CN106742018A - Retracting device on a kind of unmanned plane warship - Google Patents
Retracting device on a kind of unmanned plane warship Download PDFInfo
- Publication number
- CN106742018A CN106742018A CN201611017874.3A CN201611017874A CN106742018A CN 106742018 A CN106742018 A CN 106742018A CN 201611017874 A CN201611017874 A CN 201611017874A CN 106742018 A CN106742018 A CN 106742018A
- Authority
- CN
- China
- Prior art keywords
- lasso
- pedestal
- outer tube
- spring
- pintle
- 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
Links
- 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 20
- 238000010276 construction Methods 0.000 claims abstract description 16
- 238000011084 recovery Methods 0.000 claims abstract description 13
- 230000003139 buffering effect Effects 0.000 claims description 21
- 230000000694 effects Effects 0.000 claims description 5
- 238000004804 winding Methods 0.000 abstract 1
- 238000005516 engineering process Methods 0.000 description 3
- 238000013016 damping Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 238000013473 artificial intelligence Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000009432 framing Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000004064 recycling 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
- 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)
- Coiling Of Filamentary Materials In General (AREA)
- Ropes Or Cables (AREA)
Abstract
The invention discloses retracting device on a kind of unmanned plane warship, including island-type construction in naval vessels, unmanned body, pedestal and recovery pintle, pedestal is fixed on the side of island-type construction in naval vessels, folding sleeve is connected with pedestal, flexible bridle catcher is movably set with folding sleeve, the two ends of pedestal are each provided with leading block, cabletype hitch is provided with pedestal, cabletype hitch includes motor, decelerator and traction sheave, fixed lasso is provided with folding sleeve, connection lasso is movably set with the outside of fixed lasso, buffer spring B is provided with folding sleeve between fixed lasso and connection lasso, hauling rope is provided with connection lasso, the stage casing winding of hauling rope is on the traction sheave；Heavy burden tie-down cable is provided between the upper end of island-type construction in connection lasso and naval vessels, the outer end of flexible bridle catcher is provided with signal projector；The posterior end of unmanned body is movably set with recovery pintle；The present invention is simple and reasonable for structure, design science, advanced.
Description
Technical field
The present invention relates to a kind of unmanned plane retracting device, fixed-wing unmanned plane is returned more particularly, to a kind of naval vessels waterborne
Receiving apparatus.
Background technology
With navigation, electronics, communication, power, automatically control, the sophisticated technologies such as material and artificial intelligence are in aviation field
Integrated application and develop rapidly, the rapid unprecedented brand-new height of marching toward of current unmanned air vehicle technique level shows
The mode of operation of influence and change future naval battle is until the great potential of the form of war；Do not house and doubt, with naval's unmanned plane
The sustainable development of technology, its technical merit, task function or even operation purposes will tend to ripe within the not too long of time, will
Promote Modern Navy and naval battle field that once new revolution occurs；Military unmanned air vehicle is used as in modern wireless air military power
Member, with no one was injured, using limitation less, good concealment, efficiency-cost ratio high the features such as, status and effect in modern war
It is outstanding day by day；The Chinese patent of Application No. CN201310439325 discloses a kind of SUAV recovering mechanism, by liquid
Pressure drag Buddhist nun's brake disc, for unmanned plane removal process provides buffer deceleration damping；Can be not by adjusting brake disc brake pressure
Satisfied deceleration damping force is provided with the unmanned plane for reclaiming overload requirement；By hydraulic actuator, recycling network support can be completed certainly
It is dynamic to fold, with convenient transportation；Mechanism is made up of dictyosome, dictyosome support, hydraulic system, brake gear etc.；The present invention is applied to
The narrow spaces such as mountain region, island, naval vessel, the features such as convenience with low cost, simple to operate, working service；This invention is only
Reclaim small-sized slow unmanned plane, to more greatly, fireballing unmanned plane it is just helpless；
Fixed Wing AirVehicle has that flying speed is fast, voyage is big, carrying capacity is big, it is economical the features such as；But fixed-wing also have recovery,
The shortcomings of difficulty of taking off；Particularly recovery of the unmanned plane on naval vessels, because having island-type construction in the middle of naval vessels, deck divide into
Forward and backward two parts, it is an impossibility that larger, speed unmanned plane is reclaimed on forward and backward deck；
But the advantage of advantage and ship navigating speed of the naval vessels on the water surface can be used；The advantage of ship navigating speed is in unmanned plane
Speed during land can subtract the speed of ship navigating, so comparatively reclaim the slow many of speed, also easy many；
I am by long-term thinking and look through a great amount of information, and one kind is designed finally various unmanned plane is quickly reclaimed on naval vessels
Retracting device.
