CN106477065A - Anti- formula carrier-borne aircraft of throwing blocks rope device - Google Patents
Anti- formula carrier-borne aircraft of throwing blocks rope device Download PDFInfo
- Publication number
- CN106477065A CN106477065A CN201611140374.9A CN201611140374A CN106477065A CN 106477065 A CN106477065 A CN 106477065A CN 201611140374 A CN201611140374 A CN 201611140374A CN 106477065 A CN106477065 A CN 106477065A
- Authority
- CN
- China
- Prior art keywords
- receptor
- catcher
- rope
- carrier
- tightener
- 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
- 239000000872 buffer Substances 0.000 claims abstract description 18
- 230000000903 blocking effect Effects 0.000 claims abstract description 15
- 230000035939 shock Effects 0.000 claims abstract description 4
- 238000003032 molecular docking Methods 0.000 claims description 16
- 238000000034 method Methods 0.000 abstract description 7
- 230000008569 process Effects 0.000 abstract description 5
- 230000009977 dual effect Effects 0.000 abstract 1
- 210000001503 joint Anatomy 0.000 abstract 1
- 238000005516 engineering process Methods 0.000 description 5
- 239000000243 solution Substances 0.000 description 5
- 230000009471 action Effects 0.000 description 4
- 239000000523 sample Substances 0.000 description 4
- 230000003139 buffering effect Effects 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 206010061876 Obstruction Diseases 0.000 description 2
- 230000004888 barrier function Effects 0.000 description 2
- 239000007853 buffer solution Substances 0.000 description 2
- 230000008878 coupling Effects 0.000 description 2
- 238000010168 coupling process Methods 0.000 description 2
- 238000005859 coupling reaction Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- -1 12-1 Substances 0.000 description 1
- 206010000369 Accident Diseases 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000001179 sorption measurement Methods 0.000 description 1
- 230000001960 triggered effect Effects 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
- B64F1/04—Ground or aircraft-carrier-deck installations for launching aircraft
- B64F1/06—Ground or aircraft-carrier-deck installations for launching aircraft using catapults
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63G—OFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS; MINE-LAYING; MINE-SWEEPING; SUBMARINES; AIRCRAFT CARRIERS
- B63G11/00—Aircraft carriers
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Traffic Control Systems (AREA)
- Tires In General (AREA)
Abstract
The invention discloses a kind of anti-formula carrier-borne aircraft of throwing blocks rope device, including：The ejector being arranged at carrier-borne drive end unit and the receptor being installed on type aircraft carrier deck；Receptor is connected with power consumption deceleration device, and what ejector ejected block rope end is provided with catcher；Catcher end is provided with the buffer for shock absorbing；After ejector ejects and enters receptor, the sensor in receptor contacts triggering signal acquisition to catcher with catcher；Bonder bonds with blocking the cooperation of rope end；The tightener for closing receptor opening of receptor opening setting, operating instant is tightened up；And then achieve a butt joint, connect, lock, consume energy, connect and locking process realize dual connection guarantee further through bonder and tightener, final realize steadily warship.
Description
Technical field
The present invention relates to aircraft-carrier-deck facility, block rope device particularly to anti-formula carrier-borne aircraft of throwing.
Background technology
In the technology that presently, there are, how stopped based on carrier-borne aircraft with arrester wires and barrier, by by carrier-borne aircraft and obstruction
Rope links or barrier collision is realized carrier-borne aircraft and stopped.If hook successfully can not link arrester wires, stop unsuccessfully, or
Fatal crass, or pilot is gone around, prepares secondary obstruction, but success rate is very low, danger is very big, the overwhelming majority
Carrier-borne aircraft accident all betides warship moment, and reason is also mostly to be due to hook problem.
Content of the invention
The present invention is directed to above-mentioned technical problem, proposes a kind of safety, exempts from accurate para-position, efficiently instead throws formula carrier-borne aircraft and blocks rope
Device.
For reaching object above, it is achieved through the following technical solutions：
Anti- formula carrier-borne aircraft of throwing blocks rope device, including：It is arranged at the ejector of carrier-borne drive end unit and be installed on type aircraft carrier deck
Receptor；
Wherein, receptor is connected with power consumption deceleration device, and what ejector ejected block rope end is provided with catcher；
Catcher end is provided with the buffer for shock absorbing；
Receptor includes：The housing of hemisphere structure of plane end opening and inner hollow and sensor；
Sensor is several, and is uniformly arranged on the inner wall surface of the housing of receptor；
Bonder is arranged in catcher；
Wherein, sensor contacts triggering signal acquisition with catcher；Bonder bonds with blocking the cooperation of rope end；
Receptor opening is provided with the tightener for closing receptor opening, and the control circuit of tightener and impression
The control circuit that device contacts the signal acquisition of triggering with catcher connects；
Wherein, block the position limiting convex ring that bitter end portion outer wall is provided with radial protrusion；
Further, tightener is that horizontal slide rail formula flygate translates clamping device, and the clamping door-plate docking of tightener
Edge preset has docking semicircle orifice, and dock semicircle orifice docking after with diameter greater than be equal to block rope end diameter be less than block rope end
The diameter of position limiting convex ring, the amount of making is clamped the docking semicircle orifice of door-plate by the closed action of the clamping door-plate of tightener by this structure
Docking and with the position limiting convex ring blocking rope realize spacing.
Using the present invention of technique scheme, carrier-borne aircraft, when near aircraft carrier, is carried out the ejection of afterbody ejector first and is blocked
The ejection of rope prepares, and has the police radar on aircraft to record the position being suitable for that rope is blocked in ejection, when reaching the position that aircraft is suitable for launching
When putting, airplane tail group launches in front of both sides and blocks rope, and the end blocking rope carries catcher, and catcher enters receptor hemisphere body shell
In body, the moment that catcher is touched with any one sensor on receiver shell inwall, signal acquisition, signal acquisition will be triggered
Control circuit processes the bonding action that catcher end is bonding to by bonder simultaneously, controls receptor upper shed position simultaneously
Tightener pass through track tighten up rapidly close by block bitter end portion spacing promptly, now, receptor with eject to block rope tight
Connect, and associated movement.If bonder fails by catcher bonding completely, catcher departs from, at this moment fast in tightener
In the case of speed closure, still can block the position limiting convex ring blocking on rope and realize the docking to catcher.
In whole process, for preventing catcher ends points to be damaged when colliding with receptor, set in catcher end
Put buffer, catcher is played with the effect of buffer protection.
After docking success, reception device feeds back signal, and aircraft can reduce speed now and do landing preparation, and the receptor other end connects
Power consumption deceleration device, carries out deceleration control against warship aircraft, finally realize aircraft steadily warship.
To sum up, the present invention is before carrier-borne aircraft lands, and blocks rope from the ejection of the afterbody of carrier-borne aircraft from strap end portion catcher,
Using catcher and the docking of receptor on carrier-borne aircraft deck, formed and block cable system, thus realize carrier-borne aircraft quick, accurately,
The type aircraft carrier deck of safety warship.The coupling type commonly blocking rope warship mode, even if carrier-borne aircraft driver possess very superb
Warship technology, its landing mission also can be very dangerous, and especially night warship, blocks Suo Buyi and accurately links up with, causes fatal crass's
May be very big, the coupling type commonly blocking rope the ring the most dangerous that warship mode is that current aircraft carrier warship.And this Shen
Technical scheme please avoids problem above, warship and all can carry out in any environment, once occurring throwing to connect error, pilot can
To shift to an earlier date awareness information (catcher with receptor unmated on), to the offer grace time that takes off again, strong guarantee warship peace
Entirely.This device is small, easy for installation, does not excessively take deck space.
Described above is only the general introduction of technical solution of the present invention, in order to better understand the technological means of the present invention,
And can be practiced according to the content of description, and in order to allow the above and other objects, features and advantages of the present invention can
Become apparent, below especially exemplified by preferred embodiment, and coordinate accompanying drawing, describe in detail as follows.
Brief description
The present invention totally 7 width accompanying drawing, wherein：
Fig. 1 is that structural representation during rope is blocked in the ejector ejection of the present invention.
Structural representation when Fig. 2 completes for the carrier-borne aircraft landing of the present invention.
Fig. 3 is the receptor open ended structure schematic diagram of the present invention.
Fig. 4 is the cross-sectional view of the receptor opening of the present invention.
Fig. 5 is the cross-sectional view of the receptor closure state of the present invention.
Fig. 6 is the buffer structure schematic diagram of the present invention.
Fig. 7 is the bonder end construction schematic diagram of the present invention.
In figure：1st, type aircraft carrier deck, 2, receptor, 3, catcher, 4, block rope, 5, carrier-borne aircraft, 6, ejector, 7, tightener,
10th, position limiting convex ring, 11, bonder, 11-1, bonder end, 11-2, bonder bottom, 12, buffer, 12-1, buffer head
Portion, 12-2, spring buffer cylinder, 12-3, buffer base, 13, sensor, 14, probe.
