Alloy fixed seat and horn pipe fix aluminum alloy seat;Fuselage connection aluminium alloy fixed seat one end is fixedly installed in plant protection drone On fuselage, the other end is provided with external thread sleeve, and fuselage connection motor power supply female seat is provided in fuselage connection aluminium alloy fixed seat; Horn pipe one end is fixedly connected with horn pipe and fixes aluminum alloy seat, and horn pipe fixes the aluminum alloy seat other end and connect aluminium alloy with fuselage Fixed seat is detachably fixed connection, and the horn pipe fixation aluminum alloy seat other end, which is equipped with, connect motor power supply female seat matching with fuselage The horn connection motor of grafting is powered male seat, and the peripheral side that horn pipe fixes the aluminum alloy seat other end is set with and is used for and external screw thread The horn connection fuselage seat fixed thread set that set matching is screwed.
Patent CN106218882 discloses a kind of six rotor wing unmanned aerial vehicle Quick Release horns, including blade, brushless motor, electronics Speed adjusting module, paddle arm carbon pipe, only closing piece, horn set casing, horn metal frame, fixed card buckle, spring, male connector, the electronics Speed adjusting module is connected with the tail portion of the paddle arm carbon pipe, and the brushless motor is located above the brushless motor, described Only closing piece be inserted into the top of the paddle arm carbon pipe, the horn set casing is placed on the outer of the top of the paddle arm carbon pipe Side, the fixed card buckle are fixed on the inside of the horn set casing.
For unmanned plane horn dismounting inconvenience, there are the defect that large error and bad alignment realize Fast Installation, this realities Only the cumbersome technique for cutting carbon fiber pipe is cut with a carbon pipe connection and outfield horn blindmate is quick with novel mainly solution Installation improves outfield efficiency of installing software.
Utility model content
For the disadvantages described above or Improvement requirement of the prior art, the utility model provides a kind of fast quick-detach of unmanned plane horn With the device of installation, horn can achieve the effect that blindmate by the screw-thread fit of Quick Release horn lock nut and Quick Release horn lock core, Male connector is welded in carbon pipe on PCB, and carbon pipe liner, nylon foundation, PCB, epoxy partition board are socketed, and are integrally placed at successively in carbon pipe In Quick Release horn lock core, reduce the volume of Quick Release horn, female is welded on PCB terminal plates, and horn knot firmly installs, in outfield When installation, can quickly it install.
To achieve the goals above, the utility model provides a kind of device that unmanned plane horn quickly removes and installs, packet Horn carbon pipe and upper counterangle connector are included, the upper counterangle connector is two disposed in parallel, the upper counterangle connector Side is equipped with Quick Release horn lock core, and the Quick Release horn lock core is hollow structure, and the hollow structure side is equipped in carbon pipe PCB, the other side are equipped with female, and PCB is equipped with male connector in the carbon pipe, and epoxy partition board is equipped between the male connector and the female And nylon inner lining, the epoxy partition board and the nylon inner lining be equipped with the male connector relative to several through-holes, for public affairs The fixation of head;
Nylon foundation is arranged with outside the male connector, in the nylon foundation, carbon pipe on PCB, epoxy partition board and nylon inner lining Be all provided with there are two bolt hole, stay bolt be equipped in the bolt hole, for PCB in the nylon foundation, carbon pipe, epoxy partition board and The fixation of nylon inner lining;
Described Quick Release horn lock core one end is fixed on the upper counterangle connector, and the other end is equipped with Quick Release horn lock nut, Horn carbon pipe is set to the centre of the horn lock nut and Quick Release horn lock core, and the Quick Release horn lock nut is locked with the Quick Release horn Core screw-thread fit connects, to realize Fast Installation and the dismounting of horn.
Further, carbon pipe liner is arranged with outside the nylon foundation, the carbon pipe liner is placed in the Quick Release horn lock One end of in-core, the horn carbon pipe is placed in the carbon pipe liner.