The content of the invention
The technical problems to be solved by the invention are to provide on a kind of unmanned plane warship and reclaim receiving apparatus.
Island-type construction in retracting device, including naval vessels, unmanned body, pedestal and pintle is reclaimed on a kind of unmanned plane warship, its
It is characterised by that described pedestal is fixed on the side of island-type construction in the naval vessels, folding sleeve is connected with described pedestal,
Flexible bridle catcher is movably set with described folding sleeve, is set between described flexible bridle catcher and described folding loop bar
Expansion bend；
The two ends of the pedestal are each provided with leading block, and cabletype hitch, described cable wire are provided with described pedestal
Draw-gear includes motor, decelerator and traction sheave, and fixed lasso is provided with the folding sleeve, the fixed lasso
Outside is movably set with connection lasso, is set on the folding sleeve between described fixed lasso and described connection lasso
The side for having buffer spring B, the connection lasso is provided with hauling rope, and the other end of the hauling rope passes through leading described in two
To the opposite side that the connection lasso is fixed on after pulley, described hauling rope is wrapped on described traction sheave；
Heavy burden tie-down cable, the flexible recovery are provided with described connection lasso and the naval vessels between the upper end of island-type construction
The outer end of bar is provided with signal projector.
Reclaiming pintle includes outer tube and buffering shank, it is characterised in that the front end movable axis of the outer tube is connected on described
The posterior end of unmanned body, is provided with bales catch between described outer tube and described unmanned body, described outer tube with
Spring is provided between described unmanned body, described spring all the time flicks downwards described outer tube, described overcoat
Tie-down cable is additionally provided between pipe and described unmanned body；
Buffering chute is provided with described outer tube, the rear end of the outer tube is provided with slide opening, activity in described slide opening
Described buffering shank is provided with, the front end of the buffering shank is provided with the limited block matched with described buffering chute,
Buffer spring A is provided with the buffering shank between described limited block and described slide opening；After the buffering shank
End is provided with pintle, and lock buckling groove and switch groove are provided with described pintle, and automatic lock is movably set with described lock buckling groove
Button, is provided with spring A between described automatic locking and described pintle, described spring A is all the time by described automatic locking
Outwards ejection, is movably set with self-clinching switch in described switch groove, the bottom of described self-clinching switch and the switch groove it
Between be provided with spring B, described spring B all the time pops up described self-clinching switch, and described self-clinching switch is popped up
When described automatic locking is clasped.
The effect of unmanned plane it is bigger its speed and volume it is bigger, so its inertia is also bigger, how to eliminate it
Inertia be an important thing；There is than larger height island-type construction with the water surface, naval vessels also have than the larger speed of a ship or plane in naval vessels,
The recovery of unmanned plane is so more beneficial for, the setting of cabletype hitch and hauling rope after unmanned plane recovery and can not work
When be folded in naval vessels in island-type construction, buffer spring B can make folding sleeve and the flexible bridle catcher have relative swing, so may be used
Offset the inertia of unmanned plane.
