CN106240818B - Unmanned plane grabs object device - Google Patents

Unmanned plane grabs object device Download PDF

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Publication number
CN106240818B
CN106240818B CN201610705809.3A CN201610705809A CN106240818B CN 106240818 B CN106240818 B CN 106240818B CN 201610705809 A CN201610705809 A CN 201610705809A CN 106240818 B CN106240818 B CN 106240818B
Authority
CN
China
Prior art keywords
ring
iron wire
stationary ring
rotating
stationary
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.)
Expired - Fee Related
Application number
CN201610705809.3A
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Chinese (zh)
Other versions
CN106240818A (en
Inventor
张志安
盛娟红
盛明杰
徐文章
陈庆武
肖胜杰
胡致远
董培方
王腾
高逸夫
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 University of Science and Technology
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Nanjing University of Science and Technology
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 University of Science and Technology filed Critical Nanjing University of Science and Technology
Priority to CN201610705809.3A priority Critical patent/CN106240818B/en
Publication of CN106240818A publication Critical patent/CN106240818A/en
Application granted granted Critical
Publication of CN106240818B publication Critical patent/CN106240818B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/02Aircraft not otherwise provided for characterised by special use
    • 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
    • B64D1/00Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
    • B64D1/02Dropping, ejecting, or releasing articles
    • B64D1/08Dropping, ejecting, or releasing articles the articles being load-carrying devices
    • B64D1/12Releasing
    • 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

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

Abstract

The invention discloses a kind of unmanned planes to grab object device, and rotating disk is arranged on stationary disk top surface, and the two is connected by flange bearing so that the bearing rotation of rotation coil method orchid;Outer stationary ring is arranged on above rotating disk, is arranged in outer stationary ring with a circle baffle, interior rotating ring at the top of outer stationary ring, several rotating ring iron wire one end are uniformly distributed in a ring, and one end is fixedly connected with interior rotating ring, and the other end is connected with rotating disk;Several stationary ring iron wire one end are uniformly distributed in a ring, and one end is fixedly connected with outer stationary ring, and the other end is connected with stationary disk;The stationary ring iron wire and rotating ring iron wire are L-shaped, and the bottom surface of the two is in horizontal plane respectively;The output shaft of steering engine is connect with the flange bearing of rotating disk end face center, and the other end of steering engine is connect by support column with steering engine rack, and steering engine rack top surface is used to connect unmanned plane.The present invention solve the problems, such as remote-control channel in the prior art only there are one, unmanned plane landing position accuracy it is uncertain.

