CN110239704A - UAV flight folds arm high-altitude installation safe anti-falling hook and its application method - Google Patents

UAV flight folds arm high-altitude installation safe anti-falling hook and its application method Download PDF

Info

Publication number
CN110239704A
CN110239704A CN201910540041.2A CN201910540041A CN110239704A CN 110239704 A CN110239704 A CN 110239704A CN 201910540041 A CN201910540041 A CN 201910540041A CN 110239704 A CN110239704 A CN 110239704A
Authority
CN
China
Prior art keywords
arm
folds
unmanned plane
hanger bulk
hook
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.)
Granted
Application number
CN201910540041.2A
Other languages
Chinese (zh)
Other versions
CN110239704B (en
Inventor
杨亮
孙逊
蔡澍雨
郑瑞东
宋晓明
姜立超
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.)
Charged Operation Branch of Yunnan Power Grid Co Ltd
Original Assignee
Charged Operation Branch of Yunnan Power Grid 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 Charged Operation Branch of Yunnan Power Grid Co Ltd filed Critical Charged Operation Branch of Yunnan Power Grid Co Ltd
Priority to CN201910540041.2A priority Critical patent/CN110239704B/en
Publication of CN110239704A publication Critical patent/CN110239704A/en
Application granted granted Critical
Publication of CN110239704B publication Critical patent/CN110239704B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/30Parts of fuselage relatively movable to reduce overall dimensions of aircraft
    • 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
    • B64D47/00Equipment not otherwise provided for
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00UAVs specially adapted for particular uses or applications
    • B64U2101/30UAVs specially adapted for particular uses or applications for imaging, photography or videography
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/40Weight reduction

Abstract

The present invention relates to unmanned plane equipment technical fields, specially UAV flight folds arm high-altitude installation safe anti-falling hook and its application method, including drone body, drone body carries video camera, the bottom center of drone body is provided with fold mechanism, the top of first folding arm is connected with the first damping joint, the bottom end that third folds arm is provided with disengaging buckle, third folds arm and has snapped connection removal hook by being detached from, hitch gear is connected in removal hook, hitch gear includes hanger bulk, is connected in hanger bulk and fetches ring.The present invention is suitable for the installment work linked up with, hanger bulk is hung on target hanging point by unmanned plane, allow hanging position more free, the place that personnel can not directly contact can hang hanger bulk, whole operation does not need the position that operator is in dangerous, so that the personal safety of operator is protected, and easy to operate, it is suitable for promoting the use of.

