CN206962345U - Rotor wing unmanned aerial vehicle remove can cutting object device - Google Patents

Rotor wing unmanned aerial vehicle remove can cutting object device Download PDF

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Publication number
CN206962345U
CN206962345U CN201720690669.7U CN201720690669U CN206962345U CN 206962345 U CN206962345 U CN 206962345U CN 201720690669 U CN201720690669 U CN 201720690669U CN 206962345 U CN206962345 U CN 206962345U
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China
Prior art keywords
compressed gas
component
cylinder
mounting bracket
aerial vehicle
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Active
Application number
CN201720690669.7U
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Chinese (zh)
Inventor
罗庆雄
郑建荣
邓小康
林杰欢
郭琳
温带银
朱俊瑞
王晨玲
林东旭
许锡宇
李嘉阳
叶海宏
杨宇鹏
蔡钟皓
孙倩
许国伟
饶育平
温淦芬
蔡东晓
卢丹
邹智洛
关健
纪梓翰
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Guangzhou you Fei Intelligent Equipment Co., Ltd.
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罗庆雄
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Priority to CN201720690669.7U priority Critical patent/CN206962345U/en
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Publication of CN206962345U publication Critical patent/CN206962345U/en
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Abstract

The utility model discloses a kind of rotor wing unmanned aerial vehicle remove can cutting object device, including compressed gas Storing and conveying component, support component, shearing component and control assembly;Shearing component is connected by support component with compressed gas Storing and conveying component, support component includes hollow insulation arm mounting bracket and the hollow insulation arm being installed on hollow insulation arm mounting bracket, tracheae is provided with hollow insulation arm, tracheae one end is connected with shearing component, the other end is connected with compressed gas Storing and conveying component, and compressed gas Storing and conveying component is connected with control assembly.It can solve the problem that existing rotor wing unmanned aerial vehicle removes the problem of operating efficiency is low, risk is high to the foreign matter wound on exposed power circuit using device of the present utility model, the removing operation problem for particularly solving the exotic materials such as wire.