Outer tube is folded in unmanned body, is clasped by bales catch, and bales catch is opened during recovery, reclaims pintle in spring A
And put down in the presence of deadweight, the setting of buffer spring A can also offset a part of inertia of unmanned plane, awing self-clinching switch
Automatic locking is clasped, when reclaiming, self-clinching switch is opened in the presence of flexible bridle catcher when pintle hooks flexible bridle catcher
Automatic locking；Its inertia can make unmanned plane put somersaults centered on flexible bridle catcher when being hooked because of unmanned plane, so again
A part of inertia force of unmanned plane can be offset；The framing signal that unmanned plane can receive signal projector transmitting carries out left and right and height
The regulation of degree, so as to accurate recovery；
The present invention is simple and reasonable for structure, design science, advanced.
Brief description of the drawings
Fig. 1 is three-dimensional structure diagram of the invention；
Fig. 2 is recovery pintle profile of the invention；
Fig. 3 is pintle sectional view of the invention；
Fig. 4 is pintle sectional exploded view of the invention；
Fig. 5 is recovery pintle exploded view of the invention；
Fig. 6 is retracting device stereogram of the invention.
Specific embodiment
The present invention is described in further detail below in conjunction with accompanying drawing embodiment.
As illustrated, island-type construction in 1. naval vessels, 2. unmanned body, 11. outer tubes, 12. buffering shanks, 13. limits
Position rope, 14. buffering chutes, 16. buffer spring A, 17 pintles, 18. automatic lockings, 19. self-clinchings switch, 20. lock buckling grooves,
21. switch grooves, 22. spring A, 23. spring Bs, 30. pedestals, 31. folding sleeves, 32. flexible bridle catchers 33. fix lasso,
34. connection lassos, 35. leading blocks, 36. motor, 37. decelerators, 38. traction sheaves, 40. hauling ropes, 41. bear a heavy burden
Tie-down cable, 42. signal projectors, 43. buffer spring B.
As a shown in Figure 6：Island-type construction 1, unmanned body 2, pedestal in retracting device, including naval vessels on a kind of unmanned plane warship
30 and pintle is reclaimed, pedestal 30 is fixed on the side of island-type construction 1 in naval vessels, folding sleeve 31 is connected with pedestal 30, folds
Flexible bridle catcher 32 is movably set with sleeve pipe 31, expansion bend is set between flexible bridle catcher 32 and folding loop bar 32；
The two ends of pedestal 30 are each provided with leading block 35, and cabletype hitch, cabletype hitch bag are provided with pedestal 30
Motor 36, decelerator 37 and traction sheave 38 are included, fixed lasso 33 is provided with folding sleeve 31, the outside of fixed lasso 33 is lived
It is dynamic to be provided with connection lasso 34, buffer spring B43 is provided with the folding sleeve 31 between fixed lasso 33 and connection lasso 34,
The side for connecting lasso 34 is provided with hauling rope 40, and the other end of hauling rope 40 is fixed on connection after passing through two leading blocks 35
The opposite side of lasso, the stage casing of hauling rope 40 is wrapped on traction sheave 38；
Heavy burden tie-down cable 41 is provided between the upper end of island-type construction 1 in connection lasso 34 and naval vessels, outside the bridle catcher 32 that stretches
End is provided with signal projector 42.
