CN110435911A - A kind of unmanned plane recyclable device - Google Patents
A kind of unmanned plane recyclable device Download PDFInfo
- Publication number
- CN110435911A CN110435911A CN201910661662.6A CN201910661662A CN110435911A CN 110435911 A CN110435911 A CN 110435911A CN 201910661662 A CN201910661662 A CN 201910661662A CN 110435911 A CN110435911 A CN 110435911A
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- China
- Prior art keywords
- arm
- assembly
- cross bar
- oil cylinder
- arm assembly
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- 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
Links
- 230000009975 flexible effect Effects 0.000 claims abstract description 39
- 238000004064 recycling Methods 0.000 claims abstract description 28
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims abstract description 8
- 230000004308 accommodation Effects 0.000 claims abstract description 4
- 238000009785 tube rolling Methods 0.000 claims description 6
- 230000008602 contraction Effects 0.000 claims description 4
- 239000000446 fuel Substances 0.000 claims description 3
- 238000004804 winding Methods 0.000 claims description 2
- 238000005096 rolling process Methods 0.000 claims 1
- 238000010276 construction Methods 0.000 description 4
- 230000001360 synchronised effect Effects 0.000 description 3
- 239000003795 chemical substances by application Substances 0.000 description 2
- 238000013016 damping Methods 0.000 description 2
- FGRBYDKOBBBPOI-UHFFFAOYSA-N 10,10-dioxo-2-[4-(N-phenylanilino)phenyl]thioxanthen-9-one Chemical compound O=C1c2ccccc2S(=O)(=O)c2ccc(cc12)-c1ccc(cc1)N(c1ccccc1)c1ccccc1 FGRBYDKOBBBPOI-UHFFFAOYSA-N 0.000 description 1
- 230000002457 bidirectional effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/02—Ground or aircraft-carrier-deck installations for arresting aircraft, e.g. nets or cables
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Jib Cranes (AREA)
Abstract
The invention discloses a kind of unmanned plane recyclable devices, including flexible arm assembly, folding arm assembly, cross bar assembly, turntable, swing mechanism, pedestal and recycling rope assembly；The turntable is set on the base by swing mechanism；The cross bar assembly tail end is connected with turntable, and the flexible arm assembly tail end is connected with turntable, and flexible arm assembly front end is connected with arm assembly tail end is folded；The turntable, flexible arm assembly, folding arm assembly, cross bar assembly constitute the accommodation space of a c-type structure, connect two notches up and down of c-type structure by the recycling rope assembly, to constitute a complete unmanned aerial vehicle rope recycling space.The device retracted state space occupied is small, transport convenience, can be vehicle-mounted, can aboard ship can also use mounted in tow out on trailer, can also the transport in 20 forty equivalent unit 40s.
Description
Technical field
The present invention relates to unmanned plane fields, and in particular to a kind of unmanned plane recyclable device.
Background technique
Unmanned plane way of recycling has undercarriage running landing, parachute recycling, intercept net recycling, air bag recycling, air cushion to return
Receipts, aerial recycling, vertical landing etc..
Undercarriage running landing requires runway do not have man-machine height, some Landing Gear Designs are more fragile, damage suction with hitting
Energy is received, some band pintles can hook interception rope and slow down as early as possible.
Parachute recycling: large-scale unmanned plane is recycled in narrow and small place, and body contact site need to install damping device, is inflated
Bag, shock-damping structure etc., contact site is as far as possible far from equipment compartment.
Intercept net recycling is primarily directed to small drone, and overload of touching net is no more than 6g.
Air cushion recovery principle is similar with air cushion vehicle and aircushion vehicle, and air is pressed into air bag by engine, and compressed air is from bag hole
Middle ejection forms pressure-air area-air cushion in ventral, and landing is not limited by surface condition, do not limited, recycled by size, weight
Rate is high.
Aerial recycling, it is costly, it is desirable that high, risk is high, and only the U.S. uses at present.
Vertical recycling and Vertical Launch principle are the same.
Rope debit's formula is to realize recycling using the rope being suspended on a sunpender capture small hook of unmanned plane wing point.
