CN108216601A - A kind of unmanned plane anti-collision protection device - Google Patents

A kind of unmanned plane anti-collision protection device Download PDF

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Publication number
CN108216601A
CN108216601A CN201810057066.2A CN201810057066A CN108216601A CN 108216601 A CN108216601 A CN 108216601A CN 201810057066 A CN201810057066 A CN 201810057066A CN 108216601 A CN108216601 A CN 108216601A
Authority
CN
China
Prior art keywords
unmanned plane
loop bar
moving lever
installation
protection device
Prior art date
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.)
Pending
Application number
CN201810057066.2A
Other languages
Chinese (zh)
Inventor
袁德梅
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Nantong Zhi Hang Mechanical And Electrical Technology Co Ltd
Original Assignee
Nantong Zhi Hang Mechanical And Electrical Technology Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Nantong Zhi Hang Mechanical And Electrical Technology Co Ltd filed Critical Nantong Zhi Hang Mechanical And Electrical Technology Co Ltd
Priority to CN201810057066.2A priority Critical patent/CN108216601A/en
Publication of CN108216601A publication Critical patent/CN108216601A/en
Pending legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/006Safety devices
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/04Helicopters
    • B64C27/08Helicopters with two or more rotors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00Type of UAV
    • B64U10/10Rotorcrafts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20Rotors; Rotor supports

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Remote Sensing (AREA)
  • Vibration Dampers (AREA)

Abstract

The invention discloses a kind of unmanned plane anti-collision protection devices in unmanned air vehicle technique field,Including unmanned plane ontology,The opposite side of the gantry base is threadedly coupled organic frame,Side installation motor of the rack far from gantry base,The output terminal installation rotor of the motor,The outer side surface centre position of the motor is provided with bumper post,The other end installation guard circle of the bumper post,Loop bar is installed between the adjacent rack,Moving lever is plugged on the loop bar,The intracavity bottom installation fixed block of the loop bar,The opposite side installation scissor-type stent of the fixed block,And the other end of scissor-type stent is mounted on moving lever,The outside of guard circle is extended at the top of the moving lever and Crashworthy plate is installed,The device can be when unmanned plane generates collision to the object of surrounding by Crashworthy plate and bumper post,Pass through elastic buffer,Reduce impact force impact force caused by the component of unmanned plane body interior,Damage caused by reduction,Save maintenance cost.

Description

A kind of unmanned plane anti-collision protection device
Technical field
The present invention relates to unmanned air vehicle technique field, specially a kind of unmanned plane anti-collision protection device.
Background technology
Unmanned plane take photo by plane, rescue, forest fire protection, many fields such as security protection are widely used, mainly by machine Body and multiple rotors form, and any protective device is not provided with, therefore during outer flight indoors on the rotor of traditional unmanned plane, When especially in the more complicated forest of environment or city, may unmanned plane be made in environment with misoperation inside Object collides, while various branches or fallen leaves may interfere rotor in forest, in this way can be to unmanned plane Mechanical structure causes larger damage, may lead to situation that is out of control or falling, for this purpose, it is proposed that a kind of unmanned plane anticollision Protective device.
Invention content
It is mentioned above in the background art to solve the purpose of the present invention is to provide a kind of unmanned plane anti-collision protection device Problem.
To achieve the above object, the present invention provides following technical solution:A kind of unmanned plane anti-collision protection device, including nobody Machine ontology, the upper and lower ends of the unmanned plane ontology and left and right ends are mounted on gantry base, and offered in gantry base Threaded hole, the opposite side of the gantry base are threadedly coupled organic frame, and the bottom outer wall of rack is equipped with and matches with threaded hole Screw thread, the rack far from gantry base side installation motor, the motor output terminal installation rotor, the motor Outer side surface centre position is provided with bumper post, the other end installation guard circle of the bumper post, the adjacent rack it Between loop bar is installed, be plugged with moving lever on the loop bar, the intracavity bottom installation fixed block of the loop bar, and fixed block and nobody Machine body outer wall is fixedly mounted, the opposite side installation scissor-type stent of the fixed block, and the other end installation of scissor-type stent On moving lever, the outside of guard circle is extended at the top of the moving lever and Crashworthy plate is installed.
Preferably, the Crashworthy plate includes fixed plate, and rubber slab, and spring are installed in the top of the fixed plate by spring The compressed spring identical for four groups of structures is uniformly provided with anti-skid bulge at the top of the rubber slab.
Preferably, the fixed plate vertical direction offers the through-hole to match with moving lever, the fixed plate level side Screw hole is offered upwards, the left and right sides of the screw hole, which is slided, is provided with bolt, and rubber pad is equipped at the top of bolt.
Preferably, the bumper post includes fixed link, and the top and bottom of the fixed link are plugged with buffering loop bar, institute The outer wall installation buffer spring of fixed link is stated, and the both ends of buffer spring are connect with buffering loop bar, the top buffering loop bar Upper installation link block, and the connecting hole to match with link block is offered on guard circle.
Preferably, the guard circle is rubber ring, and the cushion hole to match with moving lever is offered on guard circle.
Preferably, the bottom of the unmanned plane ontology is equipped with pedestal, and unmanned plane ontology is fixed by screws in pedestal On.
Compared with prior art, the beneficial effects of the invention are as follows:The apparatus structure is simple, convenient for disassembly and assembly, passes through Crashworthy plate , by elastic buffer, impact force can be reduced to nobody when unmanned plane generates collision to the object of surrounding with bumper post Impact force caused by the component of machine body interior, damage caused by reduction, saves maintenance cost.
Description of the drawings
Fig. 1 is schematic structural view of the invention;
Fig. 2 is rack construction schematic diagram of the present invention;
Fig. 3 is anticollision plate structure schematic diagram of the present invention;
Fig. 4 is fixed plate structure schematic diagram of the present invention;
Fig. 5 is bumper post structure diagram of the present invention.
In figure:1 unmanned plane ontology, 2 gantry bases, 3 racks, 4 rotors, 5 bumper posts, 51 fixed links, 52 buffer springs, 53 Buffer loop bar, 54 link blocks, 6 guard circles, 7 loop bars, 8 fixed blocks, 9 scissor-type stents, 10 moving levers, 11 Crashworthy plates, 111 fixations Plate, 1111 through-holes, 1112 screw holes, 1113 bolts, 1114 rubber pads, 112 springs, 113 rubber slabs, 114 anti-skid bulges, 12 electricity Machine.
Specific embodiment
Below in conjunction with the attached drawing in the embodiment of the present invention, the technical solution in the embodiment of the present invention is carried out clear, complete Site preparation describes, it is clear that described embodiment is only part of the embodiment of the present invention, instead of all the embodiments.It is based on Embodiment in the present invention, those of ordinary skill in the art are obtained every other without making creative work Embodiment shall fall within the protection scope of the present invention.
- 5 are please referred to Fig.1, the present invention provides a kind of technical solution:A kind of unmanned plane anti-collision protection device, including unmanned plane Ontology 1, the upper and lower ends of unmanned plane ontology 1 and left and right ends are mounted on gantry base 2, and offer spiral shell in gantry base 2 Pit, the opposite side of gantry base 2 are threadedly coupled organic frame 3, and the bottom outer wall of rack 3 is equipped with the spiral shell to match with threaded hole Line 31, easy to disassemble, side installation motor 12 of the rack 3 far from gantry base 2 ensures that unmanned plane has during flight Enough power, the output terminal installation rotor 4 of motor 12, the outer side surface centre position of motor 12 are provided with bumper post 5, The other end of bumper post 5 installs guard circle 6, and loop bar 7 is installed between adjacent rack 3, moving lever 10, loop bar 7 are plugged on loop bar 7 Intracavity bottom installation fixed block 8, and fixed block 8 and 1 outer wall of unmanned plane ontology are fixedly mounted, the opposite side installation of fixed block 8 Scissor-type stent 9, and the other end of scissor-type stent 9 is mounted on moving lever 10, the top of moving lever 10 extends to guard circle 6 Outside and Crashworthy plate 11 is installed, pass through elastic buffer, reduce impact force impact force caused by the component inside unmanned plane.
Wherein, Crashworthy plate 11 includes fixed plate 111, and the top of fixed plate 111 is installed rubber slab 113 by spring 112, prevented Only unmanned plane collides with object damages unmanned plane, and the compressed spring that spring 112 is identical for four groups of structures, is conducive to improve Cushioning effect, the top of rubber slab 113 are uniformly provided with anti-skid bulge 114, are conducive to the friction between increase and object;
111 vertical direction of fixed plate offers the through-hole 1111 to match with moving lever 10, in 111 horizontal direction of fixed plate Screw hole 1112 is offered, the left and right sides of screw hole 1112, which is slided, is provided with bolt 1113, and the top of bolt 1113 is equipped with Rubber pad 1114 prevents extruding from being damaged to moving lever 10, is conducive to fix moving lever 10 by bolt 1113, while conveniently Dismounting;
Bumper post 5 includes fixed link 51, and the top and bottom of fixed link 51 are plugged with buffering loop bar 53, fixed link 51 Outer wall installs buffer spring 52, and the both ends of buffer spring 52 are connect with buffering loop bar 53, are installed on top cushion loop bar 53 Link block 54, and the connecting hole to match with link block 54 is offered on guard circle 6, further play the role of buffering, it is right Unmanned plane ontology 1 is protected;
Guard circle 6 is rubber ring, is conducive to mitigate the weight of unmanned plane, saves cost of manufacture, and offered on guard circle 6 The cushion hole to match with moving lever 10;
The bottom of unmanned plane ontology 1 is equipped with pedestal, and unmanned plane ontology 1 is fixed by screws on pedestal, is conveniently torn open Unload installation.
Operation principle:Rack 3 is symmetrically loaded onto in the surrounding of unmanned plane ontology 1, rotor 4 is installed in the end of rack 3, and Guard circle 6 is fixed by bumper post 5, by installing Crashworthy plate 11, mitigates the overall weight of unmanned plane, ensures that unmanned plane is flying There is enough power, and Crashworthy plate 11 and bumper post 5 can generate collision in unmanned plane to the object of surrounding in capable process When, by elastic buffer, reduce impact force impact force caused by the component inside unmanned plane, in forest detects, Unmanned plane generates shock to trunk, and when progress low latitude is taken photo by plane in city, shock etc. is generated to the wall of building body, simple in structure, It is convenient for disassembly and assembly.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with Understanding without departing from the principles and spirit of the present invention can carry out these embodiments a variety of variations, modification, replace And modification, the scope of the present invention is defined by the appended.

Claims (6)

1. a kind of unmanned plane anti-collision protection device, including unmanned plane ontology (1), it is characterised in that:The unmanned plane ontology (1) Upper and lower ends and left and right ends are mounted on gantry base (2), and threaded hole, the frame ground are offered in gantry base (2) The opposite side of seat (2) is threadedly coupled organic frame (3), and the bottom outer wall of rack (3) is equipped with the screw thread to match with threaded hole (31), side installation motor (12) of the rack (3) far from gantry base (2), the output terminal installation rotation of the motor (12) The wing (4), the outer side surface centre position of the motor (12) are provided with bumper post (5), the other end of the bumper post (5) Guard circle (6) is installed, loop bar (7) between the adjacent rack (3) is installed, moving lever (10), institute are plugged on the loop bar (7) The intracavity bottom installation fixed block (8) of loop bar (7) is stated, and fixed block (8) is fixedly mounted with unmanned plane ontology (1) outer wall, it is described The opposite side installation scissor-type stent (9) of fixed block (8), and the other end of scissor-type stent (9) is mounted on moving lever (10), The outside of guard circle (6) is extended at the top of the moving lever (10) and Crashworthy plate (11) is installed.
2. a kind of unmanned plane anti-collision protection device according to claim 1, it is characterised in that:The Crashworthy plate (11) includes Rubber slab (113) is installed, and spring (112) is four in fixed plate (111), the top of the fixed plate (111) by spring (112) The identical compressed spring of structure is organized, anti-skid bulge (114) is uniformly provided at the top of the rubber slab (113).
3. a kind of unmanned plane anti-collision protection device according to claim 2, it is characterised in that:The fixed plate (111) is perpendicular Nogata offers spiral shell to the through-hole (1111) that matches with moving lever (10) is offered in fixed plate (111) horizontal direction Hole (1112), the left and right sides of the screw hole (1112), which is slided, is provided with bolt (1113), and the top peace of bolt (1113) Equipped with rubber pad (1114).
4. a kind of unmanned plane anti-collision protection device according to claim 1, it is characterised in that:The bumper post (5) includes Fixed link (51), the top and bottom of the fixed link (51), which are plugged with, buffers loop bar (53), outside the fixed link (51) Wall installation buffer spring (52), and the both ends of buffer spring (52) are connect with buffering loop bar (53), the top buffering loop bar (53) link block (54) on is installed, and the connecting hole to match with link block (54) is offered on guard circle (6).
5. a kind of unmanned plane anti-collision protection device according to claim 1, it is characterised in that:The guard circle (6) is rubber Cushion rubber, and the cushion hole to match with moving lever (10) is offered on guard circle (6).
6. a kind of unmanned plane anti-collision protection device according to claim 1, it is characterised in that:The unmanned plane ontology (1) Bottom pedestal is installed, and unmanned plane ontology (1) is fixed by screws on pedestal.
CN201810057066.2A 2018-01-22 2018-01-22 A kind of unmanned plane anti-collision protection device Pending CN108216601A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810057066.2A CN108216601A (en) 2018-01-22 2018-01-22 A kind of unmanned plane anti-collision protection device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810057066.2A CN108216601A (en) 2018-01-22 2018-01-22 A kind of unmanned plane anti-collision protection device

Publications (1)

Publication Number Publication Date
CN108216601A true CN108216601A (en) 2018-06-29

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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108910029A (en) * 2018-08-02 2018-11-30 滨州学院 A kind of protection mechanism of unmanned plane wing
CN108972630A (en) * 2018-08-22 2018-12-11 安徽爱依特科技有限公司 Robot anticollision device, collision-prevention device
CN109094799A (en) * 2018-08-29 2018-12-28 温利军 A kind of unmanned plane telescopic protection device and its manufacturing method
CN109292083A (en) * 2018-11-20 2019-02-01 南京森林警察学院 A kind of anti-collision push-style rotor wing unmanned aerial vehicle
CN113525702A (en) * 2021-08-17 2021-10-22 绍兴异想科技有限公司 Unmanned aerial vehicle for factory pipeline inspection
WO2022036731A1 (en) * 2020-08-17 2022-02-24 哈尔滨工业大学(深圳) Scissor-type extendable device, and unmanned aerial vehicle using same
CN116222419A (en) * 2022-12-26 2023-06-06 中恩光电科技(苏州)有限公司 Airborne omnibearing laser scanner

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108910029A (en) * 2018-08-02 2018-11-30 滨州学院 A kind of protection mechanism of unmanned plane wing
CN108910029B (en) * 2018-08-02 2021-06-04 滨州学院 Protection mechanism of unmanned aerial vehicle wing
CN108972630A (en) * 2018-08-22 2018-12-11 安徽爱依特科技有限公司 Robot anticollision device, collision-prevention device
CN109094799A (en) * 2018-08-29 2018-12-28 温利军 A kind of unmanned plane telescopic protection device and its manufacturing method
CN109292083A (en) * 2018-11-20 2019-02-01 南京森林警察学院 A kind of anti-collision push-style rotor wing unmanned aerial vehicle
CN109292083B (en) * 2018-11-20 2023-09-12 南京森林警察学院 Anticollision formula rotor unmanned aerial vehicle
WO2022036731A1 (en) * 2020-08-17 2022-02-24 哈尔滨工业大学(深圳) Scissor-type extendable device, and unmanned aerial vehicle using same
CN113525702A (en) * 2021-08-17 2021-10-22 绍兴异想科技有限公司 Unmanned aerial vehicle for factory pipeline inspection
CN113525702B (en) * 2021-08-17 2022-12-30 绍兴异想科技有限公司 Unmanned aerial vehicle for factory pipeline inspection
CN116222419A (en) * 2022-12-26 2023-06-06 中恩光电科技(苏州)有限公司 Airborne omnibearing laser scanner

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Application publication date: 20180629

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