Description

Rotor wing unmanned aerial vehicle remove can cutting object device
Technical field
The utility model is related to unmanned plane field, more particularly to a kind of rotor wing unmanned aerial vehicle remove can cutting object device.
Device.
Background technology
The power circuit of outdoor erection is mostly nuditing wire, can easily be cut by various external kite strings, balloon line etc. Cut thing winding.These can cutting object be likely to result in feeder line fault, influence power transmission safety, it is also possible to can to touching The personnel of cutting object are discharged, and threaten human life's safety.
In recent years, due to the popularization and development of rotor wing unmanned aerial vehicle, power circuit remove can cutting object occur using spray The mode that agricultural chemicals rotor wing unmanned aerial vehicle is adapted as spraying fuel oil burn off foreign matter is spilt, this mode has the following disadvantages:First, the fuel oil of injection Imperfect combustion, sustained combustion on foreign matter, possible damage wires can be adhered to.2nd, the foreign matter to come off, will due to being attached with fuel oil Kindling material for a period of time, may be taken to ground and ignited other objects by sustained combustion.3rd, because high voltage electric field is to rotor wing unmanned aerial vehicle Electrical equipment influences very big, and flame component is conductor, and rotor wing unmanned aerial vehicle can not be close to wire, the gasoline fire that ejects at a distance Flame is difficult hit by windage.4th, the mode for spraying fuel oil burn off foreign matter is invalid for the high temperature resistant material such as wire.
Utility model content
In view of this, main purpose of the present utility model be to provide a kind of rotor wing unmanned aerial vehicle remove can cutting object dress Put, it is intended to solve existing rotor wing unmanned aerial vehicle and remove that operating efficiency is low, risk is high asks to the foreign matter that is wound on exposed power circuit Topic, particularly solves the removing operation problem of the exotic materials such as wire.
To achieve the above object, the technical solution of the utility model is realized in:
A kind of rotor wing unmanned aerial vehicle remove can cutting object device, including compressed gas Storing and conveying component, support component, cut Cut component and control assembly;Shearing component is connected by support component with compressed gas Storing and conveying component;
Wherein, support component includes rigid insulation tracheae body mounting bracket and is installed on rigid insulation tracheae body mounting bracket Rigid insulation tracheae body, support component one end are connected with shearing component, and the other end is connected with compressed gas Storing and conveying component;
Wherein, compressed gas Storing and conveying component is connected with control assembly.
Compressed gas Storing and conveying component includes compressed gas cylinder and is arranged at the gas transmission pressure regulator valve of compressed gas cylinder side, gas transmission Pressure regulator valve is connected by tracheae with gas solenoid valve, and compressed gas cylinder side is provided with check valve, and opposite side is provided with compressed gas cylinder outlet Mouthful, compressed gas cylinder mounting bracket is provided with the middle part of compressed gas cylinder, gas solenoid valve is connected with control assembly.
Support component includes support component mounting bracket and the rigid insulation tracheae body being installed on support component mounting bracket.
Shearing component includes the cylinder shell that is connected with support component one end, is provided with cylinder in cylinder shell, before cylinder Scissor body is provided with, cylinder includes cylinder body and is arranged at the back-moving spring of cylinder body both sides, and cylinder barrel rear end is provided with air inlet, promotes Piston is arranged in cylinder body, and scissors is arranged on cylinder barrel front end.
Control assembly includes wireless receiver and the transmitter with wireless receiver wireless connection, and wireless receiver includes connecing Receipts machine mounting bracket;The wireless receiving plate being arranged on receiver mounting bracket;It is arranged on the reception machine battery of wireless receiving plate side The receiver power supply being connected with receiving machine battery switchs.
Wireless launcher includes wireless launcher mounting bracket;Be arranged on wireless transmission plate on wireless launcher mounting bracket and The transmitter battery of wireless transmission plate side and the transmitter power switch of control transmitter battery are arranged on, in transmitter power Switch side is additionally provided with potentiometer.
Potentiometer includes gas solenoid valve controlling potential device, and gas solenoid valve controlling potential device is connected with gas solenoid valve.
Compared with prior art, the utility model rotor wing unmanned aerial vehicle remove can the device of cutting object have the advantages that:
This method is cut different from the use of high temperature melting, the use of rigid insulation tracheae is insulating materials, is cut using mechanical Cut component into highfield carry out operation can't by charge transfer to other devices and rotor wing unmanned aerial vehicle in itself, can safety behaviour Vertical rotor wing unmanned aerial vehicle carries out operation.
Brief description of the drawings
, below will be to embodiment in order to illustrate more clearly of the utility model embodiment or technical scheme of the prior art Or the required accompanying drawing used is briefly described in description of the prior art, it should be apparent that, drawings in the following description are only It is some embodiments of the utility model, for those of ordinary skill in the art, is not paying the premise of creative work Under, other accompanying drawings can also be obtained according to the structure shown in these accompanying drawings.