Specific embodiment
As shown in Figure 1, Figure 2, the anti-throwing formula carrier-borne aircraft shown in Fig. 3, Fig. 4, Fig. 5, Fig. 6 and Fig. 7 blocks rope device, including：It is arranged at
The ejector 6 of carrier-borne drive end unit and the receptor 2 being installed on type aircraft carrier deck；
Wherein, receptor 2 is connected with power consumption deceleration device, and what ejector 6 ejected block rope 4 end is provided with catcher
3；
Catcher 3 end is provided with the buffer 12 for shock absorbing；
Wherein, as shown in fig. 6, buffer 12 includes：Fixing buffer base 12-3, is arranged at buffering with catcher 3
Spring buffer cylinder 12-2 on the device base 12-3 and buffer header 12-1 being arranged at spring buffer cylinder 12-2 front end；
Buffer header 12-1 first with will collision object contact, then pass through spring buffer cylinder 12-2 realize flexible
During buffering (buffering mainly realized by spring)；
Receptor 2 includes：The housing of hemisphere structure of plane end opening and inner hollow and sensor 13；
Sensor 13 is several, and is uniformly arranged on the inner wall surface of the housing of receptor 2；
Bonder 11 is arranged in catcher 3；
Wherein, sensor 13 contacts triggering signal acquisition with catcher 3；Bonder 11 bonds with blocking the cooperation of rope 4 end, this
Place's bonder 11 is connected again with magnetic or the absorption of adsorbable metal combination with blocking rope 4 end using electromagnetic adsorption type structure
Connect；
As shown in fig. 7, bonder end 11-1 is the cylinder base carrying cavity for placing the inside of probe 4, bonding
Setting signal projector inside the 11-2 of device bottom；
Probe is located at bonder end, and when carrier-borne aircraft lands, ejector 6 ejects catcher 3, contains slow in catcher 3
Rush device 12 and bonder 11, there is probe 4 end of wherein bonder 11, facilitate sensor 13 on receptor 2 to sense catcher 3
Position, and send to induction signal by signal projector, finally accurately receive catcher 3；
Receptor 2 opening is provided with the tightener 7 for closing receptor 2 opening, and the control circuit of tightener 7 with
The control circuit that sensor 13 contacts the signal acquisition of triggering with catcher 3 connects；
Wherein, block the position limiting convex ring 10 that rope 4 end outer wall is provided with radial protrusion；
Further, tightener 7 is that horizontal slide rail formula flygate translates clamping device, and the clamping door-plate pair of tightener 7
Edge fit edge is preset with docking semicircle orifice, and blocks rope 4 end with diameter greater than being equal to block rope 4 end diameter and be less than after docking semicircle orifice docking
The diameter of the position limiting convex ring 10 at end, the closed action that this structure passes through the clamping door-plate of tightener 7 will make the right of two clamping door-plates
Connect semicircle orifice docking and with the position limiting convex ring 10 blocking rope 4 realize spacing.
Using the present invention of technique scheme, carrier-borne aircraft, when near aircraft carrier, is carried out afterbody ejector 6 ejection first and is blocked
The ejection of rope 4 prepares, and has the police radar on aircraft to record the position being suitable for that rope 4 is blocked in ejection, is suitable for ejection when reaching aircraft
During position, airplane tail group launches in front of both sides and blocks rope 4, and the end blocking rope 4 carries catcher 3, and catcher 3 enters receptor 2
In hemisphere housing, the moment that catcher 3 is touched with any one sensor 13 in receptor 2 inner walls, triggering is caught
Signal, signal acquisition control circuit processes the bonding action that catcher 3 end is bonding to by bonder 11 simultaneously, controls simultaneously and connects
The tightener 7 of receipts device 2 upper shed position is tightened up rapidly by track to close and is firmly grasped blocking the spacing of rope 4 end, now, receptor
2 are closely connected with the rope 4 that blocks ejecting, and associated movement.If bonder 11 fails by catcher bonding completely, catcher 3
Depart from, at this moment in the case of tightener 7 rapid closing, still can block the position limiting convex ring 10 blocking on rope 4 realize right
The docking of catcher.
In whole process, for preventing catcher 3 ends points to be damaged when colliding with receptor 2, in catcher 3 end
Setting buffer 12, plays the effect of buffer protection to catcher 3.
