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CN107416217A - A kind of unmanned plane incidental injury prevention shield - Google Patents

A kind of unmanned plane incidental injury prevention shield Download PDF

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Publication number
CN107416217A
CN107416217A CN201710646723.2A CN201710646723A CN107416217A CN 107416217 A CN107416217 A CN 107416217A CN 201710646723 A CN201710646723 A CN 201710646723A CN 107416217 A CN107416217 A CN 107416217A
Authority
CN
China
Prior art keywords
pipe fittings
unmanned plane
pipe
protective sheet
pipe fitting
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
CN201710646723.2A
Other languages
Chinese (zh)
Inventor
安秋霞
刘利波
安明琪
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.)
Henan Cool Agricultural Aviation Plant Protection Technology Co Ltd
Shenzhen Agricultural Uav Industrial Development And Application Co Ltd
Xihua Cool Agricultural Uav Industrial Park Operation Co Ltd
Original Assignee
Henan Cool Agricultural Aviation Plant Protection Technology Co Ltd
Shenzhen Agricultural Uav Industrial Development And Application Co Ltd
Xihua Cool Agricultural Uav Industrial Park Operation 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 Henan Cool Agricultural Aviation Plant Protection Technology Co Ltd, Shenzhen Agricultural Uav Industrial Development And Application Co Ltd, Xihua Cool Agricultural Uav Industrial Park Operation Co Ltd filed Critical Henan Cool Agricultural Aviation Plant Protection Technology Co Ltd
Priority to CN201710646723.2A priority Critical patent/CN107416217A/en
Publication of CN107416217A publication Critical patent/CN107416217A/en
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00Aircraft indicators or protectors not otherwise provided for
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00Type of UAV

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Catching Or Destruction (AREA)

Abstract

A kind of unmanned plane incidental injury prevention shield,Include plug-in unit,The plug-in unit is by No.1 pipe fitting and No. two pipe fittings,No. three pipe fittings,No. four pipe fittings combine,The side chain intermittent weld of the No.1 pipe fitting and No. two pipe fittings is combined into No.1 component,The side chain intermittent weld of No. three pipe fittings and No. four pipe fittings is combined into No. two components,The No.1 components welding is in top surface on No. two components,And No.1 component and No. two components are in 90 ° of installations,The No.1 pipe fitting and No. two pipe fittings,No. three pipe fittings,Interspersed bar is provided with No. four pipe fittings,The right-hand member of the interspersed bar is provided with protective sheet,The protective sheet is semi arch laminated structure,The medial surface centre position of the protective sheet is provided with fixing groove,The right-hand member of the interspersed bar is fixedly connected with fixing groove,Spring is provided with interspersed bar between the plug-in unit and fixing groove,The present invention can be good at protecting unmanned plane,Reduce the loss hit and brought,It is easy for installation,Cost is relatively low.

Description

A kind of unmanned plane incidental injury prevention shield
Technical field
The present invention relates to a kind of incidental injury prevention shield, and it particularly relates to a kind of unmanned plane incidental injury prevention shield.
Background technology
With the development of society, the raising of living standards of the people, the environment that people are lived to oneself has required, the modern times Society rapid development make people to society cognition it is broader, people thirst for explore sky, it is desirable to hovered as bird and Sky, then we have an aircraft, anyone has the possibility for the sky that flies up into the sky to but not, and it is winged not to be that everyone can drive Machine, but this is without prejudice to the our own imagination, unmanned plane are that people fly up into the sky sky, explore an invention of sky, it is not necessary to Flower how much, it is possible to fly to sky, though existing unmanned plane is not particularly expensive, but poor people common people nor Everybody can possess, and flying to sky unmanned plane similarly needs safeguard measure, be easy to bump against large-scale build if operation is bad Thing or birds are built, cause machine to ruin, but existing unmanned plane does not have corresponding safeguard measure, it is easy to occur hitting damage Thing occur.
The content of the invention
Damage is easily hit for the above-mentioned unmanned plane being previously mentioned and arrives others with misoperation accidental injury, causes damage and endangers The problem of, there is provided a kind of unmanned plane incidental injury prevention shield.
In order to solve the problems, such as it is above-mentioned be previously mentioned, a kind of unmanned plane incidental injury prevention shield includes plug-in unit, the plug-in unit by No.1 pipe fitting combines with No. two pipe fittings, No. three pipe fittings, No. four pipe fittings, and the side of the No.1 pipe fitting and No. two pipe fittings is arranged side by side Welding is combined into No.1 component, and the side chain intermittent weld of No. three pipe fittings and No. four pipe fittings is combined into No. two components, and described one Number components welding is in top surface on No. two components, and No.1 component and No. two components are managed in 90 ° of installations, the No.1 pipe fitting with No. two Part, No. three pipe fittings, interspersed bar is provided with No. four pipe fittings, the right-hand member of the interspersed bar is provided with protective sheet, the protective sheet For semi arch laminated structure, the medial surface centre position of the protective sheet is provided with fixing groove, and the right-hand member of the interspersed bar is with consolidating Determine groove to be fixedly connected, spring is provided with the interspersed bar between the plug-in unit and fixing groove, the left end side of the interspersed bar is set It is equipped with fix bar.
The No.1 pipe fitting and No. two pipe fittings, No. three pipe fittings, No. four pipe fittings are cylindrical structure, and it is hollow knot that it is internal Structure.
The protective sheet is soft plastic material.
The No.1 pipe fitting and No. two pipe fittings, No. three pipe fittings, the right-hand member of No. four pipe fittings are provided with protective sheet, described four Protective sheet is combined into circular ring structure.
The beneficial effect comprise that:Existing unmanned plane is almost completely without safeguard measure, when meeting tall and big building Thing or be possible to when having bought electric power hide it is too late or directly from falling from high altitude when, cause to damage, cause any property loss, and this hair Bright is a kind of safeguard measure, and the present invention sets and is installed on the bottom surface of unmanned plane central controller shell, and four protective sheets exist Fenced up one of protective cover around unmanned plane, and unmanned plane is prevented while protecting unmanned plane by misoperation, causes the feelings accidentally injured Condition, intert and be provided with spring on bar, when unmanned plane strikes building or people, spring can play a part of buffering, give nothing Human-machine operation person certain operation time, bigger loss and harm are avoided, and protective sheet is combined into the anti-of annular shape Protection structure, either hit from that direction, can play a very good protection, so more to the guarantor of unmanned plane Shield is more comprehensive.
Generally the present invention can be good at protecting unmanned plane, reduces and hits the loss that brings, easy for installation, cost compared with It is low.
Brief description of the drawings
Fig. 1 is top surface structure connection diagram of the present invention.
Embodiment
Below in conjunction with the accompanying drawings to embodiments of the invention further instruction.
Embodiment 1:
A kind of unmanned plane incidental injury prevention shield, include plug-in unit 1, the plug-in unit 1 is by 3, No. three pipes of No.1 pipe fitting 2 and No. two pipe fittings 4, No. four pipe fittings 5 of part combine, and the side chain intermittent weld of the No.1 pipe fitting 2 and No. two pipe fittings 3 is combined into No.1 component, institute The side chain intermittent weld for stating No. three pipe fittings 4 and No. four pipe fittings 5 is combined into No. two components, and the No.1 components welding is in No. two components Upper top surface, and No.1 component and No. two components are in 90 ° of installations, the No.1 pipe fitting 2 and No. two pipe fittings 4, four of pipe fitting 3, three Interspersed bar 6 is provided with pipe fitting 5, the right-hand member of the interspersed bar 6 is provided with protective sheet 7, and the protective sheet 7 is semicircle arc sheet Structure, the medial surface centre position of the protective sheet 7 are provided with fixing groove 8, and the right-hand member of the interspersed bar 6 is fixed with fixing groove 8 Connect, be provided with spring 9 on the interspersed bar 6 between the plug-in unit 1 and fixing groove 8, the left end side of the interspersed bar 6 is provided with Fix bar 10.
The No.1 pipe fitting 2 and No. two pipe fittings 5 of pipe fitting 4, four of pipe fitting 3, three are cylindrical structure, and it is internal for sky Core structure.
The protective sheet 7 is soft plastic material.
The right-hand member of the No.1 pipe fitting 2 and No. two pipe fittings 3, No. three pipe fittings, 4, No. four pipe fittings 5 is provided with protective sheet 7, institute State four protective sheets 7 and be combined into circular ring structure.
The present invention is when in use:The present invention is a kind of protective cover, for protecting unmanned plane misoperation to cause damage and missing The situation of people is hurt, first to check whether all parts are perfect, and whether the quantity of all parts is enough, and these problems are complete using preceding After portion checks, you can assembling, make in interspersed bar insertion plug-in unit, four interspersed bars are respectively interposed manages into No.1 pipe fitting and No. two Part, No. three pipe fittings, No. four pipe fittings, it is in decussate texture that four interspersed bars, which intert and entered rear in plug-in unit, can be installed after interspersed Protective sheet, four protective sheets are in toroidal protection unmanned plane, and protective sheet sheet can more protect nobody as soft plastic material Machine, the impulsive force of unmanned plane is reduced, reduce misoperation, the harm and loss brought.
The present invention can be good at protecting unmanned plane, reduce harm and loss.