Further, the device that the horn quickly removes and installs further includes axis pin, and the side wall of the carbon pipe liner is set Have a through-hole, the nylon foundation and the horn carbon pipe are also correspondingly provided with through-hole, the axis pin sequentially pass through the horn carbon pipe, Through-hole on carbon pipe liner and nylon foundation is for fixing.
Further, the device that the horn quickly removes and installs further includes PCB in carbon pipe, and the male connector is fixed on institute It states in carbon pipe on PCB, PCB is placed in the nylon foundation in the carbon pipe.
Further, the device that the horn quickly removes and installs further includes PCB terminal plates, the PCB terminal plates one Side is welded with the female, and the other side is welded with positive and negative anodes silica gel line.
Further, the PCB terminal plates are set between two upper counterangle connectors disposed in parallel, and are fixed on described fast Horn lock core is torn open close to the side of the upper counterangle connector.
In general, it can obtain down the above technical solutions conceived by the present invention are compared with the prior art, Row advantageous effect:
(1) device that the utility model unmanned plane horn quickly removes and installs, horn is by Quick Release horn lock nut and soon It tears the screw-thread fit of horn lock core open, can achieve the effect that blindmate, male connector are welded in carbon pipe on PCB, carbon pipe liner, nylon bottom PCB, epoxy partition board are socketed successively in column, carbon pipe, and are integrally placed in Quick Release horn lock core, and the volume of Quick Release horn is reduced, female Head is welded on PCB terminal plates, and horn knot firmly installs, and when outfield is installed, can quickly install.
(2) device that the utility model unmanned plane horn quickly removes and installs, the side wall of carbon pipe liner and nylon foundation It is equipped with through-hole, axis pin passes through through-hole to prevent part to be subjected to displacement in carbon pipe for fixing all parts.
Description of the drawings
Fig. 1 is a kind of structural schematic diagram for the device that unmanned plane horn quickly removes and installs of the utility model embodiment.
Wherein:1- Quick Release horns lock nut, 2- carbon pipes liner, 3- axis pins, 4- nylon foundation, in 5- carbon pipes PCB, 6- epoxy every Plate, 7- nylon inner linings, 8- male connectors, 9- Quick Release horns lock core, the upper counterangles 10- connector, 11- females, 12-PCB terminal plates, 13- Horn carbon pipe.
Specific implementation mode
In order to make the purpose of the utility model, technical solutions and advantages more clearly understood, below in conjunction with attached drawing and implementation Example, the present invention will be further described in detail.It should be appreciated that specific embodiment described herein is only explaining this Utility model is not used to limit the utility model.In addition, involved in the various embodiments of the present invention described below And to technical characteristic can be combined with each other as long as they do not conflict with each other.
Fig. 1 is a kind of structural schematic diagram for the device that unmanned plane horn quickly removes and installs of the utility model embodiment. As shown in Figure 1, the device that unmanned plane horn quickly removes and installs includes Quick Release horn lock nut 1, carbon pipe liner 2, axis pin 3, One component, the second component and third component, wherein first assembly includes upper counterangle connector 10 and Quick Release horn lock core 9, In, upper counterangle connector 10 is two, arranged in parallel, and two the intermediate of parallel upper counterangle connector 10 form hollow out Region;The end of one end of two upper counterangle connectors 10 is equipped with screw hole, for being connect with the fuselage of unmanned plane.Quick Release horn 9 one end of lock core is the hollow columnar structures of both-side opening, and the other end is square platy structure, four angles of square platy structure It is fixed on the end of the other end of two upper counterangle connectors 10, for Quick Release horn lock core 9 to be connect with the fuselage of unmanned plane. 9 one end far from upper counterangle connector 10 of Quick Release horn lock core is equipped with screw thread, and Quick Release horn lock nut 1 is hollow cylindric knot Structure, and its inner surface is equipped with screw thread, Quick Release horn lock core 9 is connect with 1 screw-thread fit of Quick Release horn lock nut, and horn carbon pipe 13 is set to It in Quick Release horn lock nut 1 and Quick Release horn lock core 9, is screwed by Quick Release horn lock nut 1 and Quick Release horn lock core 9, realizes horn Fast Installation and dismounting.