Description

UAV flight folds arm high-altitude installation safe anti-falling hook and its application method
Technical field
The present invention relates to unmanned plane equipment technical field, specially UAV flight folds arm high-altitude installation safe anti-falling and hangs Hook and its application method.
Background technique
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, is using radio robot and to provide for oneself The not manned aircraft of presetting apparatus manipulation, or fully or intermittently automatically operated by car-mounted computer.
Operator generallys use the artificial mode for directly connecting hook with hanging point when installing hook at present, such The position that method causes the installation site of hook lower, little higher, operator require to borrow the climbing tools such as ladder, no Only operational hazards, while some more dangerously steep positions are all unable to complete the suspension work for hook by ladder, for this purpose, needing Designing one kind can be in the case where needing operator and directly contacting, the device that hook is connect with hanging point, to make The installation site that must be linked up with is more changeable and free.In consideration of it, we, which provide UAV flight, folds arm high-altitude installation safety Anti-fall hook and its application method.
Summary of the invention
The purpose of the present invention is to provide UAV flights to fold arm high-altitude installation safe anti-falling hook and its application method, To solve to propose nowadays to link up in above-mentioned background technique to connect with hanging point to carry out contact installation, operational hazards by operator The problem of.
To achieve the above object, the invention provides the following technical scheme:
UAV flight folds arm high-altitude installation safe anti-falling hook, including unmanned plane, the unmanned plane carry video camera, The bottom center of unmanned plane is provided with fold mechanism, and the fold mechanism includes first folding arm and second and folding arm, and described the The top of one folding arm is connected with the first damping joint, and described first, which folds arm, passes through the bottom surface in the first damping joint and unmanned plane Center connection, the top and bottom end of the second folding arm are respectively connected with the second damping joint, and described second folds the top of arm It is connect by the second damping joint with the bottom end of the first folding arm, the described second bottom end for folding arm is closed by the second damping Section is connected with third and folds arm, and the bottom end that the third folds arm is provided with disengaging buckle, and the third folds arm and passes through disengaging Removal hook has been snapped connection, hitch gear is connected in the removal hook, the hitch gear includes hanger bulk, the hook It is connected on ontology and fetches ring, be equipped with folded wall joint lock in the middle part of the first folding arm and the second folding arm.
Preferably, the first damping joint damps joint using twin shaft.
Preferably, the top of the second folding arm and the second damping joint of bottom end are uniaxial damping joint.
Preferably, the hanger bulk is equipped with guide wheel far from the one end for fetching ring.
UAV flight folds the application method of arm high-altitude installation safe anti-falling hook, the user including safety rope mounting The application method of method and safety rope recycling.
Preferably, the application method of the safety rope mounting includes the following steps:
S11: prepare unmanned plane and associated components before work;
S12: corresponding traction rope, safety rope and hanger bulk are chosen according to the height of target hanging point;
S13: the disengaging that hanger bulk upper end folds arm lower end with third is snapped connection;
S14: it opens the folded wall joint that first folds on arm and the second folding arm and locks;
S15: control unmanned plane takes off, and first, which folds arm, the second folding arm and third, folds arm under gravity certainly Dynamic expansion;
S16: unmanned plane flies to target position, and slow falling head returns picture by video camera;
S17: adjusting the aperture position of hanger bulk, when the opening of hanger bulk is caught in hanging point, controls unmanned plane forward Flight is detached from hanger bulk and fold mechanism;
S18: after hanger bulk falls into hanging point, unmanned plane returns to landing;
S19: traction rope is substituted for safety rope.
Preferably, the application method of the safety rope recycling includes the following steps:
S21: safety rope is substituted for traction rope;
S22: removal hook is folded into arm lower end with third and is connect;
S23: unmanned plane takes off and slowly increases, and first, which folds arm, the second folding arm and third, folds arm in gravity Lower Automatic-expanding;