Some is needed to assemble structure scene mostly, be had plenty of in fixation using easy rope receiving apparatus in industry
Basis is made in place, and recyclable device is fixed thereon.Although the principle received of restricting is close, implements and have nothing in common with each other.
Summary of the invention
Insufficient according to prior art, a kind of unmanned plane recyclable device of the present invention adapts to various transport agents, can it is vehicle-mounted or
Person is carrier-borne, can carry out Container Transport.
The present invention is realized by following technical scheme:
A kind of unmanned plane recyclable device, including flexible arm assembly, folding arm assembly, cross bar assembly, turntable, swing mechanism, pedestal
With recycling rope assembly；The turntable is set on the base by swing mechanism；The cross bar assembly tail end is connected with turntable, described
Flexible arm assembly tail end is connected with turntable, and flexible arm assembly front end is connected with arm assembly tail end is folded；The turntable, telescopic arm are total
At, fold arm assembly, cross bar assembly and constitute the accommodation space of a c-type structure, pass through the recycling and restrict assembly connection c-type knot
Two notches up and down of structure, to constitute a complete unmanned aerial vehicle rope recycling space.
Further, the flexible arm assembly includes basic arm and multi-stage telescopic arms, and multi-stage telescopic arms are sequentially loaded into basic arm
In, multi-stage telescopic arms synchronization telescope on basic arm is realized by the tactic pattern of single cylinder plus component of restricting.
Further, the flexible arm assembly is by connecting amplitude oil cylinder I for flexible arm assembly pitching to scheduled angle.
Further, the folding arm assembly includes folding arm I and folding arm II；Wherein, the folding arm I is total with telescopic arm
It is hinged at front end, and with flexible arm assembly at an angle less than 180 °；The folding arm II is hinged with arm I is folded,
Variable angle between the two is 0-180 °.
Further, the folding arm assembly further includes amplitude oil cylinder II and amplitude oil cylinder III；Described II one end of amplitude oil cylinder
It is hinged with arm I is folded, II other end of amplitude oil cylinder is hinged with connecting rod I and connecting rod II, and connecting rod I is again and before flexible arm assembly
End is hinged, and connecting rod II is hinged with folding arm I again；Arm assembly pitching will be folded to predetermined angular by amplitude oil cylinder II；Institute
It states III one end of amplitude oil cylinder and is hinged with arm I is folded, III other end of amplitude oil cylinder is hinged with connecting rod III and connecting rod IV, and connecting rod
III is hinged with folding arm I again, and connecting rod IV is hinged with folding arm II again；It is swung to by amplitude oil cylinder III by arm II is folded
180°。
Further, after the folding arm II is unfolded, by being located at the mechanical position limitation for folding arm I and folding II hinged place of arm
Limit the freedom degree in one direction of gyrobearing.
Further, the amplitude oil cylinder II and amplitude oil cylinder III pass through high-pressure hose tube rolling device fuel feeding and oil return, and luffing
Respectively there are oil inlet all the way and oil return all the way in oil cylinder II and amplitude oil cylinder III.
Further, the cross bar assembly include cross bar basic arm, cross bar telescopic arm I, cross bar telescopic arm II, brake motor and
Rope component；The rope component includes wirerope, rope socket I and rope socket II；The brake motor is fixed on cross bar basic arm,
Roller is equipped in the shaft of brake motor, the wirerope comes out the rope socket I to misplace up and down after winding multi-turn on roller
With rope socket II；The rope socket I bypasses the fixed pulley being mounted on cross bar basic arm and is connected with the tail portion of cross bar telescopic arm I,
Rope socket II is connected with I head of cross bar telescopic arm.
Further, the bottom surface of the pedestal is equipped with a circle threaded connection hole I, to be fixed on stationary plane by multiple bolts
On；After unmanned plane recyclable device is in contraction state, by the support frame that is fixed on stationary plane to unmanned plane recyclable device
Front is supported.