Description

Unmanned plane grabs object device
Technical field
The invention belongs to unmanned plane attachmentes, and in particular to a kind of unmanned plane grabs object device.
Background technology
With the needs of application and the development of aeronautical technology, the research heat to unmanned plane has been started in world wide in recent years Tide is readily transported, repairs and maintains to find out its cause, substituting manned aircraft with unmanned plane and can reduce production cost, and Without considering the physiology of people and the psychological endurance limit.Following unmanned plane all has wide practical use on military and civil. Military field is fought and is scouted using unmanned plane, it is possible to reduce the injures and deaths of personnel, moreover it is possible to have the maneuver energy of superelevation overload Power is conducive to attack and breaks away from threat.In civil field, unmanned plane can complete resources observation, disaster searching, communication relay, The heavy repetition such as environmental monitoring or the task with certain danger.
The already present transport unmanned plane function in the world is single at present, often can only solely transport cargo from one another One ground, and period can not carry out additional action, such as selectively crawl article, in locality launch article etc., And the present invention can facilitate realization crawl transport to launch spherical object compared with existing transporter.
Invention content
The purpose of the present invention is to provide a kind of unmanned planes to grab object device, solves remote-control channel in the prior art Only there are one, the uncertain problem of unmanned plane landing position accuracy.
Realize the object of the invention technical solution be:A kind of unmanned plane grabs object device, including steering engine rack, steering engine, Support column, rotating disk, interior rotating ring, stationary disk, outer stationary ring, flange bearing, several rotating ring iron wires and several are static Ring iron wire, rotating disk are arranged on stationary disk top surface, and the two is connected by flange bearing so that the bearing rotation of rotation coil method orchid; Outer stationary ring is arranged on above rotating disk, is arranged in outer stationary ring with a circle baffle, interior rotating ring at the top of outer stationary ring, if Dry root rotating ring iron wire one end is uniformly distributed in a ring, and one end is fixedly connected with interior rotating ring, and the other end is connected with rotating disk;If Dry root stationary ring iron wire one end is uniformly distributed in a ring, and one end is fixedly connected with outer stationary ring, and the other end is connected with stationary disk;Institute It states stationary ring iron wire and rotating ring iron wire is L-shaped, and the bottom surface of the two is in horizontal plane respectively;The output shaft and rotating disk of steering engine The flange bearing connection of end face center, the other end of steering engine are connect by support column with steering engine rack, and steering engine rack top surface is used for Connect unmanned plane.
The outer diameter of the interior rotating ring is not less than the internal diameter of outer stationary ring, and the outer diameter and height of interior rotating ring are no more than gear Plate.
The bending angle of the rotating ring iron wire is less than the bending angle of stationary ring iron wire, and the inflection point of rotating ring iron wire The outside diameter of composition is more than the outside diameter that the inflection point of stationary ring iron wire is formed.
Rotating ring iron wire is identical with the quantity of stationary ring iron wire.
Compared with prior art, the present invention its remarkable advantage is:(1)When grabbing object throwing object, rely only on steering engine and rotate one Slight fixed angle will not generate recoil, and unmanned plane during flying will not be caused unbalance, and whole device exquisiteness simple in structure, It is made, light weight, unmanned plane will not be caused to bear of plastics and thin wire.
(2)Only control is realized using a motor, that channel that remote controler can be utilized only surplus completely realizes control, right The requirement of manipulator can also substantially reduce.
(3)It changes to realize that grabbing object throws object using the spacing between rotating ring iron wire and stationary ring iron wire.As long as unmanned plane It drops to and takes object location, even if landing place is not allowed, but utilize the wind-force of unmanned plane rotor, sphere object also can automatically edge It to enter to grab into channel and play inside device, rotating ring iron wire is controlled to move again at this time, spherical object can follow unmanned plane Movement, takes object more rapidly in this way, and efficiency can higher.
Description of the drawings
Fig. 1 is the overall structure diagram that unmanned plane of the present invention grabs object device.
Fig. 2 is the bottom view that unmanned plane of the present invention grabs object device.
Fig. 3 grabs object device sectional view for unmanned plane of the present invention.
Specific embodiment
The present invention is described in further detail below in conjunction with the accompanying drawings.
With reference to Fig. 1 ~ Fig. 3, a kind of unmanned plane grabs object device, including steering engine rack 1, steering engine 2, support column 3, rotating disk 4, interior Rotating ring 5, rotating ring iron wire 6, stationary disk 7, outer stationary ring 8, stationary ring iron wire 9 and flange bearing 10, rotating disk 4 are arranged on quiet Only 7 top surface of disk, the two are connected by flange bearing 10 so that rotating disk 4 can be rotated around flange bearing 10.Outer stationary ring 8 is set It puts above rotating disk 4, outer 8 top of stationary ring is with a circle baffle, and interior rotating ring 5 is arranged in outer stationary ring 8, several rotations 6 one end of change iron wire is uniformly distributed in a ring, and one end is fixedly connected by bolt with interior rotating ring 5, the other end by screw thread with Rotating disk 4 is connected.Several 9 one end of stationary ring iron wire are uniformly distributed in a ring, and one end is fixed by bolt and outer stationary ring 8 to be connected It connects, the other end is connected by screw thread and stationary disk 7.The stationary ring iron wire 9 and rotating ring iron wire 6 are L-shaped, and the bottom of the two Face is in horizontal plane respectively.The output shaft of steering engine 2 is connect with the flange bearing 10 of 4 end face center of rotating disk, and the other end of steering engine 2 leads to It crosses support column 3 to connect with steering engine rack 1,1 top surface of steering engine rack is used to connect unmanned plane.
The outer diameter of the interior rotating ring 5 is not less than the internal diameter of outer stationary ring 8, and the outer diameter and height of interior rotating ring 5 do not surpass Cross baffle.
The bending angle of the rotating ring iron wire 6 is less than the bending angle of stationary ring iron wire 9, and rotating ring iron wire 6 is curved The outside diameter that break is formed is more than the outside diameter that the inflection point of stationary ring iron wire 9 is formed, convenient for positioning during rotation.
Rotating ring iron wire 6 is identical with the quantity of stationary ring iron wire 9.
The effect of baffle is to prevent interior 5 play of rotating ring, influences to rotate the rotation of iron wire ring 6.
Operation principle:
When initial, rotating ring iron wire 6 and stationary ring iron wire 9 correspond eccentric coincidence, adjacent two rotating ring iron wires 6 Between form spherical object and enter channel, land after unmanned plane reaches designated position so that Part-spherical object is logical from entering Road, which enters, grabs bullet device, when unmanned plane rotor wing rotation, forms swirling eddy, drive other spherical objects continue along channel into Enter to grab bullet device, steering engine 2 rotates by a certain angle, and drives rotating disk 4 so that rotating ring iron wire 6 deviates stationary ring iron wire 9, quite Enter channel in closing, rotating ring iron wire 6 and stationary ring iron wire 9 form arrest net at this time, and the spherical object arrested is taken back Destination.After arriving at, steering engine 2 turns round equal angular, drives rotating disk 4 so that rotating ring iron wire 6 and stationary ring iron wire 9 correspond eccentric coincidence, and spherical object is detached from from arrest net.