Second component includes nylon foundation 4, PCB5, male connector 8, epoxy partition board 6 and nylon inner lining 7 in carbon pipe, the second component In Quick Release horn lock core 9, from one end to the other end close to upper counterangle connector 10 be followed successively by nylon inner lining 7, epoxy every Plate 6, male connector 8, PCB5 and nylon foundation 4 in carbon pipe, PCB are printed circuit board, and PCB5 is equipped with several circular holes, male connector in carbon pipe It is inserted into carbon pipe in PCB circular holes, and welded by solder stick;Nylon foundation 4 is hollow structure, and PCB is set in carbon pipe In the hollow structure of nylon foundation 4, the side wall of nylon foundation 4 is equipped with through-hole;Epoxy partition board 6 and nylon inner lining 7 correspond to male connector 8 Position is equipped with several through-holes, and male connector 8 sequentially passes through the through-hole of epoxy partition board 6 and nylon inner lining 7.
It is arranged with carbon pipe liner 2 outside second component, carbon pipe liner 2 is set in Quick Release horn lock nut 1,2 He of carbon pipe liner The side wall of horn carbon pipe 13 is equipped with through-hole corresponding with the through-hole on the side wall of nylon foundation 4.Axis pin 3 sequentially passes through carbon pipe Through-hole on liner 2, horn carbon pipe 13 and nylon foundation 4, for fixing all parts, to prevent occurring in carbon pipe in part Displacement.It is equipped with bolt hole on PCB5, nylon inner lining 7 and epoxy partition board 6 in nylon foundation 4, carbon pipe, stay bolt is successively from a left side Nylon foundation 4 is passed through to the right side, PCB5 and epoxy partition board 6, nylon inner lining 7 and is tightened in carbon pipe, is filled in carbon pipe liner 2, most It Quick Release horn lock nut 1 and is screwed in rear enclosure.
Third component includes PCB terminal plates 12 and female 11, and PCB terminal plates 12 are square structure, and female 11 is welded on PCB The other side of the side of terminal plate 12, PCB terminal plates 12 is welded with positive and negative anodes silica gel line, and female 11 is set to Quick Release horn lock core 9 Hollow columnar structures in, and with male connector 8 be connected, PCB terminal plates 12 be set to two upper counterangles connector void region It is interior, and be fixed in the square platy structure of Quick Release horn lock core 9.
Preferably, upper counterangle connector 10 is with the center storehouse of fuselage, carbon fiber board is connect up and down, and passes through in 8 M3 six Angle pan-headed screw is fixed;
Preferably, by Quick Release horn lock core 9 with hexagonal pan-headed screw lock in 4 M3 in two upper counterangle connectors 10 On;
Preferably, PCB terminal plates 12 are connected and fixed on two upper counterangle connectors 10 with hexagonal pan-headed screw in 4 M3 On;
Preferably, positive and negative anodes silica gel line is 16AWG positive and negative anodes silica gel lines.
It is set preferably, being equipped with bolt hole on PCB5, nylon inner lining 7 and epoxy partition board 6 in nylon foundation 4, carbon pipe It is two, but is not limited to two.
As it will be easily appreciated by one skilled in the art that the above is only the preferred embodiment of the utility model only, not For limiting the utility model, any modification made within the spirit and principle of the present invention, equivalent replacement and change Into etc., it should be included within the scope of protection of this utility model.