Structural representation when Fig. 1 is the scissors closure in the utility model.
Fig. 2 is structural representation when the scissors in the utility model opens.
Fig. 3 is compressed gas Storing and conveying component, control assembly and the support component structural representation in the utility model.
Drawing reference numeral explanation:
Label title label name claims
The gas solenoid valve mounting bracket of 1 compressed gas Storing and conveying component 122
The support component of 10 compressed gas cylinder 2
The rigid insulation tracheae body of 11 gas transmission pressure regulator valve 21
The rigid insulation tracheae body mounting bracket of 12 gas solenoid valve 22
The tracheae of 101 check valve 8
The control assembly of 102 compressed gas cylinder gas outlet 5
The wireless receiver of 103 compressed gas cylinder mounting bracket 50
The receiver mounting bracket of 110 gas transmission pressure regulator valve air inlet 501
The wireless receiving plate of 111 gas transmission pressure regulation valve air gate 502
112 adjusting pressuring knobs 503 receive machine battery
The receiver power supply of 113 pressure gauge 504 switchs
The wireless launcher of 120 gas solenoid valve air inlet 51
The shearing component of 121 gas solenoid valve gas outlet 3
The gas solenoid valve controlling potential device of 510 wireless launcher mounting bracket 514
The potentiometer of 511 wireless transmission plate 515
The cylinder shell of 512 transmitter battery 31
513 transmitter powers switch 33 target seekers
The scissors bit of 311 cylinder body inlet suction port 3221
The scissor body of 3222 shear shank 321
The scissor body mounting seat of 332 seeker mounting seat 316
The shear shank of 3211 scissors bit 3212
315 back-moving springs 3141 bore groove
The O-ring seal of 314 taper head part 3131
313 promote the cylinder body of piston 312
The back-moving spring of 331 guid arm 325
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the embodiment of the utility model is carried out Clearly and completely describing, it is clear that described embodiment is only part of the embodiment of the present utility model, rather than all Embodiment.
Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made The every other embodiment obtained, belong to the scope of the utility model protection.
It is to be appreciated that the directional instruction (such as up, down, left, right, before and after ...) of institute in the utility model embodiment It is only used for explaining relative position relation under a certain particular pose (as shown in drawings) between each part, motion conditions etc., such as When the fruit particular pose changes, then directionality instruction also correspondingly changes therewith.
In the utility model such as relating to the description of " first ", " second " etc. be only used for describe purpose, and it is not intended that Indicate or imply its relative importance or the implicit quantity for indicating indicated technical characteristic.Thus, define " first ", At least one this feature can be expressed or be implicitly included to the feature of " second ".
In description of the present utility model, " multiple " are meant that at least two, such as two, three etc., unless otherwise It is clearly specific to limit.
In the utility model, unless otherwise clearly defined and limited, term " connection ", " fixation " etc. should do broad sense reason Solution, for example, " fixation " can be fixedly connected or be detachably connected, or integrally;Can mechanically connect, also may be used Be electrical connection;Can be joined directly together, can also be indirectly connected by intermediary, can be the connection of two element internals Or the interaction relationship of two elements, limited unless otherwise clear and definite.For the ordinary skill in the art, can be with Concrete meaning of the above-mentioned term in the utility model is understood as the case may be.
In addition, the technical scheme between each embodiment of the utility model can be combined with each other, but must be with ability Domain those of ordinary skill can be implemented as basis, will be understood that when the combination appearance of technical scheme is conflicting or can not realize The combination of this technical scheme is not present, also not within the protection domain of the requires of the utility model.
As shown in figure 3, the rotor wing unmanned aerial vehicle remove can cutting object device, including compressed gas Storing and conveying component 1, branch Support component 2, shearing component 3 and control assembly 5;Shearing component 3 is connected by support component 2 and compressed gas Storing and conveying component 1 Connect.
Wherein, support component 2 includes rigid insulation tracheae body mounting bracket 22 and is installed on rigid insulation tracheae body mounting bracket Rigid insulation tracheae body 21 on 22, the one end of support component 2 is connected with shearing component 3, the other end and compressed gas Storing and conveying Component 1 connects.
Wherein, compressed gas Storing and conveying component 1 is connected with control assembly 5.
Gas Storing and conveying component is controlled by control assembly 5.
1~Fig. 3 of reference picture, compressed gas Storing and conveying component 1 include compressed gas cylinder 10 and are arranged at compressed gas cylinder 10 1 The gas transmission pressure regulator valve 11 of side, gas transmission pressure regulator valve 11 are connected by tracheae 8 with gas solenoid valve 12, and the side of compressed gas cylinder 10 is provided with single To valve 101, opposite side is provided with compressed gas cylinder gas outlet 102, and the middle part of compressed gas cylinder 10 is provided with compressed gas cylinder mounting bracket 103, gas Magnetic valve 12 is connected with control assembly 5.
Compressed gas cylinder 10 is sealing cylinder, can store compressed gas, is provided with compressed gas cylinder mounting bracket 103, is provided with and fills Gas check valve 101, gas outlet.