S24: unmanned plane flies to target position, and slow falling head returns picture by camera;
S25: adjusting the position of removal hook, and removal hook is inserted into fetching in ring above hanger bulk, controls nobody upwards Machine takes out hanger bulk;
S26: unmanned plane carries hanger bulk landing.
Preferably, the first folding arm, the second folding arm and third fold arm and cannot be fully extended under the effect of gravity It when position, is manually moved, is allowed in unfolded state.
Compared with prior art, the beneficial effects of the present invention are: this UAV flight, which folds arm high-altitude, installs safe anti-falling Hanger bulk is hung on target hanging point by unmanned plane, is made suitable for the installment work linked up with by hook and its application method Obtaining hanging position can more freely, and the place that personnel can not directly contact can hang hanger bulk, and whole operation is not required to Operator is wanted to be in dangerous position, so that the personal safety of operator is protected, and easy to operate, it is suitable for promoting It uses.
Detailed description of the invention
Fig. 1 is that the structural schematic diagram connecting under arm bending state with hanger bulk is folded in the present invention;
Fig. 2 is that the structural schematic diagram connecting under arm unfolded state with hanger bulk is folded in the present invention;
Fig. 3 is the structural schematic diagram for folding under arm bending state and fetching hook connects in the present invention;
Fig. 4 is the structural schematic diagram for folding under arm unfolded state and fetching hook connects in the present invention;
Fig. 5 is the main view for folding arm in the present invention and connecting with hanger bulk;
Fig. 6 is to fold arm in the present invention and fetch the main view of hook connects;
Fig. 7 is the stereoscopic schematic diagram of hanger bulk in the present invention.
In figure: 1, unmanned plane;2, fold mechanism;3, hanger bulk;4, removal hook;5, ring is fetched;6, the first damping joint; 7, folded wall joint is locked;8, first arm is folded;9, second arm is folded;10, the second damping joint;11, third folds arm;12, it leads Wheel;13, it is detached from buckle;14, hitch gear.
Specific embodiment
Below in conjunction with the embodiment of the present invention, technical scheme in the embodiment of the invention is clearly and completely described, Obviously, described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.Based in the present invention Embodiment, every other embodiment obtained by those of ordinary skill in the art without making creative efforts, all Belong to the scope of protection of the invention.
In the description of the present invention, it is to be understood that, term " center ", " longitudinal direction ", " transverse direction ", " length ", " width ", " thickness ", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outside", " up time The orientation or positional relationship of the instructions such as needle ", " counterclockwise " is to be based on the orientation or positional relationship shown in the drawings, and is merely for convenience of The description present invention and simplified description, rather than the equipment of indication or suggestion meaning or element must have a particular orientation, with spy Fixed orientation construction and operation, therefore be not considered as limiting the invention.
Please refer to Fig. 1-7, the present invention the following technical schemes are provided:
UAV flight folds arm high-altitude installation safe anti-falling hook, as Figure 1-Figure 4, including unmanned plane 1, unmanned plane 1 included video camera, the bottom center of unmanned plane 1 are provided with fold mechanism 2, and fold mechanism 2 includes the first folding arm 8 and the second folding Folded arm 9, the top of the first folding arm 8 are connected with the first damping joint 6, and the first damping joint 6 damps joint using twin shaft, can be with For buffering the collision in the direction unmanned plane 1roll and pith, and make the first folding arm 8 that can damp strength with free movement It is adjustable, while inside can install rebounding mechanism, convenient for the recycling of device.
Further, as shown in figure 5, first folds the company, bottom center that arm 8 damps joint 6 and unmanned plane 1 by first It connects, the top and bottom end of the second folding arm 9 are respectively connected with the second damping joint 10, and second folds the of the top of arm 9 and bottom end Two damping joints 10 are uniaxial damping joint, and gravity can be used for buffering when being unfolded, and prevent development rate too fast, unmanned plane 1 Unstable, internal damping strength is adjustable, while inside can install rebounding mechanism, convenient for the recycling of device.