As shown in Fig. 1,2,3,4,5：Reclaiming pintle includes outer tube 11 and buffering shank 12, the front end activity of outer tube 11
Axle connects the posterior end of unmanned body 2, and bales catch, outer tube 11 and unmanned body 2 are provided between outer tube 11 and unmanned body 2
Between be provided with spring, outer tube 11 is flicked downwards, is additionally provided between outer tube 11 and unmanned body 2 spacing by spring all the time
Rope 13；
Buffering chute 14 is provided with outer tube 11, the rear end of outer tube 11 is provided with slide opening, buffering is movably set with slide opening
Shank 12, the front end for buffering shank 12 is provided with the limited block matched with buffering chute 14, slow between limited block and slide opening
Rush and buffer spring A16 is provided with shank 12；
The rear end for buffering shank 12 is provided with pintle 17, lock buckling groove 20 and switch groove 21 is provided with pintle 17, in lock buckling groove 20
Automatic locking 18 is movably set with, spring A22 is provided between automatic locking 18 and pintle 17, spring A22 will lock automatically all the time
The outwards ejection of button 18, is movably set with self-clinching switch 19 in switch groove 21, set between self-clinching switch 19 and the bottom of switch groove 21
Spring B 23 is equipped with, the spring B 23 all the time pops up self-clinching switch 19, and self-clinching switch 19 will be locked automatically when popping up
Button 18 is clasped.
Claims (2)
1. island-type construction in retracting device, including naval vessels, unmanned body, pedestal and pintle is reclaimed, it is special on a kind of unmanned plane warship
The side that the pedestal described in being is fixed on island-type construction in the naval vessels is levied, folding sleeve, institute are connected with described pedestal
Flexible bridle catcher is movably set with the folding sleeve stated, is set between described flexible bridle catcher and described folding loop bar and stretched
Contracting device；
The two ends of the pedestal are each provided with leading block, and cabletype hitch, described cable wire are provided with described pedestal
Draw-gear includes motor, decelerator and traction sheave, and fixed lasso is provided with the folding sleeve, the fixed lasso
Outside is movably set with connection lasso, is set on the folding sleeve between described fixed lasso and described connection lasso
The side for having buffer spring B, the connection lasso is provided with hauling rope, and the other end of the hauling rope passes through leading described in two
To the opposite side that the connection lasso is fixed on after pulley, described hauling rope is wrapped on described traction sheave；
Heavy burden tie-down cable, the flexible recovery are provided with described connection lasso and the naval vessels between the upper end of island-type construction
The outer end of bar is provided with signal projector.
2. retracting device on a kind of unmanned plane warship according to claim 1, described recovery pintle includes outer tube and slow
Rush shank, it is characterised in that the front end movable axis of the outer tube is connected on the posterior end of the unmanned body, described outer tube
Electric magnet hook is provided between described unmanned body, spring is provided between described outer tube and described unmanned body,
Described spring all the time flicks downwards described outer tube, is additionally provided between described outer tube and described unmanned body
Tie-down cable；
Buffering chute is provided with described outer tube, the rear end of the outer tube is provided with slide opening, activity in described slide opening
Described buffering shank is provided with, the front end of the buffering shank is provided with the limited block matched with described buffering chute,
Buffer spring A is provided with the buffering shank between described limited block and described slide opening；
The rear end of the buffering shank is provided with pintle, and lock buckling groove and switch groove, described lock are provided with described pintle
Automatic locking is movably set with groove, spring A, described spring A are provided between described automatic locking and described pintle
All the time described automatic locking is outwards ejected, self-clinching switch, described self-clinching switch is movably set with described switch groove