The invention has the advantages that:
1) rope modular construction is added using single cylinder, it is possible to reduce the weight of executive component, while realizing synchronization telescope, improve flexible effect
Rate；
2) artificial luffing is replaced using the folding arm of oil-cylinder variable amplitude, mitigates operator's intensity, while realizing operation readiness；
3) add rope modular construction that oil cylinder is replaced to add rope modular construction using brake motor, the section of transverse arm is effectively reduced, to subtract
Light weight；
4) collapsing length of flexible arm assembly is adjustable, cross bar collapsing length is adjustable, the change angle of folding arm assembly is adjustable, this
Sample has met requirement of the different type of machines for recycling space；
5) integral module designs, and adapts to various transport agents, can be vehicle-mounted or carrier-borne, can carry out Container Transport.
Detailed description of the invention
Fig. 1 is unmanned plane recyclable device unfolding state figure of the invention；
Fig. 1 a is the A direction view of Fig. 1；
Fig. 2 is unmanned plane recyclable device contraction state figure of the invention；
Fig. 2 a is the B direction view of Fig. 2；
Fig. 3 is folding arm junction layout drawing of the invention；
Fig. 4 is cross bar assembly retracted state figure of the invention；
Fig. 5 is that cross bar assembly of the invention stretches out state diagram；
Fig. 6 is cross bar assembly structure chart of the invention.
In figure: 1- stretches arm assembly；1-1- basic arm；The first telescopic arm of 1-2-；The second telescopic arm of 1-3-；1-4- third is stretched
Contracting arm；2- folds arm assembly；2-1- folds arm I；2-2- folds arm II；3- cross bar assembly；3-1- cross bar basic arm；3-2- cross bar
Telescopic arm I；3-3- cross bar telescopic arm II；4- turntable；5- swing mechanism；6- pedestal；7- recycling rope assembly；8- amplitude oil cylinder I；9-
Amplitude oil cylinder II；10- amplitude oil cylinder III；11- high-pressure hose tube rolling device；12- connecting rod I；13- connecting rod II；14- connecting rod III；15- connects
Bar IV；16- mechanical position limitation；17- threaded connection hole I；18- threaded connection hole II；19- brake motor；20- rope component；20-1 rope
Connector I；20-2 rope socket II；20-3 wirerope；21- roller；22- fixed pulley；23- support frame.
Specific embodiment
To keep the purposes, technical schemes and advantages of the invention implemented clearer, below in conjunction in the embodiment of the present invention
Attached drawing, technical solution in the embodiment of the present invention is further described in more detail.In the accompanying drawings, identical from beginning to end or class
As label indicate same or similar element or element with the same or similar functions.Described embodiment is the present invention
A part of the embodiment, instead of all the embodiments.The embodiments described below with reference to the accompanying drawings are exemplary, it is intended to use
It is of the invention in explaining, and be not considered as limiting the invention.Based on the embodiments of the present invention, ordinary skill people
Member's every other embodiment obtained without making creative work, shall fall within the protection scope of the present invention.Under
Face is described in detail the embodiment of the present invention in conjunction with attached drawing.
As shown in Figure 1 and Figure 2, the present invention provides a kind of unmanned plane recyclable device, and what is used in terms of constructing space first stretches
The form folded afterwards.Flexible is the short transverse in order to construct recycling space, and folding arm is the revolution in order to construct recycling space
Radius.Concrete scheme is as follows:
A kind of unmanned plane recyclable device, including flexible arm assembly 1, fold arm assembly 2, cross bar assembly 3, turntable 4, swing mechanism 5,
Pedestal 6 and recycling rope assembly 7；Turntable 4 is arranged on pedestal 6 by swing mechanism 5；3 tail end of cross bar assembly is connected with turntable 4,
Flexible 1 tail end of arm assembly is connected with turntable 4, and flexible 1 front end of arm assembly is connected with 2 tail end of arm assembly is folded；Turntable 4, telescopic arm
Assembly 1, folding arm assembly 2, cross bar assembly 3 constitute the accommodation space of a c-type structure, pass through recycling rope assembly 7 and connect c-type
Two notches up and down of structure, to constitute a complete unmanned aerial vehicle rope recycling space.