Specifically, as shown in fig. 6, the second top for folding arm 9 folds the bottom of arm 8 by the second damping joint 10 and first End connection, the bottom end of the second folding arm 9 are connected with third by the second damping joint 10 and fold arm 11, and third folds the bottom of arm 11 End is provided with disengaging buckle 13, and being detached from and buckling 13 full name is that overload is detached from buckle, when hanger bulk 3 and the stuck situation of hanging point are sent out When raw, unmanned plane 1, which can be shaken off, to be left, and is detached from buckle 13 and is set as standard interface, can be with 3 He of Fast Installation hanger bulk Removal hook 4.
In addition, being connected in removal hook 4 as shown in fig. 7, third, which folds arm 11,13 is connected with removal hook 4 by being detached from buckle There is a hitch gear 14, hitch gear 14 includes hanger bulk 3, is connected in hanger bulk 3 and fetches ring 5, and first folds arm 8 and the Folded wall joint lock 7 is equipped in the middle part of two-fold arm 9.The first of fold mechanism 2 folds arm 8, second and folds during transportation Arm 9 and third fold arm 11 and can constantly shake, at this time in order to guarantee transport when whole device stabilization, pass through setting folding Folded shoulder joint lock 7 folds arm 8 for first and the second folding arm 9 is fixed, to ensure that the stabilization in whole device transportational process.
It is worth noting that hanger bulk 3 is equipped with guide wheel 12 far from the one end for fetching ring 5, can be incited somebody to action by guide wheel 12 Safety rope and traction rope are connect with hanger bulk 3.
UAV flight of the invention folds the application method of arm high-altitude installation safe anti-falling hook, including safety rope mounting Application method and safety rope recycling application method.
Specifically, the application method of safety rope mounting includes the following steps:
S11: prepare unmanned plane 1 and associated components before work;
S12: corresponding traction rope, safety rope and hanger bulk 3 are chosen according to the height of target hanging point;
S13: 3 upper end of hanger bulk is connect with the disengaging buckle 13 that third folds arm lower end;
S14: it opens the folded wall joint that first folds on arm 8 and the second folding arm 9 and locks 7;
S15: control unmanned plane 1 takes off, and first, which folds arm, the second folding arm and third, folds arm under gravity certainly Dynamic expansion;
S16: unmanned plane 1 flies to target position, and slow falling head returns picture by video camera;
S17: the aperture position for adjusting hanger bulk 3 controls forward nobody when the opening of hanger bulk 3 is caught in hanging point Machine 1 flies, and is detached from hanger bulk 3 and fold mechanism 2;
S18: after hanger bulk 3 falls into hanging point, unmanned plane 1 returns to landing;
S19: traction rope is substituted for safety rope.
Further, the application method of safety rope recycling includes the following steps:
S21: safety rope is substituted for traction rope;
S22: removal hook 4 is folded into 11 lower end of arm with third and is connect;
S23: unmanned plane 1 takes off and slowly increases, and first, which folds arm 8, second, folds arm 9 and third folding arm 11 in gravity Act on lower Automatic-expanding;
S24: unmanned plane 1 flies to target position, and slow falling head returns picture by camera;
S25: removal hook 4 is inserted into fetching in ring 5 above hanger bulk 3, controlled upwards by the position of adjustment removal hook 4 Unmanned plane 1 takes out hanger bulk 3;
S26: unmanned plane 1 carries hanger bulk 3 and lands.
It is worth noting that, the first folding arm 8, second folds arm 9 and third folding arm 11 under the effect of gravity cannot be complete It when expanding in place entirely, is manually moved, is allowed in unfolded state.
UAV flight of the invention folds arm high-altitude installation safe anti-falling hook suitable for the installment work linked up with, leads to It crosses unmanned plane 1 to hang over hanger bulk 3 on target hanging point, allows hanging position more free, personnel can not directly contact Place can hang hanger bulk 3, whole operation do not need the position that operator is in dangerous, so that operator Personal safety is protected, and easy to operate, is suitable for promoting the use of.
The basic principles, main features and advantages of the present invention have been shown and described above.The technology of the industry For personnel it should be appreciated that the present invention is not limited to the above embodiments, described in the above embodiment and specification is only the present invention Preference, be not intended to limit the invention, without departing from the spirit and scope of the present invention, the present invention also has various Changes and improvements, these changes and improvements all fall within the protetion scope of the claimed invention.The claimed scope of the invention is by institute Attached claims and its equivalent thereof.