Spring B is provided with and the bottom of the switch groove between, described spring B all the time pops up described self-clinching switch, institute
The self-clinching switch stated clasps described automatic locking when popping up.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611017874.3A CN106742018B (en) | 2016-11-20 | 2016-11-20 | Recyclable device on a kind of unmanned plane warship |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611017874.3A CN106742018B (en) | 2016-11-20 | 2016-11-20 | Recyclable device on a kind of unmanned plane warship |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106742018A true CN106742018A (en) | 2017-05-31 |
| CN106742018B CN106742018B (en) | 2019-05-10 |
Family
ID=58969056
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611017874.3A Active CN106742018B (en) | 2016-11-20 | 2016-11-20 | Recyclable device on a kind of unmanned plane warship |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106742018B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107336828A (en) * | 2017-07-06 | 2017-11-10 | 上海复亚通信科技有限公司 | A kind of unmanned plane provided with bridle catcher |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1011733A (en) * | 1911-04-29 | 1911-12-12 | Hensley T Ballew | Mail device. |
| US2989272A (en) * | 1958-11-19 | 1961-06-20 | All American Eng Co | Aircraft tail hook assembly |
| US20090224097A1 (en) * | 2006-07-31 | 2009-09-10 | Amnon Kariv | Unmanned aerial vehicle launching and landing system |
| EP2186728A1 (en) * | 2008-11-14 | 2010-05-19 | The Boeing Company | Unmanned air vehicle recovery system |
| CN102625766A (en) * | 2009-04-24 | 2012-08-01 | 英西图公司 | Systems and methods for recovering and controlling post-recovery motion of unmanned aircraft |
| FR2962408B1 (en) * | 2010-07-09 | 2013-05-17 | Innovations Technologiques Et Ind Avancees Par Abreviation S I T I A Soc D | DEVICE FOR RECOVERING AND, PREFERABLY, LAUNCHING FLYING OBJECT |
| CN203078761U (en) * | 2012-11-21 | 2013-07-24 | 耿全水 | Capture anchor used for shipboard aircraft landing |
| CN106628223A (en) * | 2016-11-20 | 2017-05-10 | 宁波市镇海丹发机械科技有限公司 | Naval vessel unmanned aerial vehicle recycling device |
-
2016
- 2016-11-20 CN CN201611017874.3A patent/CN106742018B/en active Active
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1011733A (en) * | 1911-04-29 | 1911-12-12 | Hensley T Ballew | Mail device. |
| US2989272A (en) * | 1958-11-19 | 1961-06-20 | All American Eng Co | Aircraft tail hook assembly |
| US20090224097A1 (en) * | 2006-07-31 | 2009-09-10 | Amnon Kariv | Unmanned aerial vehicle launching and landing system |
| EP2186728A1 (en) * | 2008-11-14 | 2010-05-19 | The Boeing Company | Unmanned air vehicle recovery system |
| CN102625766A (en) * | 2009-04-24 | 2012-08-01 | 英西图公司 | Systems and methods for recovering and controlling post-recovery motion of unmanned aircraft |
| FR2962408B1 (en) * | 2010-07-09 | 2013-05-17 | Innovations Technologiques Et Ind Avancees Par Abreviation S I T I A Soc D | DEVICE FOR RECOVERING AND, PREFERABLY, LAUNCHING FLYING OBJECT |
| CN203078761U (en) * | 2012-11-21 | 2013-07-24 | 耿全水 | Capture anchor used for shipboard aircraft landing |
| CN106628223A (en) * | 2016-11-20 | 2017-05-10 | 宁波市镇海丹发机械科技有限公司 | Naval vessel unmanned aerial vehicle recycling device |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107336828A (en) * | 2017-07-06 | 2017-11-10 | 上海复亚通信科技有限公司 | A kind of unmanned plane provided with bridle catcher |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106742018B (en) | 2019-05-10 |
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Effective date of registration: 20201223 Address after: 225700 No. 1 Chuang Road, Zhaoyang street, Xinghua, Taizhou, Jiangsu. Patentee after: XINGHUA TIANDONG SOFTWARE TECHNOLOGY Co.,Ltd. Address before: NO.201, No.13, Mingnan Road, Zhaobaoshan street, Zhenhai District, Ningbo City, Zhejiang Province Patentee before: NINGBO ZHENHAI DANFA MACHINERY TECHNOLOGY Co.,Ltd. |
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Effective date of registration: 20211230 Address after: 274000 in Antong Logistics Institute, economic development zone, Dingtao District, Heze City, Shandong Province Patentee after: Shandong Ba Ling special cable Co.,Ltd. Address before: 225700 No. 1 Chuang Road, Zhaoyang street, Xinghua, Taizhou, Jiangsu. Patentee before: XINGHUA TIANDONG SOFTWARE TECHNOLOGY Co.,Ltd. |