It is given below in above-described embodiment about flexible one preferred embodiment of arm assembly:
Flexible arm assembly includes basic arm and three section telescopic arms (the first telescopic arm 1-2, the second telescopic arm 1-3, third i.e. in figure
Telescopic arm 1-4), three section telescopic arms are sequentially loaded into basic arm 1-1, realize that three sections are stretched by the tactic pattern of single cylinder plus component of restricting
Contracting arm synchronization telescope on basic arm 1-1.Flexible arm assembly 1 is by connection amplitude oil cylinder I 8 by flexible 1 pitching of arm assembly in advance
Fixed angle.
It should be noted that above-mentioned single cylinder add rope component tactic pattern and it is existing in crane telescopic arm original
Reason is consistent, and it be not described in detail herein.The collapsing length of flexible arm assembly is changed (not accordingly according to the difference of type
It is confined to three above-mentioned section telescopic arms).
It is given below in above-described embodiment about folding one preferred embodiment of arm assembly:
As shown in figure 3, folding arm assembly 2 includes folding I 2-1 of arm and folding II 2-2 of arm；Wherein, I 2-1 of arm and telescopic arm are folded
1 front end of assembly is hinged, and with flexible arm assembly 1 at an angle less than 180 °；It folds II 2-2 of arm and folds I 2-1 phase of arm
Hingedly, variable angle between the two is 0-180 °.
Folding arm assembly 2 further includes amplitude oil cylinder II 9 and amplitude oil cylinder III 10；II 9 one end of amplitude oil cylinder and folding I 2- of arm
1 is hinged, and II 9 other end of amplitude oil cylinder is hinged with connecting rod I 12 and connecting rod II 13, and connecting rod I 12 is again and before flexible arm assembly 1
End is hinged, and connecting rod II 13 is hinged with folding I 2-1 of arm again；By amplitude oil cylinder II 9 will fold 2 pitching of arm assembly to make a reservation for
Angle；III 10 one end of amplitude oil cylinder is hinged with I 2-1 of arm is folded, III 10 other end of amplitude oil cylinder and connecting rod III 14 and connecting rod IV
15 are hinged, and connecting rod III 14 is hinged with folding I 2-1 of arm again, and connecting rod IV 15 is hinged with folding II 2-2 of arm again；Pass through change
Width oil cylinder III 10 swings to 180 ° for II 2-2 of arm is folded.
After folding II 2-2 of arm expansion, by being located at the mechanical position limitation 16 for folding I 2-1 of arm and folding II hinged place 2-2 of arm
The freedom degree in one direction of gyrobearing is limited, in addition the limit of gyrobearing is limited by oil cylinder, as shown in figure 3, oily
Cylinder by pressure not by pulling force, thus effectively control oil cylinder outer dimension.
Further embodiment:
It is III 10 fuel feeding of amplitude oil cylinder II9 amplitude oil cylinder and oil return by high-pressure hose tube rolling device 11.This mode replaces tradition
Drag chain structure, integrally seem succinct agile.Each amplitude oil cylinder respectively has oil inlet all the way and oil return all the way, so using 8 line systems
High-pressure hose tube rolling device 11.The high-pressure hose tube rolling device 11 is fixed on the basic arm 1-1 of flexible arm assembly 1 that (telescopic arm is total
The arm being connect at 1 outermost with turntable 4 and amplitude oil cylinder I 8), the oil pipe of stretching is fixed on (telescopic arm on third telescopic arm 1-4
The most inboard arms of assembly).
It is given below in above-described embodiment about one preferred embodiment of cross bar assembly:
As shown in Fig. 4, Fig. 5, Fig. 6, the two-stage telescopic arm structure of the use of cross bar assembly 3.It is mutually tied using brake motor and rope component
The structure of conjunction, the mechanism combined instead of conventional oil cylinder with rope component.This structure cabinet section can be done it is small, to have
Effect mitigates weight.