Gas transmission pressure regulator valve 11 includes, gas transmission pressure regulator valve air inlet 110, gas transmission pressure regulation valve air gate 111, the and of pressure gauge 113 Adjusting pressuring knob 112, outlet pressure can be adjusted by adjusting pressuring knob 112.
When gas solenoid valve 12 powers off gas solenoid valve air inlet 120 hold one's breath, gas solenoid valve gas outlet 121 and gas Solenoid valve vents mouth is ventilated, and gas solenoid valve air inlet 120 and gas solenoid valve gas outlet 121 are logical when gas solenoid valve 12 is powered Gas, gas solenoid valve exhaust outlet are held one's breath, and control assembly 5 is powered and controlled to it.
Reference picture 3, the hard that support component 2 includes the mounting bracket of support component 2 and is installed on the mounting bracket of support component 2 are exhausted Edge tracheae body 21.
Reference picture 1, shearing component 3 include the cylinder shell 31 being connected with the one end of support component 2, set in cylinder shell 31 There is cylinder, scissor body 321 is provided with before cylinder, cylinder includes cylinder body 312 and is arranged at the back-moving spring 325 of the both sides of cylinder body 312, Piston is promoted to be arranged in cylinder body 312, scissors is arranged on the front end of cylinder body 312.
Reference picture 3, control assembly 5 include wireless receiver 50 and the transmitter with the wireless connection of wireless receiver 50, nothing Line receiver 50 includes receiver mounting bracket 501;The wireless receiving plate 502 being arranged on receiver mounting bracket 501;It is arranged on nothing The reception machine battery 503 of the side of line receiver board 502 and the receiver power supply switch 504 being connected with receiving machine battery 503.
Reference picture 3, wireless launcher 51 include wireless launcher mounting bracket 510;It is arranged on wireless launcher mounting bracket 510 On wireless transmission plate 511 and be arranged on the transmitter battery 512 and control transmitter battery 512 of the side of wireless transmission plate 511 Transmitter power switch 513, transmitter power switch 513 sides be additionally provided with potentiometer 515.
Reference picture 3, potentiometer 515 include gas solenoid valve controlling potential device 514, gas solenoid valve controlling potential device 514 It is connected with gas solenoid valve 12.
The utility model rotor wing unmanned aerial vehicle remove can cutting object device operation principle it is as follows:
As shown in figure 3, specific component is by compressed gas Storing and conveying component 1, support component 2, shearing component 3 and control Component 5 forms.
Compressed gas cylinder 10 is filled with compressed gas by check valve 101.
By compressed gas cylinder 10, gas transmission pressure regulator valve 11, tracheae 8, gas solenoid valve 12, support component 2, shearing component 3, wireless Receiver 50 is assembled and is installed on rotor wing unmanned aerial vehicle, and wireless launcher 51 is pacified by wireless launcher mounting bracket 510 It is attached in rotor wing unmanned aerial vehicle remote control.
The adjusting pressuring knob 112 of gas transmission pressure regulator valve 11 is rotated as required adjusts outlet pressure size.
It is gas solenoid valve to control wireless receiver 50 by the gas solenoid valve controlling potential device 514 of wireless launcher 51 12 are powered, when gas solenoid valve 12 is powered gas solenoid valve air inlet 120 and gas solenoid valve gas outlet 121 ventilate, gas electricity Magnet valve gas outlet 121 is held one's breath, compressed gas by compressed gas cylinder 10, gas transmission pressure regulator valve 11, tracheae 8, gas solenoid valve 12, tracheae 8, Rigid insulation tracheae body 21 enters cylinder body 312.
Compression gas push piston 313, taper head part 314 slide toward the direction of 321 mounting seat of scissor body 316 in cylinder 31, The opening angle of shear shank 3212 and shear shank 3222 is corresponding as the groove width of cone groove 3141 of taper head part 314 diminishes and diminishes Scissors bit 3211 and the opening angle of scissors bit 3221 also diminish therewith, with produce shearing can cutting object action, simultaneously will Spring 315, the compression of the back-moving spring 325 of scissor body 321 produce elastic potential energy.
It is gas solenoid valve to control wireless receiver 50 by the gas solenoid valve controlling potential device 514 of wireless launcher 51 12 power-off, gas solenoid valve air inlet is held one's breath, gas solenoid valve gas outlet 121 is ventilated with gas solenoid valve gas outlet, cylinder body 312 Interior compressed gas is discharged by rigid insulation tracheae 21, tracheae 8 from gas solenoid valve gas outlet 121.
The spring compressed before in cylinder body 312 produces kinetic energy by taper head part 314 and promotes the pushed home of piston 313, The back-moving spring 325,315 of scissor body 321 produces kinetic energy and pushes the opening angle of shear shank 3212 and shear shank 3222 open recovery original Shape, the opening angle also big reinstatement of covariant of corresponding scissors bit 3211 and scissors bit 3221.
Because rigid insulation tracheae body 221 is insulating materials, therefore the entrance highfield progress operation of shearing component 3 can't incite somebody to action Charge transfer to other devices and rotor wing unmanned aerial vehicle in itself, can the manipulation rotor wing unmanned aerial vehicle of safety carry out operation.
Target seeker 33 be advantageous to by can cutting object be guided into the opening of scissors bit 3211 and scissors bit 3221, improve The reliability of operation.
Preferred embodiment of the present utility model is the foregoing is only, not thereby limits the scope of the claims of the present utility model, Every equivalent structure under utility model of the present utility model design, made using the utility model specification and accompanying drawing content Conversion, or directly/be used in other related technical areas indirectly and be included in scope of patent protection of the present utility model.

