CN108528688A - A kind of unmanned plane wing protective device - Google Patents

A kind of unmanned plane wing protective device Download PDF

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Publication number
CN108528688A
CN108528688A CN201810444625.5A CN201810444625A CN108528688A CN 108528688 A CN108528688 A CN 108528688A CN 201810444625 A CN201810444625 A CN 201810444625A CN 108528688 A CN108528688 A CN 108528688A
Authority
CN
China
Prior art keywords
unmanned plane
plane wing
protection net
wing
branch sleeve
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.)
Withdrawn
Application number
CN201810444625.5A
Other languages
Chinese (zh)
Inventor
陈茜
郭祥
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.)
Sichuan University
Jincheng College of Sichuan University
Original Assignee
Sichuan University
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 Sichuan University filed Critical Sichuan University
Priority to CN201810444625.5A priority Critical patent/CN108528688A/en
Publication of CN108528688A publication Critical patent/CN108528688A/en
Withdrawn legal-status Critical Current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
    • B64U50/00Propulsion; Power supply
    • B64U50/10Propulsion
    • B64U50/19Propulsion using electrically powered motors

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Remote Sensing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Toys (AREA)

Abstract

The invention discloses a kind of unmanned plane wing protective devices, it includes drone body and unmanned plane wing, is fixedly connected with drone body by connecting rod equipped with motor on the downside of unmanned plane wing.Unmanned plane wing protective device further includes protection net, and protection net is symmetrically disposed on the both sides up and down of unmanned plane wing, and one end of protection net is connected to by reinforcing adjusting rod in drone body;Protection net is by buffering adjustment structure connection;Buffering adjustment structure is made of the branch sleeve, elastic parts and decoupling rod positioned at both ends, the tail end of branch sleeve is fixed on the top side face of protection net, the front end of branch sleeve is open-celled structure, and elastic parts is provided in its hole, decoupling rod passes through the extension of branch sleeve front end to be fixed on elastic parts.The invention has the advantages that it is detachable, it solves wing and bumps against safety problem caused by object, more comprehensive protection, reasonable design, safety coefficient height are carried out to unmanned plane wing.

Description

A kind of unmanned plane wing protective device
Technical field
The present invention relates to air vehicle technique fields, more particularly, to a kind of unmanned plane wing protective device.
Background technology
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, using radio robot and is provided for oneself The not manned aircraft that presetting apparatus manipulates, or fully or intermittently automatically operated by car-mounted computer.With someone It drives an airplane and compares, unmanned plane is often more suitable for those participating in for tasks that can be unwilling to mankind's generation danger or the mankind.Nobody Machine press application field, can be divided into it is military with it is civilian.Military aspect, unmanned plane are divided into reconnaissance plane and target drone.Civilian aspect, unmanned plane + sector application, which is unmanned plane, really just have been needed;At present take photo by plane, agricultural, plant protection, miniature self-timer, express transportation, disaster relief, Observe wild animal, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field Application, greatly expanded the purposes of unmanned plane itself, developed country is also in actively extension sector application and development unmanned plane Technology.
But the wing of existing unmanned plane it is general it is exposed outside, on the one hand there is wing and contact other objects, cause Wing damages, and influences to fly;On the other hand, there are possibility to contact people, causes safety problem.Even if being protected using existing wing Device, but its be generally too it is simple and crude, and be not easy to dismounting installation, design it is unreasonable, use and be also inconvenient.
Invention content
To solve the above-mentioned problems, the present invention proposes that the present invention provides a kind of unmanned plane wing protective devices.
To achieve the goals above, the present invention adopts the following technical scheme that:A kind of unmanned plane wing protective device, this nobody Machine wing protective device includes drone body and unmanned plane wing, and the inorganic man-machine wing is uniformly arranged on the week of drone body Side.
The drone body is provided with cavity body in its side, and unmanned plane wing is placed in cavity body, unmanned plane machine Motor is provided on the downside of the wing, the output shaft end side of motor is connected in the central shaft hole of unmanned plane wing, to realize unmanned plane The rotation of wing;The motor is fixedly connected by connecting rod with drone body, and one end of connecting rod is provided with for fixing The support portion of motor.
The unmanned plane wing protective device further includes having protection net, and protection net is symmetrically disposed on unmanned plane wing One end of upper and lower both sides, protection net is connected to by reinforcing adjusting rod in drone body;The protection net passes through buffering Adjustment structure connects.
The buffering adjustment structure is made of the branch sleeve, elastic parts and decoupling rod positioned at both ends, branch sleeve Tail end is fixed on the top side face of protection net, and the front end of branch sleeve is open-celled structure, and is provided with elastic parts in its hole, is subtracted Shake bar passes through the extension of branch sleeve front end to be fixed on elastic parts.
Further, the branch sleeve in the buffering adjustment structure forms telescoping mechanism with decoupling rod.
Further, the buffering adjustment structure sets at least to two between every group of protection net, and quantity is even Number.
Further, the structure for reinforcing adjusting rod and operation principle are identical as buffering adjustment structure.
Further, the material of the protection net is stainless steel wire or nylon rope.
Compared with prior art, the beneficial effects of the present invention are:Detachably, it is easily installed;Use telescopic connection Sleeve coordinates the use of decoupling rod and elastic parts, can effectively be buffered to impact force, solve wing and bump against object Caused by safety problem, more comprehensive protection carried out to unmanned plane wing, reasonable design, safety coefficient is high.
Description of the drawings
Fig. 1 is the structural diagram of the present invention;
Fig. 2 is the overlooking structure diagram of office of the present invention;
Fig. 3 is the attachment structure schematic diagram of present invention buffering adjustment structure;
Reference sign:1- drone bodies;2- protection nets;3- unmanned plane wings;4- connecting rods;5- motors;6- is buffered Adjustment structure;61- decoupling rods;62- elastic parts;63- branch sleeves;7- reinforces adjusting rod.
Specific implementation mode
For a clearer understanding of the technical characteristics, objects and effects of the present invention, now control illustrates this hair Bright specific implementation mode, but protection scope of the present invention be not limited to it is as described below.
As shown in Fig. 1 ~ Fig. 3, the present invention provides a kind of unmanned plane wing protective device, the unmanned plane wing protective devices Include drone body 1 and unmanned plane wing 3, the inorganic man-machine wing 3 is uniformly arranged on the side of drone body.
The drone body 1 is provided with cavity body in its side, and unmanned plane wing 3 is placed in cavity body, unmanned plane The downside of wing 3 is provided with motor 5, and the output shaft end side of motor 5 is connected in the central shaft hole of unmanned plane wing 3, to realize The rotation of unmanned plane wing 3;The motor 5 is fixedly connected by connecting rod 4 with drone body 1, one end setting of connecting rod 4 It is useful for the support portion of fixed motor 5.
The unmanned plane wing protective device further includes having protection net 2, and protection net 2 is symmetrically disposed on unmanned plane wing One end of 3 both sides up and down, protection net 2 is connected to by reinforcing adjusting rod 7 in drone body 1;The protection net 2 is logical It is too slow to reconstitute the connection of section structure 6.
The buffering adjustment structure 6 is made of the branch sleeve 63, elastic parts 62 and decoupling rod 61 positioned at both ends, connection The tail end of sleeve 63 is fixed on the top side face of protection net 2, and the front end of branch sleeve 63 is open-celled structure, and is provided in its hole Elastic parts 62, decoupling rod 61 pass through the extension of 63 front end of branch sleeve to be fixed on elastic parts 62.
Branch sleeve 63 in the buffering adjustment structure 6 forms telescoping mechanism with decoupling rod 61.
Further, in this embodiment the buffering adjustment structure 6 is set as four between every group of protection net 2.
The structure for reinforcing adjusting rod 7 and operation principle are identical as buffering adjustment structure 6.
Further, in this embodiment the material of the protection net 2 is stainless steel wire.
It should be noted that unmanned plane is in use, unmanned plane wing 3 may be made to hit in the case of operation error On the shelters such as building, due to the fragility of of unmanned plane wing 3 itself, powerful impact force easily damages unmanned plane wing 3, So protection net 2 is arranged in the outside of unmanned plane wing 3, when protection net 2 is hit, decoupling rod 61 can be promoted to connect Telescopic moving in sleeve 63,62 forced compression of elastic parts or stretching, promote buffer adjustment structure 6 and reinforce adjusting rod 7 by The elastic recovery of force compresses, elastic parts 62 can drive decoupling rod 61 and branch sleeve 63 to be moved to negative direction again, to Achieve the purpose that weaken impact force, comprehensive protection carries out wing with this.
The above disclosure is only the preferred embodiments of the present invention, cannot limit the right model of the present invention with this certainly It encloses, therefore equivalent changes made in accordance with the claims of the present invention, is still within the scope of the present invention.