Brake motor 19 is fixed on cross bar basic arm 3-1, can drive cross bar telescopic arm by wirerope with bidirectional rotation
It stretches out or retracts, as shown in Figure 4, Figure 5.Based on different types, the collapsing length of cross bar is carried out corresponding by corresponding program
Matching.
Rope component 20 on cross bar assembly is made of wirerope 20-3 and two rope ends, and rope component 20 is wound on roller 21
Three circles, two rope ends to misplace up and down out, wherein I 20-1 of rope socket is fixed on cross bar base around fixed pulley 22(fixed pulley 22
On this arm 3-1) it is connected with the tail portion of I 3-2 of cross bar telescopic arm, II 20-2 of rope socket is connected with I head 3-1 of cross bar telescopic arm.
When brake motor 19 rotates clockwise, brake motor 19 is rotated clockwise with roller 21, hauls rope socket I
20-1 is moved to 19 direction of brake motor, and I 3-2 of cross bar telescopic arm is retracted.(cross bar is flexible for the synchronous retraction of II 3-2 of cross bar telescopic arm
The synchronization telescope principle of II 3-2 of arm compared with telescopic crane boom principle, this will not be detailed here).
When brake motor 19 rotates counterclockwise, brake motor 19 rotates counterclockwise with roller 21, hauls rope socket II
20-2 is moved away from 19 direction of brake motor, and I 3-2 of cross bar telescopic arm stretches out.II 3-2 of cross bar telescopic arm is synchronous to stretch out (cross
The synchronization telescope principle of bar telescopic arm II compared with telescopic crane boom principle, this will not be detailed here).
The bottom surface of pedestal 6 is equipped with a circle threaded connection hole I 17, to be fixed on stationary plane by multiple bolts；Work as nothing
After man-machine recyclable device is in contraction state, by the support frame 23 that is fixed on stationary plane to unmanned plane recyclable device front into
Row support.The bottom surface of support frame 23 is equipped with multiple threaded connection holes II 18, to be fixed on stationary plane by multiple bolts.
To sum up, by flexible 1 pitching of arm assembly to certain angle, the arm assembly 1 that stretches is synchronous to be stretched out amplitude oil cylinder I 8.According to
The collapsing length of different types, the arm assembly 1 that stretches is adjustable.Amplitude oil cylinder II 9 will fold 2 pitching of arm assembly to certain angle
Degree, the angle can be adjusted according to different types.Amplitude oil cylinder III 10 swings to 180 degree for II 2-2 of arm is folded, structurally
The lateral length at end, that is, distance of the lanyard point apart from the centre of gyration.The brake motor that cross bar assembly 3 uses adds the mechanism of rope component,
Realize that the two-stage of cross bar is flexible.The advantages of mechanism is to occupy little space, and telescopic arm section adds rope modular construction small compared with oil cylinder.
Turntable 4, flexible arm assembly 1, folding arm assembly 2, cross bar assembly 3 constitute the space of an approximate c-type.Pass through recycling rope assembly
Two notches above and below 7 connection c-type structures, to constitute a complete unmanned aerial vehicle rope recycling space.The device withdraws shape
State space occupied is small, transport convenience, can be vehicle-mounted, can aboard ship can also use, can also fill mounted in tow out on trailer
It is transported in 20 forty equivalent unit 40s.
Finally it should be noted that: the above embodiments are merely illustrative of the technical scheme of the present invention and are not intended to be limiting thereof；To the greatest extent
The present invention is described in detail with reference to preferred embodiments for pipe, it should be understood by those ordinary skilled in the art that: still
It can modify to a specific embodiment of the invention or some technical features can be equivalently replaced；Without departing from this hair
The spirit of bright technical solution should all cover within the scope of the technical scheme claimed by the invention.
Claims (9)
1. a kind of unmanned plane recyclable device, it is characterised in that: including flexible arm assembly, fold arm assembly, cross bar assembly, turntable,
Swing mechanism, pedestal and recycling rope assembly；
The turntable is set on the base by swing mechanism；
The cross bar assembly tail end is connected with turntable, and the flexible arm assembly tail end is connected with turntable, stretch arm assembly front end with
Arm assembly tail end is folded to be connected；
The turntable, flexible arm assembly, folding arm assembly, cross bar assembly constitute the accommodation space of a c-type structure, pass through institute
Two notches up and down of recycling rope assembly connection c-type structure are stated, to constitute a complete unmanned aerial vehicle rope recycling space.