Claims (7)

1. a kind of rotor wing unmanned aerial vehicle remove can cutting object device, it is characterised in that including compressed gas Storing and conveying component, branch Support component, shearing component and control assembly;The shearing component passes through the support component and the compressed gas Storing and conveying Component connects;
Wherein, support component includes rigid insulation tracheae body mounting bracket and is installed on the rigid insulation tracheae body mounting bracket Rigid insulation tracheae body, described support component one end are connected with the shearing component, and the other end stores defeated with the compressed gas Sending component connects;The compressed gas Storing and conveying component is connected with the control assembly.
2. rotor wing unmanned aerial vehicle according to claim 1 remove can cutting object device, it is characterised in that the compressed gas Storing and conveying component includes compressed gas cylinder and is arranged at the gas transmission pressure regulator valve of the compressed gas cylinder side, and the gas transmission pressure regulator valve leads to Cross tracheae to be connected with gas solenoid valve, the compressed gas cylinder side is provided with check valve, and opposite side is provided with compressed gas cylinder gas outlet, institute State and be provided with compressed gas cylinder mounting bracket in the middle part of compressed gas cylinder, the gas solenoid valve is connected with the control assembly.
3. rotor wing unmanned aerial vehicle according to claim 1 remove can cutting object device, it is characterised in that the support component Including support component mounting bracket and the rigid insulation tracheae body being installed on the support component mounting bracket.
4. rotor wing unmanned aerial vehicle according to claim 1 remove can cutting object device, it is characterised in that the shearing component Including the cylinder shell being connected with described support component one end, cylinder is provided with the cylinder shell, is set before the cylinder There is scissor body, the cylinder includes cylinder body and is arranged at the back-moving spring of the cylinder body both sides, is provided with to promote in the cylinder body and lives Plug, the scissors are arranged on the cylinder body front end.
5. rotor wing unmanned aerial vehicle according to claim 1 remove can cutting object device device, it is characterised in that the control Component includes wireless receiver and the wireless launcher with the wireless receiver wireless connection, and the wireless receiver includes connecing Receipts machine mounting bracket;The wireless receiving plate being arranged on the receiver mounting bracket;It is arranged on connecing for the wireless receiving plate side Receive machine battery and switched with the receiver power supply that the reception machine battery is connected.
6. rotor wing unmanned aerial vehicle according to claim 5 remove can cutting object device device, it is characterised in that it is described wireless Transmitter includes wireless launcher mounting bracket;The wireless transmission plate that is arranged on the wireless launcher mounting bracket and it is arranged on institute The transmitter battery for stating wireless transmission plate side and the transmitter power switch for controlling the transmitter battery, in the transmitter Power switch side is additionally provided with potentiometer.
7. rotor wing unmanned aerial vehicle according to claim 6 remove can cutting object device, it is characterised in that the potentiometer bag Gas solenoid valve controlling potential device is included, the gas solenoid valve controlling potential device is connected with the gas solenoid valve.
CN201720690669.7U 2017-06-14 2017-06-14 Rotor wing unmanned aerial vehicle remove can cutting object device Active CN206962345U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201720690669.7U CN206962345U (en) 2017-06-14 2017-06-14 Rotor wing unmanned aerial vehicle remove can cutting object device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201720690669.7U CN206962345U (en) 2017-06-14 2017-06-14 Rotor wing unmanned aerial vehicle remove can cutting object device

Publications (1)

Publication Number Publication Date
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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110883819A (en) * 2019-11-23 2020-03-17 佛山市信成洋自动化设备有限公司 Large-shear high-precision pneumatic scissors

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110883819A (en) * 2019-11-23 2020-03-17 佛山市信成洋自动化设备有限公司 Large-shear high-precision pneumatic scissors

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Date Code Title Description
GR01 Patent grant
GR01 Patent grant
TR01 Transfer of patent right

Effective date of registration: 20180725

Address after: 510000 self compiled 2-11-1, No. 311, Whampoa Avenue, Tianhe District, Guangzhou, Guangdong.

Patentee after: Guangzhou you Fei Intelligent Equipment Co., Ltd.

Address before: 516000 yufengyuan 1206, 2 Mai Di Road, Huicheng District, Huizhou, Guangdong.

Patentee before: Luo Qingxiong

TR01 Transfer of patent right