Claims (8)

1. UAV flight folds arm high-altitude installation safe anti-falling hook, including unmanned plane (1), the unmanned plane (1) is included to be taken the photograph Camera, it is characterised in that: the bottom center of unmanned plane (1) is provided with fold mechanism (2), and the fold mechanism (2) includes first It folding arm (8) and second and folds arm (9), the top of first folding arm (8) is connected with the first damping joint (6), and described the One, which folds arm (8), is connect by the first damping joint (6) with the bottom center of unmanned plane (1), and described second folds the top of arm (9) End and bottom end are respectively connected with the second damping joint (10), and the described second top for folding arm (9) passes through the second damping joint (10) The bottom end for folding arm (8) with described first is connect, and the described second bottom end for folding arm (9) passes through the second damping joint (10) connection There is third to fold arm (11), the bottom end that the third folds arm (11) is provided with disengaging buckle (13), and the third folds arm (11) it is connected with removal hook (4) by being detached from buckle (13), is connected with hitch gear (14), the extension on the removal hook (4) Hook mechanism (14) includes hanger bulk (3), is connected with and fetches ring (5) on the hanger bulk (3), and described first folds arm (8) It is folded with second and is equipped with folded wall joint lock (7) in the middle part of arm (9).
2. UAV flight according to claim 1 folds arm high-altitude installation safe anti-falling hook, it is characterised in that: described First damping joint (6) damps joint using twin shaft.
3. UAV flight according to claim 1 folds arm high-altitude installation safe anti-falling hook, it is characterised in that: described Second damping joint (10) on the top and bottom end of the second folding arm (9) is uniaxial damping joint.
4. UAV flight according to claim 1 folds arm high-altitude installation safe anti-falling hook, it is characterised in that: described Hanger bulk (3) is equipped with guide wheel (12) far from the one end for fetching ring (5).
5. UAV flight folds the application method of arm high-altitude installation safe anti-falling hook, including claim 1-4 any one The UAV flight folds arm high-altitude installation safe anti-falling and hangs, it is characterised in that: the application method including safety rope mounting With the application method of safety rope recycling.
6. UAV flight according to claim 5 folds the application method of arm high-altitude installation safe anti-falling hook, special Sign is: the application method of the safety rope mounting includes the following steps:
S11: prepare unmanned plane and associated components before work;
S12: corresponding traction rope, safety rope and hanger bulk are chosen according to the height of target hanging point;
S13: the disengaging that hanger bulk upper end folds arm lower end with third is snapped connection;
S14: it opens the folded wall joint that first folds on arm and the second folding arm and locks;
S15: control unmanned plane takes off, and the first folding arm, the second folding arm and third fold arm and open up automatically under gravity It opens;
S16: unmanned plane flies to target position, and slow falling head returns picture by video camera;
S17: adjusting the aperture position of hanger bulk, when the opening of hanger bulk is caught in hanging point, controls unmanned plane during flying forward, Make hanger bulk and folds arm disengaging;
S18: after hanger bulk falls into hanging point, unmanned plane returns to landing;
S19: traction rope is substituted for safety rope.
7. UAV flight according to claim 5 folds the application method of arm high-altitude installation safe anti-falling hook, special Sign is: the application method of the safety rope recycling includes the following steps:
S21: safety rope is substituted for traction rope;
S22: removal hook is folded into arm lower end with third and is connect;
S23: unmanned plane takes off and slowly increases, and first, which folds arm, the second folding arm and third, folds arm under the effect of gravity certainly Dynamic expansion;
S24: unmanned plane flies to target position, and slow falling head returns picture by camera;
S25: adjusting the position of removal hook, and removal hook is inserted into fetching in ring above hanger bulk, unmanned plane is controlled upwards, takes Hanger bulk out;
S26: unmanned plane carries hanger bulk landing.
8. UAV flight according to claim 7 folds the application method of arm high-altitude installation safe anti-falling hook, special Sign is: when the first folding arm, the second folding arm third folding arm cannot be fully deployed in place under the effect of gravity, carrying out artificial It moves, is allowed in unfolded state.
CN201910540041.2A 2019-06-21 2019-06-21 Unmanned aerial vehicle carried folding arm high-altitude installation safety anti-falling hook and use method thereof Active CN110239704B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201910540041.2A CN110239704B (en) 2019-06-21 2019-06-21 Unmanned aerial vehicle carried folding arm high-altitude installation safety anti-falling hook and use method thereof

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201910540041.2A CN110239704B (en) 2019-06-21 2019-06-21 Unmanned aerial vehicle carried folding arm high-altitude installation safety anti-falling hook and use method thereof

Publications (2)

Publication Number Publication Date
CN110239704A true CN110239704A (en) 2019-09-17
CN110239704B CN110239704B (en) 2023-05-16

Family

ID=67888581

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201910540041.2A Active CN110239704B (en) 2019-06-21 2019-06-21 Unmanned aerial vehicle carried folding arm high-altitude installation safety anti-falling hook and use method thereof

Country Status (1)

Country Link
CN (1) CN110239704B (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110816822A (en) * 2019-12-06 2020-02-21 西安爱生技术集团公司 Be used for unmanned aerial vehicle to block hook band pulley hook head structure
CN117902043A (en) * 2024-03-19 2024-04-19 成都翼比特自动化设备有限公司 Unmanned aerial vehicle mounting tower climbing anti-falling device and control method
CN117902043B (en) * 2024-03-19 2024-05-14 成都翼比特自动化设备有限公司 Unmanned aerial vehicle mounting tower climbing anti-falling device and control method

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN202235051U (en) * 2011-09-16 2012-05-30 罗轶 Foldable cantilever shower
CN103470933A (en) * 2013-09-30 2013-12-25 罗轶 Wearable support
CN105390988A (en) * 2015-12-17 2016-03-09 国家电网公司 Ultra-high voltage power transmission line equipotential live working device and use method thereof
CN106240824A (en) * 2016-07-28 2016-12-21 山东兆源智能科技有限公司 Heavy unmanned fog machine
CN206918583U (en) * 2017-04-26 2018-01-23 南京易纹兴智能科技有限公司 A kind of folding-type portable rephotograph stand
CN206932261U (en) * 2017-05-16 2018-01-26 陈允安 A kind of folding bracket for slowing down arm and lifting mobile phone and fatigue for a long time
CN108452451A (en) * 2018-04-28 2018-08-28 国网河南省电力公司郑州供电公司 Mobile power line shaft tower climbs personal safety guard method and device
CN109173113A (en) * 2018-10-25 2019-01-11 国网四川省电力公司德阳供电公司 Falling proof device and its hanging method based on unmanned plane suspension
CN109250115A (en) * 2018-11-12 2019-01-22 云南电网有限责任公司红河供电局 Multi-rotor unmanned aerial vehicle power grid high-altitude working safety rope hooking method