2. a kind of unmanned plane recyclable device according to claim 1, it is characterised in that: the flexible arm assembly includes basic
Arm and multi-stage telescopic arms, multi-stage telescopic arms are sequentially loaded into basic arm, realize more piece by the tactic pattern of single cylinder plus component of restricting
Telescopic arm synchronization telescope on basic arm.
3. a kind of unmanned plane recyclable device according to claim 1, it is characterised in that: the flexible arm assembly passes through connection
Amplitude oil cylinder I is by flexible arm assembly pitching to scheduled angle.
4. a kind of unmanned plane recyclable device according to claim 1, it is characterised in that: the folding arm assembly includes folding
Arm I and folding arm II；Wherein, the folding arm I is hinged with flexible arm assembly front end, and is less than with flexible arm assembly at one
180 ° of angle；
The folding arm II is hinged with arm I is folded, and variable angle between the two is 0-180 °.
5. a kind of unmanned plane recyclable device according to claim 4, it is characterised in that: the folding arm assembly further includes becoming
Width oil cylinder II and amplitude oil cylinder III；
Described II one end of amplitude oil cylinder is hinged with arm I is folded, and II other end of amplitude oil cylinder is hinged with connecting rod I and connecting rod II,
And connecting rod I is hinged with flexible arm assembly front end again, connecting rod II is hinged with folding arm I again；It will be folded by amplitude oil cylinder II
Arm assembly pitching is to predetermined angular；
Described III one end of amplitude oil cylinder is hinged with arm I is folded, and III other end of amplitude oil cylinder is hinged with connecting rod III and connecting rod IV,
And connecting rod III is hinged with folding arm I again, connecting rod IV is hinged with folding arm II again；It is put by amplitude oil cylinder III by arm II is folded
To 180 °.
6. a kind of unmanned plane recyclable device according to claim 5, it is characterised in that: after the folding arm II is unfolded,
The freedom degree in mechanical position limitation limitation one direction of gyrobearing of arm I and folding II hinged place of arm is folded by being located at.
7. a kind of unmanned plane recyclable device according to claim 5, it is characterised in that: the amplitude oil cylinder II and luffing oil
Cylinder III respectively has oil inlet all the way and all the way by high-pressure hose tube rolling device fuel feeding and oil return in amplitude oil cylinder II and amplitude oil cylinder III
Oil return.
8. a kind of unmanned plane recyclable device according to claim 1, it is characterised in that: the cross bar assembly includes cross bar base
This arm, cross bar telescopic arm I, cross bar telescopic arm II, brake motor and rope component；
The rope component includes wirerope, rope socket I and rope socket II；
The brake motor is fixed on cross bar basic arm, and roller is equipped in the shaft of brake motor, and the wirerope is rolling
The rope socket I and rope socket II to misplace up and down is come out after winding multi-turn on son；
The rope socket I bypasses the fixed pulley being mounted on cross bar basic arm and is connected with the tail portion of cross bar telescopic arm I, rope socket II
It is connected with I head of cross bar telescopic arm.
9. a kind of unmanned plane recyclable device according to claim 1, it is characterised in that: the bottom surface of the pedestal is equipped with a circle
Threaded connection hole I, to be fixed on stationary plane by multiple bolts；
After unmanned plane recyclable device is in contraction state, by the support frame that is fixed on stationary plane to unmanned plane recyclable device
Front is supported.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910661662.6A CN110435911A (en) | 2019-07-22 | 2019-07-22 | A kind of unmanned plane recyclable device |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910661662.6A CN110435911A (en) | 2019-07-22 | 2019-07-22 | A kind of unmanned plane recyclable device |
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| CN110435911A true CN110435911A (en) | 2019-11-12 |
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| CN201910661662.6A Pending CN110435911A (en) | 2019-07-22 | 2019-07-22 | A kind of unmanned plane recyclable device |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110979713A (en) * | 2019-12-25 | 2020-04-10 | 三一汽车制造有限公司 | Unmanned aerial vehicle recovery unit |
| CN112607026A (en) * | 2020-12-30 | 2021-04-06 | 山东省科学院海洋仪器仪表研究所 | Automatic recovery and release device and method for multi-rotor unmanned aerial vehicle |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2005014390A2 (en) * | 2003-01-17 | 2005-02-17 | The Insitu Group | Methods and apparatuses for storing, launching, and capturing unmanned aircraft |
| US20050093507A1 (en) * | 2003-11-03 | 2005-05-05 | Sliwa Steven M. | Methods and systems for starting propeller-driven devices |
| KR20100133810A (en) * | 2009-06-12 | 2010-12-22 | (주)엔에스에이치 | Apparatus and method for guiding landing of uninhabited aerial vehicle using wire |
| WO2012047677A2 (en) * | 2010-09-27 | 2012-04-12 | Craig Aram Thomasian | Line capture devices for unmanned aircraft, and associated systems and methods |
| US20150259048A1 (en) * | 2011-11-28 | 2015-09-17 | Aeplog, Inc. | Launch and recovery device |
| CN205971887U (en) * | 2016-07-14 | 2017-02-22 | 西安思坦测控技术有限公司 | Unmanned aerial vehicle recovery system |
| CN207000837U (en) * | 2017-05-10 | 2018-02-13 | 周健航 | A kind of unmanned plane draw off gear and UAS |
| CN108688828A (en) * | 2018-05-23 | 2018-10-23 | 河南卫华特种车辆有限公司 | A kind of movable unmanned helicopter high-altitude reclaimer |
| CN210681186U (en) * | 2019-07-22 | 2020-06-05 | 徐州川一工程机械有限公司 | Unmanned aerial vehicle recovery unit |
-
2019
- 2019-07-22 CN CN201910661662.6A patent/CN110435911A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2005014390A2 (en) * | 2003-01-17 | 2005-02-17 | The Insitu Group | Methods and apparatuses for storing, launching, and capturing unmanned aircraft |
| US20050093507A1 (en) * | 2003-11-03 | 2005-05-05 | Sliwa Steven M. | Methods and systems for starting propeller-driven devices |
| KR20100133810A (en) * | 2009-06-12 | 2010-12-22 | (주)엔에스에이치 | Apparatus and method for guiding landing of uninhabited aerial vehicle using wire |
| WO2012047677A2 (en) * | 2010-09-27 | 2012-04-12 | Craig Aram Thomasian | Line capture devices for unmanned aircraft, and associated systems and methods |
| US20150259048A1 (en) * | 2011-11-28 | 2015-09-17 | Aeplog, Inc. | Launch and recovery device |
| CN205971887U (en) * | 2016-07-14 | 2017-02-22 | 西安思坦测控技术有限公司 | Unmanned aerial vehicle recovery system |
| CN207000837U (en) * | 2017-05-10 | 2018-02-13 | 周健航 | A kind of unmanned plane draw off gear and UAS |
| CN108688828A (en) * | 2018-05-23 | 2018-10-23 | 河南卫华特种车辆有限公司 | A kind of movable unmanned helicopter high-altitude reclaimer |
| CN210681186U (en) * | 2019-07-22 | 2020-06-05 | 徐州川一工程机械有限公司 | Unmanned aerial vehicle recovery unit |
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| CN110979713A (en) * | 2019-12-25 | 2020-04-10 | 三一汽车制造有限公司 | Unmanned aerial vehicle recovery unit |
| CN110979713B (en) * | 2019-12-25 | 2023-04-07 | 湖南省地面无人装备工程研究中心有限责任公司 | Unmanned aerial vehicle recovery unit |
| CN112607026A (en) * | 2020-12-30 | 2021-04-06 | 山东省科学院海洋仪器仪表研究所 | Automatic recovery and release device and method for multi-rotor unmanned aerial vehicle |
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