CN107745805A - A kind of suspension type unmanned plane - Google Patents

A kind of suspension type unmanned plane Download PDF

Info

Publication number
CN107745805A
CN107745805A CN201710876803.7A CN201710876803A CN107745805A CN 107745805 A CN107745805 A CN 107745805A CN 201710876803 A CN201710876803 A CN 201710876803A CN 107745805 A CN107745805 A CN 107745805A
Authority
CN
China
Prior art keywords
rotor
unmanned plane
main body
motor
connector
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
CN201710876803.7A
Other languages
Chinese (zh)
Inventor
刘凤英
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.)
Nanjing Lvzhicheng Patent Technology Development Co Ltd
Original Assignee
Nanjing Lvzhicheng Patent Technology Development 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 Nanjing Lvzhicheng Patent Technology Development Co Ltd filed Critical Nanjing Lvzhicheng Patent Technology Development Co Ltd
Priority to CN201710876803.7A priority Critical patent/CN107745805A/en
Publication of CN107745805A publication Critical patent/CN107745805A/en
Pending legal-status Critical Current

Links

Classifications

    • 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
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D9/00Equipment for handling freight; Equipment for facilitating passenger embarkation or the like
    • 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
    • B64U2101/00UAVs specially adapted for particular uses or applications
    • B64U2101/60UAVs specially adapted for particular uses or applications for transporting passengers; for transporting goods other than weapons

Abstract

The present invention provides a kind of suspension type unmanned plane, including unmanned plane main body, rotor support, rotor motor, rotor blade, retainer ring, connector and suspension ring, the unmanned plane main body is box-like, the front and rear sides of the unmanned plane main body are respectively provided with a rotor support, rotor motor is installed in the outboard end of the rotor support, each corresponding 24 rotor blades of rotor motor, the rotor blade is arranged on the rotating shaft outer wall of rotor motor, the rotor blade angularly around corresponding rotor motor rotating shaft center line one week, the rotor mid-stent is set with retainer ring, there is connecting line below the retainer ring, the connecting line lower end is connected by connector with suspension ring.The present invention provides a kind of suspension type unmanned plane, should be the characteristics of unmanned plane utilize existing rotor wing unmanned aerial vehicle, and design corresponding suspension ring to match somebody with somebody nest of boxes formula top-hung and be hooked into capable transport, to reach corresponding cargo transport effect.

Description

A kind of suspension type unmanned plane
Technical field
The present invention relates to unmanned plane field, more particularly to a kind of suspension type unmanned plane.
Background technology
With the continuous development of society, the continuous progress in epoch, unmanned plane correlation technique develops extremely rapid, wherein shipping Transport is the quickest with Development of UAV, and conventional cargo unmanned plane often uses box transport, but this transport needs nobody Machine is attached to thereon, as the continuous development of location technology can contemplate by setting hook to enter by hook mode on freight container Row hanging transport.
The content of the invention
In order to solve above-mentioned problem, the present invention provides a kind of suspension type unmanned plane, should be utilized for unmanned plane existing The characteristics of rotor wing unmanned aerial vehicle, corresponding suspension ring are designed to match somebody with somebody nest of boxes formula top-hung and are hooked into capable transport, to reach corresponding goods Effect is transported, for up to this purpose, the present invention provides a kind of suspension type unmanned plane, including unmanned plane main body, rotor support, rotor electricity Machine, rotor blade, retainer ring, connector and suspension ring, the unmanned plane main body are box-like, the front and rear sides of the unmanned plane main body One rotor support is respectively installed, rotor motor is installed in the outboard end of the rotor support, each rotor motor is corresponding 2-4 rotor blade, the rotor blade are arranged on the rotating shaft outer wall of rotor motor, and the rotor blade angularly revolves around corresponding The center line of the rotating shaft of wing motor one week, the rotor mid-stent are set with retainer ring, have connecting line below the retainer ring, The connecting line lower end is connected by connector with suspension ring.
Further improvement of the present invention, the front and rear side of the unmanned plane main body are installed with infrared inductor, set sense Device is answered to be monitored with surrounding environment.
Further improvement of the present invention, the unmanned plane bottom part body are provided with a pair of inverted U-shaped landing gears, for the ease of drop Fall to set above landing gear.
Further improvement of the present invention, the connector are detachable detachable connecting piece, and so design can be according to need Change suspension parts.
The present invention provides a kind of suspension type unmanned plane, and the unmanned plane has suspension ring in rotor support Design, can lead to article Cross hook and hang over and transported accordingly below, compared with Traditional Transportation, this transport container is not easy to drop, and transport is stable Property is more preferable, and carrying capacity is stronger, is particularly suitable for the long-distance transport of relatively large casing.
Brief description of the drawings
Fig. 1 is schematic diagram of the present invention;
Component in figure is:
1st, unmanned plane main body;2nd, rotor support;3rd, rotor motor;4th, rotor blade;5th, infrared inductor;6th, inverted U-shaped landing Frame;7th, retainer ring;8th, connector;9th, suspension ring.
Embodiment
The present invention is described in further detail with embodiment below in conjunction with the accompanying drawings:
The present invention provides a kind of suspension type unmanned plane, should be the characteristics of unmanned plane utilize existing rotor wing unmanned aerial vehicle, and design is corresponding Suspension ring are hooked into capable transport to match somebody with somebody nest of boxes formula top-hung, to reach corresponding cargo transport effect.
The application provides a kind of embodiment.A kind of suspension type unmanned plane as shown in Figure 1, including unmanned plane main body 1, rotor Support 2, rotor motor 3, rotor blade 4, retainer ring 7, connector 8 and suspension ring 9, the unmanned plane main body 1 are box-like, the nothing The front and rear sides of man-machine main body 1 are respectively provided with a rotor support 2, and rotor is provided with the outboard end of the rotor support 2 Motor 3, the corresponding 2-4 rotor blade 4 of each rotor motor 3, the rotor blade 4 are arranged on the rotating shaft outer wall of rotor motor 3, The rotor blade 4 angularly around corresponding rotor motor 3 rotating shaft center line one week, be set with the middle part of the rotor support 2 There is connecting line retainer ring 7, the lower section of retainer ring 7, and the connecting line lower end is connected by connector 8 with suspension ring 9.
The application provides a kind of specific embodiment, a kind of suspension type unmanned plane, including unmanned plane main body 1, rotor support 2, Rotor motor 3, rotor blade 4, retainer ring 7, connector 8 and suspension ring 9, the unmanned plane main body 1 are box-like, the unmanned owner The front and rear side of body is installed with infrared inductor, sets inductor to be monitored with surrounding environment, the unmanned plane main body Bottom is provided with a pair of inverted U-shaped landing gears, and above landing gear is set for the ease of landing, and front and rear the two of the unmanned plane main body 1 Side is respectively provided with a rotor support 2, and rotor motor 3, each rotor motor are provided with the outboard end of the rotor support 2 3 corresponding 2-4 rotor blades 4, the rotor blade 4 are arranged on the rotating shaft outer wall of rotor motor 3, the isogonism of rotor blade 4 The center line one week around the rotating shaft of corresponding rotor motor 3 is spent, retainer ring 7, the retainer ring are set with the middle part of the rotor support 2 There is connecting line 7 lower sections, and the connecting line lower end is connected by connector 8 with suspension ring 9, and the connector is detachable split type company Fitting, so design can change suspension parts as needed.
The above described is only a preferred embodiment of the present invention, it is not the limit for making any other form to the present invention System, and any modification made according to technical spirit of the invention or equivalent variations, still fall within present invention model claimed Enclose.