Claims (4)

1. a kind of unmanned plane incidental injury prevention shield, includes plug-in unit, it is characterised in that:The plug-in unit is managed by No.1 pipe fitting and No. two Part, No. three pipe fittings, No. four pipe fittings combine, and the side chain intermittent weld of the No.1 pipe fitting and No. two pipe fittings is combined into No.1 group Part, the side chain intermittent weld of No. three pipe fittings and No. four pipe fittings are combined into No. two components, and the No.1 components welding is in No. two Top surface on component, and No.1 component and No. two components are in 90 ° of installations, the No.1 pipe fitting and No. two pipe fittings, No. three pipe fittings, No. four Interspersed bar is provided with pipe fitting, the right-hand member of the interspersed bar is provided with protective sheet, and the protective sheet is semi arch laminated structure, The medial surface centre position of the protective sheet is provided with fixing groove, and the right-hand member of the interspersed bar is fixedly connected with fixing groove, described Spring is provided with interspersed bar between plug-in unit and fixing groove, the left end side of the interspersed bar is provided with fix bar.
A kind of 2. unmanned plane incidental injury prevention shield according to claim 1, it is characterised in that:The No.1 pipe fitting and No. two pipes Part, No. three pipe fittings, No. four pipe fittings are cylindrical structure, and it is hollow-core construction that it is internal.
A kind of 3. unmanned plane incidental injury prevention shield according to claim 1, it is characterised in that:The protective sheet is soft plasticity material Matter.
A kind of 4. unmanned plane incidental injury prevention shield according to claim 1, it is characterised in that:The No.1 pipe fitting and No. two pipes Part, No. three pipe fittings, the right-hand member of No. four pipe fittings are provided with protective sheet, and four protective sheets are combined into circular ring structure.
CN201710646723.2A 2017-08-01 2017-08-01 A kind of unmanned plane incidental injury prevention shield Pending CN107416217A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710646723.2A CN107416217A (en) 2017-08-01 2017-08-01 A kind of unmanned plane incidental injury prevention shield

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710646723.2A CN107416217A (en) 2017-08-01 2017-08-01 A kind of unmanned plane incidental injury prevention shield

Publications (1)

Publication Number Publication Date
CN107416217A true CN107416217A (en) 2017-12-01

Family

ID=60436417

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201710646723.2A Pending CN107416217A (en) 2017-08-01 2017-08-01 A kind of unmanned plane incidental injury prevention shield

Country Status (1)

Country Link
CN (1) CN107416217A (en)

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2572490A1 (en) * 1984-10-31 1986-05-02 Alkan R & Cie SAFETY CONNECTOR FOR SEPARABLE OR WIDTHABLE ELEMENT WITH AUTOMATIC RETRACTION DEVICE
CN205366090U (en) * 2016-01-12 2016-07-06 南充驭云创新科技有限公司 Many rotors unmanned aerial vehicle with protection device
US20160200415A1 (en) * 2015-01-08 2016-07-14 Robert Stanley Cooper Multi-rotor safety shield
CN205525011U (en) * 2016-03-11 2016-08-31 零度智控(北京)智能科技有限公司 Protect oar quick assembly disassembly structure
CN205770161U (en) * 2016-05-30 2016-12-07 龙岩市经纬测绘有限公司 A kind of unmanned plane anti-collision protection device
CN205989812U (en) * 2015-06-25 2017-03-01 瑞德利斯技术公司 Many rotor wing unmanned aerial vehicles
CN207225677U (en) * 2017-08-01 2018-04-13 西华酷农无人机产业园运营有限公司 A kind of unmanned plane incidental injury prevention shield

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2572490A1 (en) * 1984-10-31 1986-05-02 Alkan R & Cie SAFETY CONNECTOR FOR SEPARABLE OR WIDTHABLE ELEMENT WITH AUTOMATIC RETRACTION DEVICE
US20160200415A1 (en) * 2015-01-08 2016-07-14 Robert Stanley Cooper Multi-rotor safety shield
CN205989812U (en) * 2015-06-25 2017-03-01 瑞德利斯技术公司 Many rotor wing unmanned aerial vehicles
CN205366090U (en) * 2016-01-12 2016-07-06 南充驭云创新科技有限公司 Many rotors unmanned aerial vehicle with protection device
CN205525011U (en) * 2016-03-11 2016-08-31 零度智控(北京)智能科技有限公司 Protect oar quick assembly disassembly structure
CN205770161U (en) * 2016-05-30 2016-12-07 龙岩市经纬测绘有限公司 A kind of unmanned plane anti-collision protection device
CN207225677U (en) * 2017-08-01 2018-04-13 西华酷农无人机产业园运营有限公司 A kind of unmanned plane incidental injury prevention shield

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SE01 Entry into force of request for substantive examination
WD01 Invention patent application deemed withdrawn after publication
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Application publication date: 20171201