Claims (6)

1. a kind of device that unmanned plane horn quickly removes and installs, including horn carbon pipe (13) and upper counterangle connector (10), The upper counterangle connector (10) is two disposed in parallel, which is characterized in that
The side of the upper counterangle connector (10) is equipped with Quick Release horn lock core (9), and the Quick Release horn lock core (9) is hollow knot Structure, the hollow structure side are equipped with PCB (5) in carbon pipe, and the other side is equipped with female (11), and PCB (5) is equipped in the carbon pipe Male connector (8), between the male connector (8) and the female (11) be equipped with epoxy partition board (6) and nylon inner lining (7), the epoxy every Plate (6) and the nylon inner lining (7) be equipped with the male connector relative to several through-holes, be used for the fixation of male connector (8);
Be arranged with nylon foundation (4) outside the male connector (8), PCB (5) in the nylon foundation (4), carbon pipe, epoxy partition board (6) and It is all provided on nylon inner lining (7) there are two bolt hole, the bolt hole is interior to be equipped with stay bolt, for the nylon foundation (4), carbon pipe The fixation of interior PCB (5), epoxy partition board (6) and nylon inner lining (7);
Described Quick Release horn lock core (9) one end is fixed on the upper counterangle connector (10), and the other end is locked equipped with Quick Release horn Cap (1), horn carbon pipe (13) are set to the centre of the horn lock nut (1) and Quick Release horn lock core (9), the Quick Release horn lock nut (1) it is connect with Quick Release horn lock core (9) screw-thread fit, to realize Fast Installation and the dismounting of horn.
2. a kind of device that unmanned plane horn quickly removes and installs according to claim 1, which is characterized in that the Buddhist nun Carbon pipe liner (2) is arranged with outside imperial foundation (4), the carbon pipe liner (2) is placed in the Quick Release horn lock core (9), the carbon One end of pipe liner (2) is placed in the horn carbon pipe (13).
3. a kind of device that unmanned plane horn quickly removes and installs according to claim 2, which is characterized in that the machine The device that arm quickly removes and installs further includes axis pin (3), and the side wall of the carbon pipe liner (2) is equipped with through-hole, the nylon bottom Column (4) and the horn carbon pipe (13) are also correspondingly provided with through-hole, and the axis pin (3) sequentially passes through the horn carbon pipe (13), carbon Through-hole on pipe liner (2) and nylon foundation (4) is for fixing.
4. a kind of device that unmanned plane horn quickly removes and installs according to claim 2, which is characterized in that the machine The device that arm quickly removes and installs further includes (5) PCB in carbon pipe, and the male connector (8) is fixed in the carbon pipe on PCB (5), PCB (5) is placed in the nylon foundation (4) in the carbon pipe.
5. a kind of device that unmanned plane horn quickly removes and installs according to claim 1, which is characterized in that the machine The device that arm quickly removes and installs further includes PCB terminal plates (12), and PCB terminal plates (12) side is welded with the female (11), the other side is welded with positive and negative anodes silica gel line.
6. a kind of device that unmanned plane horn quickly removes and installs according to claim 5, which is characterized in that described PCB terminal plates (12) are set between two upper counterangle connectors (10) disposed in parallel, and are fixed on the Quick Release horn lock core (9) Close to the side of the upper counterangle connector (10).
CN201820339820.7U 2018-03-12 2018-03-12 A kind of device that unmanned plane horn quickly removes and installs Active CN207931974U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201820339820.7U CN207931974U (en) 2018-03-12 2018-03-12 A kind of device that unmanned plane horn quickly removes and installs

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201820339820.7U CN207931974U (en) 2018-03-12 2018-03-12 A kind of device that unmanned plane horn quickly removes and installs

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110077571A (en) * 2019-06-10 2019-08-02 山东蜂巢航空科技有限公司 A kind of unmanned plane horn connection component and unmanned plane
CN113363760A (en) * 2021-08-09 2021-09-07 西安羚控电子科技有限公司 Can realize quick assembly disassembly's registrate structure
CN115230938B (en) * 2022-08-04 2024-04-26 西北工业大学 Quick connecting mechanism for modular unmanned aerial vehicle module replacement

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110077571A (en) * 2019-06-10 2019-08-02 山东蜂巢航空科技有限公司 A kind of unmanned plane horn connection component and unmanned plane
CN113363760A (en) * 2021-08-09 2021-09-07 西安羚控电子科技有限公司 Can realize quick assembly disassembly's registrate structure
CN113363760B (en) * 2021-08-09 2021-12-14 西安羚控电子科技有限公司 Can realize quick assembly disassembly's registrate structure
CN115230938B (en) * 2022-08-04 2024-04-26 西北工业大学 Quick connecting mechanism for modular unmanned aerial vehicle module replacement

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