Claims (4)

1. a kind of suspension type unmanned plane, including unmanned plane main body(1), rotor support(2), rotor motor(3), rotor blade(4)、 Retainer ring(7), connector(8)And suspension ring(9), it is characterised in that:The unmanned plane main body(1)To be box-like, the unmanned owner Body(1)Front and rear sides one rotor support is respectively installed(2), the rotor support(2)Outboard end on rotor is installed Motor(3), each rotor motor(3)Corresponding 2-4 rotor blade(4), the rotor blade(4)Installed in rotor motor(3) Rotating shaft outer wall, the rotor blade(4)Angularly around corresponding rotor motor(3)Rotating shaft center line one week, the rotor Support(2)Middle part is set with retainer ring(7), the retainer ring(7)There is connecting line lower section, and the connecting line lower end passes through connector (8)With suspension ring(9)It is connected.
A kind of 2. suspension type unmanned plane according to claim 1, it is characterised in that:The unmanned plane main body(1)It is front and rear End is respectively provided with an infrared inductor(5).
A kind of 3. suspension type unmanned plane according to claim 1, it is characterised in that:The unmanned plane main body(1)Pacify bottom Equipped with a pair of inverted U-shaped landing gears(6).
A kind of 4. suspension type unmanned plane according to claim 1, it is characterised in that:The connector(8)For detachable point Body formula connector.
CN201710876803.7A 2017-09-25 2017-09-25 A kind of suspension type unmanned plane Pending CN107745805A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710876803.7A CN107745805A (en) 2017-09-25 2017-09-25 A kind of suspension type unmanned plane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710876803.7A CN107745805A (en) 2017-09-25 2017-09-25 A kind of suspension type unmanned plane

Publications (1)

Publication Number Publication Date
CN107745805A true CN107745805A (en) 2018-03-02

Family

ID=61255095

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201710876803.7A Pending CN107745805A (en) 2017-09-25 2017-09-25 A kind of suspension type unmanned plane

Country Status (1)

Country Link
CN (1) CN107745805A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110844057A (en) * 2019-11-28 2020-02-28 湖南库里斯智能科技有限公司 Multi-functional environmental protection unmanned aerial vehicle that patrols and examines

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN204236774U (en) * 2014-11-25 2015-04-01 南京机电职业技术学院 Rotary wind type unmanned plane is used in a kind of transport
CN105035336A (en) * 2015-07-23 2015-11-11 国网辽宁省电力有限公司葫芦岛供电公司 Unmanned aerial vehicle hoisting device for electric transmission line parts
CN204822090U (en) * 2015-06-23 2015-12-02 深圳飞豹航天航空科技有限公司 Unmanned aerial vehicle
CN106477035A (en) * 2016-11-29 2017-03-08 江苏新思维信息系统工程有限公司 A kind of express mail transport unmanned plane

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN204236774U (en) * 2014-11-25 2015-04-01 南京机电职业技术学院 Rotary wind type unmanned plane is used in a kind of transport
CN204822090U (en) * 2015-06-23 2015-12-02 深圳飞豹航天航空科技有限公司 Unmanned aerial vehicle
CN105035336A (en) * 2015-07-23 2015-11-11 国网辽宁省电力有限公司葫芦岛供电公司 Unmanned aerial vehicle hoisting device for electric transmission line parts
CN106477035A (en) * 2016-11-29 2017-03-08 江苏新思维信息系统工程有限公司 A kind of express mail transport unmanned plane

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110844057A (en) * 2019-11-28 2020-02-28 湖南库里斯智能科技有限公司 Multi-functional environmental protection unmanned aerial vehicle that patrols and examines

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SE01 Entry into force of request for substantive examination
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Application publication date: 20180302

WD01 Invention patent application deemed withdrawn after publication