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN202235051U (en) * 2011-09-16 2012-05-30 罗轶 Foldable cantilever shower
CN103470933A (en) * 2013-09-30 2013-12-25 罗轶 Wearable support
CN105390988A (en) * 2015-12-17 2016-03-09 国家电网公司 Ultra-high voltage power transmission line equipotential live working device and use method thereof
CN106240824A (en) * 2016-07-28 2016-12-21 山东兆源智能科技有限公司 Heavy unmanned fog machine
CN206918583U (en) * 2017-04-26 2018-01-23 南京易纹兴智能科技有限公司 A kind of folding-type portable rephotograph stand
CN206932261U (en) * 2017-05-16 2018-01-26 陈允安 A kind of folding bracket for slowing down arm and lifting mobile phone and fatigue for a long time
CN108452451A (en) * 2018-04-28 2018-08-28 国网河南省电力公司郑州供电公司 Mobile power line shaft tower climbs personal safety guard method and device
CN109173113A (en) * 2018-10-25 2019-01-11 国网四川省电力公司德阳供电公司 Falling proof device and its hanging method based on unmanned plane suspension
CN109250115A (en) * 2018-11-12 2019-01-22 云南电网有限责任公司红河供电局 Multi-rotor unmanned aerial vehicle power grid high-altitude working safety rope hooking method

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110816822A (en) * 2019-12-06 2020-02-21 西安爱生技术集团公司 Be used for unmanned aerial vehicle to block hook band pulley hook head structure
CN117902043A (en) * 2024-03-19 2024-04-19 成都翼比特自动化设备有限公司 Unmanned aerial vehicle mounting tower climbing anti-falling device and control method
CN117902043B (en) * 2024-03-19 2024-05-14 成都翼比特自动化设备有限公司 Unmanned aerial vehicle mounting tower climbing anti-falling device and control method

Also Published As

Publication number Publication date
CN110239704B (en) 2023-05-16

Similar Documents

Publication Publication Date Title
KR200496170Y1 (en) Suspended Cargo Stabilization Systems and Methods
US10469757B2 (en) Flying camera and a system
US11142316B2 (en) Control of drone-load system method, system, and apparatus
US8985878B2 (en) System for camera stabilization
US20180086460A1 (en) In flight transfer of packages between aerial drones
WO2016192021A1 (en) Systems and methods for foldable arms
CN110239704A (en) UAV flight folds arm high-altitude installation safe anti-falling hook and its application method
EP3494043A1 (en) Methods and systems for detecting and resolving failure events when raising and lowering a payload
JP3217820U (en) Drone
WO2007132454A3 (en) Aircraft with cables to deploy hanging cabin
CN202783782U (en) Parachute disconnecting device for unmanned aircraft
US20070063103A1 (en) Parachute release apparatus
JP6213968B2 (en) Shooting unit
JP6243768B2 (en) Method for opening flying object and parachute
WO2019041126A1 (en) Frame and multi-rotor unmanned aerial vehicle
CN107226214A (en) Panorama camera mounting structure on a kind of unmanned plane
KR20100070685A (en) Recovery system of unmanned aerial vehicle
JP6635426B1 (en) Telescopic bar
CN204998755U (en) Rotor unmanned aerial vehicle balance adjustment device
WO2019113775A1 (en) Unmanned aerial vehicle and pan-tilt shock-absorbing mechanism and pan-tilt assembly therefor
CN210133276U (en) Special folding arm device of electrified coaster that hangs of unmanned aerial vehicle
JP2019137251A (en) Mobile work device
US20160209732A1 (en) Camera Supporting and Stabilization Apparatus and Methods
CN206926834U (en) Panorama camera mounting structure on a kind of unmanned plane
JP2020063121A (en) Rotation suppression device and crane operation system

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant