CN207496937U - The wired self-locking Self-resetting Throwing device of unmanned plane - Google Patents

The wired self-locking Self-resetting Throwing device of unmanned plane Download PDF

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Publication number
CN207496937U
CN207496937U CN201721334490.4U CN201721334490U CN207496937U CN 207496937 U CN207496937 U CN 207496937U CN 201721334490 U CN201721334490 U CN 201721334490U CN 207496937 U CN207496937 U CN 207496937U
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CN
China
Prior art keywords
suspension hook
shrapnel
self
carbon plate
unmanned plane
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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.)
Expired - Fee Related
Application number
CN201721334490.4U
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Chinese (zh)
Inventor
康海碧
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Yunnan Baoyu Science And Technology Co Ltd
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Yunnan Baoyu Science And Technology Co Ltd
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Publication date
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Priority to CN201721334490.4U priority Critical patent/CN207496937U/en
Application granted granted Critical
Publication of CN207496937U publication Critical patent/CN207496937U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a kind of wired self-locking Self-resetting Throwing device of unmanned plane, including carbon plate, outside plate;The carbon plate, outside plate is arranged in parallel, steering engine has been bolted to connection on the carbon plate, the output terminal of the steering engine is fixedly connected with eccentric wheel, one end of the eccentric wheel and connecting rod is slidably connected, one end rotation connection of the other end and locating piece of the connecting rod, the other end and suspension hook the lock locking connection of the locating piece, in the carbon plate, suspension hook lock shaft is fixedly installed between outside plate, locating shaft, shrapnel axis, fixed pin, first positioning pin, second positioning pin, the middle part rotation connection of the suspension hook lock shaft and suspension hook lock, the middle part of the locating shaft and locating piece is rotatablely connected, the middle part of the shrapnel axis and mousing-hook shrapnel is rotatablely connected.After the suspension hook of the utility model slings cargo, cargo does not break off relations in transportational process, and the utility model controls the automatic unloading operation of cargo by circuit during unloading, and cargo unloads rear hanger and automatically resets.

Description

The wired self-locking Self-resetting Throwing device of unmanned plane
Technical field
The utility model is related to the Throwing device equipment technical fields of unmanned plane, and in particular to a kind of wired self-locking of unmanned plane is certainly Reset Throwing device.
Background technology
In unmanned plane field, unmanned plane can be used for freight is partly needed to carry out hoisting transportation, in unmanned plane pair When cargo carries out hoisting transportation, unmanned plane slings cargo firstly the need of with suspension hook, and the cargo needs sling ensure transporting Do not break off relations in journey, when unmanned plane is by near cargo transport to destination, need to unload cargo, to cargo to unload process usual Just cargo is thrown down when being the skyborne certain altitude of unmanned plane, it is mainly that unmanned plane passes through circuit and controls suspension hook will to throw lower process Cargo unloads.
Utility model content
The purpose of this utility model is to provide a kind of wired self-locking Self-resetting Throwing device of unmanned plane, the use of the new type can be right Cargo is lifted, and cargo can be carried out to throw lower discharging.
To solve the technical issues of above-mentioned, the utility model uses following technical scheme:
The wired self-locking Self-resetting Throwing device of unmanned plane, including carbon plate, outside plate;The carbon plate, outside plate are arranged in parallel, institute State and steering engine be bolted to connection on carbon plate, the output terminal of the steering engine is fixedly connected with eccentric wheel, the eccentric wheel and One end of connecting rod is slidably connected, one end rotation connection of the other end and locating piece of the connecting rod, the other end of the locating piece With suspension hook locking connection, suspension hook lock shaft, locating shaft, shrapnel axis, fixation are fixedly installed between the carbon plate, outside plate The middle part rotation connection of pin, the first positioning pin, the second positioning pin, the suspension hook lock shaft and suspension hook lock, the locating shaft and positioning The middle part rotation connection of part, the middle part rotation connection of the shrapnel axis and mousing-hook shrapnel, first positioning pin and described fixed The side of position part is located by connecting, and the side of second positioning pin and the mousing-hook shrapnel is located by connecting, and the fixed pin leads to It crosses a spring and is connected with the side elastic force that the suspension hook is locked, the fixed pin also passes through another spring and the mousing-hook bullet One end elastic force connection of piece.After locating piece rotation, the first positioning pin is used for position of the fixed positioning piece between carbon plate, outside plate, The other end and suspension hook lock for ensureing locating piece accurately realize locking connection, when another described spring pulls mousing-hook shrapnel During one end, a fulcrum for functioning as the rotation of mousing-hook shrapnel for the second positioning pin.
Further, the inside of the steering engine is equipped with motor, and the motor is connected with wire circuit.
Further, the carbon plate is the plank that material is carbon fiber, and the outside plate is the plank that material is aluminium alloy.
Further, the shrapnel axis, locating shaft, suspension hook lock shaft are simultaneously through carbon plate and outside plate.
Further, the locating piece, suspension hook lock, spring are arranged between the carbon plate, outside plate, and the mousing-hook bullet One end of piece is also disposed between the carbon plate, outside plate.
Further, the suspension hook lock is fixedly connected with one end of suspension hook, the other end of the suspension hook and the mousing-hook bullet The other end of piece is closed connection.
Compared with prior art, the beneficial effects of the utility model are:
1st, the utility model is simple in structure, easy to use, and when unmanned plane carries out hoisting transportation to cargo, suspension hook is by cargo After slinging, it ensure that cargo does not break off relations in transportational process due to being provided with mousing-hook shrapnel, when needing that cargo is thrown down The utility model controls the automatic unloading operation of cargo by circuit during unloading, and cargo unloads rear hanger and automatically resets.
2nd, the material of the carbon plate of the utility model is carbon fiber, and the material of outside plate is aluminium alloy, ensure that the utility model Be not in that carbon plate, outside plate destroy after practical for a long time.
3rd, it is such to be provided with conducive to mousing-hook since shrapnel axis, locating shaft, suspension hook lock shaft are through carbon plate, outside plate Shrapnel, locating piece, suspension hook lock are overhauled.
Description of the drawings
Fig. 1 is the construction profile of the utility model.
Fig. 2 is the positive internal structure chart of the utility model.
In figure, 1- suspension hooks, 2- shrapnels axis, 3- locating shafts, 4- steering engines, 5- bolts, 6- eccentric wheels, 7- carbon plates, 8- connecting rods, 9- Outside plate, 10- suspension hooks lock shaft, 11- suspension hooks lock, 12- locating shafts, the first positioning pins of 13-, 14- fixed pins, 15- springs, 16- second Positioning pin, 17- mousing-hook shrapnels.
Specific embodiment
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 is further described in detail.It should be appreciated that specific embodiment described herein is only used to explain The utility model is not used to limit the utility model.
Embodiment 1:
The wired self-locking Self-resetting Throwing device of unmanned plane, including carbon plate 7, outside plate 9;The carbon plate 7, outside plate 9 are mutually parallel and set It puts, steering engine 4 is fixedly connected with by bolt 5 on the carbon plate 7, the output terminal of the steering engine 4 is fixedly connected with eccentric wheel 6, institute The one end for stating eccentric wheel 6 and connecting rod 8 is slidably connected, one end rotation connection of the other end and locating piece 12 of the connecting rod 8, described The 11 locking connection of the other end and suspension hook lock of locating piece 12, suspension hook lock shaft is fixedly installed between the carbon plate 7, outside plate 9 10th, locating shaft 3, shrapnel axis 2, fixed pin 14, the first positioning pin 13, the second positioning pin 16, the suspension hook lock shaft 10 and suspension hook lock The middle part rotation connection of 11 middle part rotation connection, the locating shaft 3 and locating piece 12, the shrapnel axis 2 and mousing-hook shrapnel The side of 17 middle part rotation connection, first positioning pin 13 and the locating piece 12 is located by connecting, second positioning pin 16 and the side of the mousing-hook shrapnel 17 be located by connecting, the fixed pin 14 passes through a spring 15 and suspension hook lock 11 Side elastic force connection, the fixed pin 14 are also connected by another spring 15 with one end elastic force of the mousing-hook shrapnel 17, After locating piece 12 rotates, the first positioning pin 13 is used for position of the fixed positioning piece 12 between carbon plate 7, outside plate 9, ensures locating piece 12 other end and suspension hook lock 11 accurately realizes locking connection, when another described spring 15 pulls the one of mousing-hook shrapnel 17 During end, a fulcrum for functioning as the rotation of mousing-hook shrapnel 17 for the second positioning pin 16.
Embodiment 2:
On the basis of embodiment 1, the inside of the steering engine 4 is equipped with motor, and the motor is connected with wire circuit.
Embodiment 3:
On the basis of Examples 1 to 2, the carbon plate 7 is the plank that material is carbon fiber, and the outside plate 9 is that material is The plank of aluminium alloy, ensure that the utility model is not in that carbon plate 7, outside plate 9 destroy after practical for a long time.
Embodiment 4:
On the basis of Examples 1 to 3, the shrapnel axis 2, locating shaft 3, suspension hook lock shaft 10 simultaneously through carbon plate 7 with Outside plate 9, such be provided with 11 are overhauled conducive to mousing-hook shrapnel 17, locating piece 12, suspension hook lock, and when maintenance does not need to tear open The part needed replacing is taken out after opening carbon plate 7, outside plate 9, it is only necessary to remove shrapnel axis 2 or locating shaft 3 or suspension hook lock shaft accordingly 10, the corresponding part of corresponding axis can be carried out and be replaced.
Embodiment 5:
On the basis of Examples 1 to 4, the locating piece 12, suspension hook lock 11, spring 15 are arranged at the carbon plate 7, outer Between plate 9, and one end of the mousing-hook shrapnel 17 is also disposed between the carbon plate 7, outside plate 9, and such structure ensure that Entirely utility model structure is compact.
Embodiment 6:
On the basis of Examples 1 to 5, suspension hook lock 11 is fixedly connected with one end of suspension hook 1, the suspension hook 1 it is another The other end of one end and the mousing-hook shrapnel 17 is closed connection, after ensure that cargo hoisting on suspension hook 1, locating piece 12 and hangs During the locking connection of hook lock 11, cargo does not break off relations on suspension hook 1.
The course of work of the utility model is:
The utility model is simple in structure, easy to use, when using the utility model that can be lifted to cargo, stirs anti- After unhook shrapnel 17 by cargo hoisting on suspension hook 1, after cargo hoisting is on suspension hook 1, since fixed pin 14 passes through another bullet Spring 15 is connected with one end elastic force of mousing-hook shrapnel 17, and mousing-hook shrapnel 17 rebounds automatically, the other end of suspension hook 1 and the anticreep The other end of hook shrapnel 17 is closed connection, ensure that cargo hoisting on suspension hook 1 and when carrying out hoisting transportation to cargo, cargo exists It does not break off relations in transportational process on suspension hook 1, when near cargo transport to destination, needs that cargo is carried out to throw lower unloading, at this time After motor of the conducting wire into steering engine 4 sends signal, the motor in steering engine 4 drives the rotation of 4 output terminal of steering engine, 4 output terminal band of steering engine Movable eccentric wheel 6 rotates, and eccentric wheel 6 drives connecting rod 8 again, and connecting rod 8 is controlled after locating piece 12 turns an angle, locating piece 12 it is another One end and suspension hook lock 11 cancel locking connection, and suspension hook 1 is influenced by cargo gravity after automatically opening at this time, and object, which takes off hook, to be completed to throw Lower unloading operation, after the completion of unloading, since fixed pin 14 is connected by the side elastic force of a spring 15 and suspension hook lock 11, at this time It is automatically reset on suspension hook 1 without lifting cargo, suspension hook 1 by the pulling force of spring 15.
Although reference be made herein to the utility model is described in multiple explanatory embodiments of the utility model, still, It should be understood that those skilled in the art can be designed that a lot of other modifications and embodiment, these modifications and embodiment It will fall within spirit disclosed in the present application and spirit.More specifically, it discloses in the application, drawings and claims In the range of, a variety of variations and modifications can be carried out to the building block and/or layout of theme combination layout.In addition to building block And/or outside the modification and improvement of layout progress, to those skilled in the art, other purposes also will be apparent.

Claims (6)

1. the wired self-locking Self-resetting Throwing device of unmanned plane, it is characterised in that:Including carbon plate(7), outside plate(9);The carbon plate(7)、 Outside plate(9)It is arranged in parallel, the carbon plate(7)On pass through bolt(5)It is fixedly connected with steering engine(4), the steering engine(4)It is defeated Outlet is fixedly connected with eccentric wheel(6), the eccentric wheel(6)And connecting rod(8)One end be slidably connected, the connecting rod(8)It is another One end and locating piece(12)One end rotation connection, the locating piece(12)The other end and suspension hook lock(11)Locking connection, The carbon plate(7), outside plate(9)Between be fixedly installed suspension hook lock shaft(10), locating shaft(3), shrapnel axis(2), fixed pin (14), the first positioning pin(13), the second positioning pin(16), the suspension hook lock shaft(10)It is locked with suspension hook(11)Middle part rotation connect It connects, the locating shaft(3)And locating piece(12)Middle part rotation connection, the shrapnel axis(2)With mousing-hook shrapnel(17)In Portion is rotatablely connected, first positioning pin(13)With the locating piece(12)Side be located by connecting, second positioning pin (16)With the mousing-hook shrapnel(17)Side be located by connecting, the fixed pin(14)Pass through a spring(15)It is hung with described Hook lock(11)The connection of side elastic force, the fixed pin(14)Also pass through another spring(15)With the mousing-hook shrapnel(17) The connection of one end elastic force.
2. the wired self-locking Self-resetting Throwing device of unmanned plane according to claim 1, it is characterised in that:The steering engine(4)'s Inside is equipped with motor, and the motor is connected with wire circuit.
3. the wired self-locking Self-resetting Throwing device of unmanned plane according to claim 1, it is characterised in that:The carbon plate(7)It is Plank of the material for carbon fiber, the outside plate(9)It is the plank that material is aluminium alloy.
4. the wired self-locking Self-resetting Throwing device of unmanned plane according to claim 1, it is characterised in that:The shrapnel axis(2)、 Locating shaft(3), suspension hook lock shaft(10)Simultaneously through carbon plate(7)With outside plate(9).
5. the wired self-locking Self-resetting Throwing device of unmanned plane according to claim 1, it is characterised in that:The locating piece (12), suspension hook lock(11), spring(15)It is arranged at the carbon plate(7), outside plate(9)Between, and the mousing-hook shrapnel(17) One end be also disposed at the carbon plate(7), outside plate(9)Between.
6. the wired self-locking Self-resetting Throwing device of unmanned plane according to 1 or 5 any one of claim, it is characterised in that:Institute State suspension hook lock(11)And suspension hook(1)One end be fixedly connected, the suspension hook(1)The other end and the mousing-hook shrapnel(17)'s The other end is closed connection.
CN201721334490.4U 2017-10-17 2017-10-17 The wired self-locking Self-resetting Throwing device of unmanned plane Expired - Fee Related CN207496937U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201721334490.4U CN207496937U (en) 2017-10-17 2017-10-17 The wired self-locking Self-resetting Throwing device of unmanned plane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201721334490.4U CN207496937U (en) 2017-10-17 2017-10-17 The wired self-locking Self-resetting Throwing device of unmanned plane

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108583903A (en) * 2018-06-25 2018-09-28 南京大学 It is a kind of to launch mechanical hook and unmanned plane automatically
CN108891604A (en) * 2018-07-01 2018-11-27 陈爱霞 Unmanned plane dropping gear
CN109334984A (en) * 2018-09-20 2019-02-15 河南豫乾技术转移中心有限公司 A kind of deliverance apparatus and rescue mode based on unmanned plane
CN114506454A (en) * 2021-12-10 2022-05-17 武汉航空仪表有限责任公司 Loading and unloading system and method for airborne suspended object

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108583903A (en) * 2018-06-25 2018-09-28 南京大学 It is a kind of to launch mechanical hook and unmanned plane automatically
CN108891604A (en) * 2018-07-01 2018-11-27 陈爱霞 Unmanned plane dropping gear
CN108891604B (en) * 2018-07-01 2021-07-16 山东金塘电子科技有限公司 Unmanned aerial vehicle air-drop device
CN109334984A (en) * 2018-09-20 2019-02-15 河南豫乾技术转移中心有限公司 A kind of deliverance apparatus and rescue mode based on unmanned plane
CN114506454A (en) * 2021-12-10 2022-05-17 武汉航空仪表有限责任公司 Loading and unloading system and method for airborne suspended object

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CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20180615

Termination date: 20191017