Claims (4)

1. a kind of unmanned plane grabs object device, it is characterised in that:Including steering engine rack(1), steering engine(2), support column(3), rotating disk (4), interior rotating ring(5), stationary disk(7), outer stationary ring(8), flange bearing(10), several rotating ring iron wires(6)With it is several Root stationary ring iron wire(9), rotating disk(4)It is arranged on stationary disk(7)Top surface, the two pass through flange bearing(10)Connection so that rotation Turntable(4)Around flange bearing(10)Rotation;Outer stationary ring(8)It is arranged on rotating disk(4)Top, outer stationary ring(8)Top carries One circle baffle, interior rotating ring(5)It is arranged on outer stationary ring(8)It is interior, several rotating ring iron wires(6)One end is uniformly divided in a ring Cloth, one end and interior rotating ring(5)It is fixedly connected, the other end and rotating disk(4)It is connected;Several stationary ring iron wires(9)One end is in Annular is uniformly distributed, one end and outer stationary ring(8)It is fixedly connected, the other end and stationary disk(7)It is connected;The stationary ring iron wire (9)With rotating ring iron wire(6)It is L-shaped, and the bottom surface of the two is in horizontal plane respectively;Steering engine(2)Output shaft and rotating disk(4) The flange bearing of end face center(10)Connection, steering engine(2)The other end pass through support column(3)With steering engine rack(1)Connection, steering engine Rack(1)Top surface is used to connect unmanned plane.
2. unmanned plane according to claim 1 grabs object device, it is characterised in that:The interior rotating ring(5)Outer diameter it is not small In outer stationary ring(8)Internal diameter, interior rotating ring(5)Outer diameter and height be no more than baffle.
3. unmanned plane according to claim 1 grabs object device, it is characterised in that:The rotating ring iron wire(6)Bending angle Degree is less than stationary ring iron wire(9)Bending angle, and rotating ring iron wire(6)Inflection point form outside diameter be more than stationary ring Iron wire(9)Inflection point form outside diameter.
4. unmanned plane according to claim 1 grabs object device, it is characterised in that:Rotating ring iron wire(6)With stationary ring iron wire (9)Quantity it is identical.
CN201610705809.3A 2016-08-22 2016-08-22 Unmanned plane grabs object device Expired - Fee Related CN106240818B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610705809.3A CN106240818B (en) 2016-08-22 2016-08-22 Unmanned plane grabs object device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610705809.3A CN106240818B (en) 2016-08-22 2016-08-22 Unmanned plane grabs object device

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CN106240818A CN106240818A (en) 2016-12-21
CN106240818B true CN106240818B (en) 2018-06-26

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Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106927047B (en) * 2017-03-22 2021-01-26 电子科技大学 Unmanned aerial vehicle grabbing device
CN107426739A (en) * 2017-08-19 2017-12-01 中国矿业大学 A kind of delivery device and its method of mine detecting airplane wireless communication node
CN109432725A (en) * 2018-11-02 2019-03-08 浙江海洋大学 A kind of unmanned thermomechanical components of auxiliary for tennis

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN202223841U (en) * 2011-09-16 2012-05-23 刘保龙 Ball catcher
CN102642620A (en) * 2012-04-11 2012-08-22 北京航空航天大学 Pneumatic free grasping/releasing system of small-sized helicopter
CN204527648U (en) * 2015-04-21 2015-08-05 刘亚敏 For the grabbing device of multi-rotor aerocraft
ES1143485U (en) * 2015-08-18 2015-09-09 Francisco Javier GARCÍA MEDINA Multifunctional device for unmanned aircraft, specifically multirotor, designed for the sampling and collection of aerobic particles (Machine-translation by Google Translate, not legally binding)
CN105173083A (en) * 2015-07-31 2015-12-23 北京邮电大学 Dropping device for rotor craft
DE102015000157A1 (en) * 2015-01-05 2016-07-07 Viktor Moor Dosing and portioning device
CN205931259U (en) * 2016-08-22 2017-02-08 南京理工大学 Unmanned aerial vehicle grabs thing device

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN202223841U (en) * 2011-09-16 2012-05-23 刘保龙 Ball catcher
CN102642620A (en) * 2012-04-11 2012-08-22 北京航空航天大学 Pneumatic free grasping/releasing system of small-sized helicopter
DE102015000157A1 (en) * 2015-01-05 2016-07-07 Viktor Moor Dosing and portioning device
CN204527648U (en) * 2015-04-21 2015-08-05 刘亚敏 For the grabbing device of multi-rotor aerocraft
CN105173083A (en) * 2015-07-31 2015-12-23 北京邮电大学 Dropping device for rotor craft
ES1143485U (en) * 2015-08-18 2015-09-09 Francisco Javier GARCÍA MEDINA Multifunctional device for unmanned aircraft, specifically multirotor, designed for the sampling and collection of aerobic particles (Machine-translation by Google Translate, not legally binding)
CN205931259U (en) * 2016-08-22 2017-02-08 南京理工大学 Unmanned aerial vehicle grabs thing device

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