Claims (5)

1. a kind of unmanned plane wing protective device, which includes drone body(1)And unmanned plane Wing(3), the inorganic man-machine wing(3)It is uniformly arranged on the side of drone body, it is characterised in that:
The drone body(1)Its side is provided with cavity body, unmanned plane wing(3)It is placed in cavity body, unmanned plane Wing(3)Downside be provided with motor(5), motor(5)Output shaft end side be connected to unmanned plane wing(3)Central shaft hole In, to realize unmanned plane wing(3)Rotation;The motor(5)Pass through connecting rod(4)With drone body(1)It is fixedly connected, Connecting rod(4)One end be provided with for fixing motor(5)Support portion;
The unmanned plane wing protective device further includes having protection net(2), protection net(2)It is symmetrically disposed on unmanned plane wing (3)Both sides up and down, protection net(2)One end pass through reinforce adjusting rod(7)It is connected to drone body(1)On;It is described anti- Protecting wire net cover(2)By buffering adjustment structure(6)Connection;
The buffering adjustment structure(6)By the branch sleeve positioned at both ends(63), elastic parts(62)And decoupling rod(61)Composition, Branch sleeve(63)Tail end be fixed on protection net(2)Top side face, branch sleeve(63)Front end be open-celled structure, and its Elastic parts is provided in hole(62), decoupling rod(61)Across branch sleeve(63)Front end, which extends, is fixed on elastic parts(62) On.
2. a kind of unmanned plane wing protective device described in claim 1, it is characterised in that:The buffering adjustment structure(6)In Branch sleeve(63)With decoupling rod(61)Form telescoping mechanism.
3. a kind of unmanned plane wing protective device as claimed in claim 1 or 2, it is characterised in that:The buffering adjustment structure(6) In every group of protection net(2)Between set at least to two, and quantity is even number.
4. a kind of unmanned plane wing protective device as claimed in claim 1 or 2, it is characterised in that:The reinforcing adjusting rod(7)'s Structure and operation principle and buffering adjustment structure(6)It is identical.
5. a kind of unmanned plane wing protective device described in claim 1, it is characterised in that:The protection net(2)Material For stainless steel wire or nylon rope.
CN201810444625.5A 2018-05-10 2018-05-10 A kind of unmanned plane wing protective device Withdrawn CN108528688A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810444625.5A CN108528688A (en) 2018-05-10 2018-05-10 A kind of unmanned plane wing protective device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810444625.5A CN108528688A (en) 2018-05-10 2018-05-10 A kind of unmanned plane wing protective device

Publications (1)

Publication Number Publication Date
CN108528688A true CN108528688A (en) 2018-09-14

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201810444625.5A Withdrawn CN108528688A (en) 2018-05-10 2018-05-10 A kind of unmanned plane wing protective device

Country Status (1)

Country Link
CN (1) CN108528688A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2021053407A1 (en) 2019-09-18 2021-03-25 Uab "Sg Consulting Baltics&By" Multi-propeller aircraft

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2021053407A1 (en) 2019-09-18 2021-03-25 Uab "Sg Consulting Baltics&By" Multi-propeller aircraft

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Application publication date: 20180914

WW01 Invention patent application withdrawn after publication