After docking success, reception device feeds back signal, and aircraft can reduce speed now and do landing preparation, and receptor 2 other end is even
Connect power consumption deceleration device, carry out deceleration control against warship aircraft, finally realize aircraft steadily warship.
The above, be only presently preferred embodiments of the present invention, not the present invention is made with any pro forma restriction, though
So the present invention is disclosed above with preferred embodiment, but is not limited to the present invention, any is familiar with this professional technology people
Member, in the range of without departing from technical solution of the present invention, a little change or is modified to when the technology contents of available the disclosure above are made
The Equivalent embodiments of equivalent variations, as long as being the content without departing from technical solution of the present invention, according to the technical spirit pair of the present invention
Any simple modification made for any of the above embodiments, equivalent variations and modification, all still fall within the range of technical solution of the present invention.
Claims (2)
1. anti-throwing formula carrier-borne aircraft block rope device it is characterised in that：Including, be arranged at carrier-borne drive end unit ejector (6) and install
Receptor (2) in type aircraft carrier deck；
Wherein, receptor (2) is connected with power consumption deceleration device, and what ejector (6) ejected block rope (4) end is provided with seizure
Device (3)；
Described catcher (3) end is provided with the buffer (12) for shock absorbing；
Described receptor (2) includes：The housing of hemisphere structure of plane end opening and inner hollow and sensor (13)；
Described sensor (13) is several, and is uniformly arranged on the inner wall surface of the housing of receptor (2)；
Described bonder (11) is arranged in catcher (3)；
Wherein, sensor (13) contacts triggering signal acquisition with catcher (3)；Bonder (11) is glued with blocking the cooperation of rope (4) end
Knot；
Described receptor (2) opening is provided with the tightener (7) for closing receptor (2) opening, and the control of tightener (7)
The control circuit of the signal acquisition that circuit processed contacts triggering with sensor (13) with catcher (3) connects；
Wherein, block the position limiting convex ring (10) that rope (4) end outer wall is provided with radial protrusion.
2. anti-throwing formula carrier-borne aircraft according to claim 1 block rope device it is characterised in that：Described tightener (7) is horizontal
Slide rail type flygate translates clamping device, and the clamping door-plate abutting edge of tightener (7) is preset with docking semicircle orifice, and docks
Block, with diameter greater than being equal to, the diameter that rope (4) end diameter is less than the position limiting convex ring (10) blocking rope (4) end after semicircle orifice docking.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611140374.9A CN106477065B (en) | 2016-12-12 | 2016-12-12 | Anti- formula carrier-borne aircraft of throwing blocks rope device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611140374.9A CN106477065B (en) | 2016-12-12 | 2016-12-12 | Anti- formula carrier-borne aircraft of throwing blocks rope device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106477065A true CN106477065A (en) | 2017-03-08 |
| CN106477065B CN106477065B (en) | 2019-02-12 |
Family
ID=58284726
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611140374.9A Expired - Fee Related CN106477065B (en) | 2016-12-12 | 2016-12-12 | Anti- formula carrier-borne aircraft of throwing blocks rope device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106477065B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113086094A (en) * | 2021-04-21 | 2021-07-09 | 鹏城实验室 | Unmanned underwater vehicle recovery system and recovery method |
Citations (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3178132A (en) * | 1962-12-06 | 1965-04-13 | Dowty Rotol Ltd | Aircraft and devices for launching same |
| GB1223374A (en) * | 1969-04-14 | 1971-02-24 | All American Eng Co | Aircraft arresting system |
| EP0497646A1 (en) * | 1991-01-29 | 1992-08-05 | Grumman Aerospace Corporation | Vtol aircraft convertible shipping container |
| JPH0577795A (en) * | 1991-09-19 | 1993-03-30 | Mitsui Eng & Shipbuild Co Ltd | Movable equipment table for flying object |
| CN102358430A (en) * | 2011-07-27 | 2012-02-22 | 南京航空航天大学 | Ship-borne aircraft capturing and arresting device |
| KR20130005503A (en) * | 2011-07-06 | 2013-01-16 | 부산대학교 산학협력단 | Helicopter landing apparatus |
| CN103204245A (en) * | 2013-04-11 | 2013-07-17 | 西南交通大学 | Auxiliary landing device for shipboard aircraft of aircraft carrier |
| CN103507964A (en) * | 2012-06-16 | 2014-01-15 | 姜汝诚 | Aircraft catapult-assisted take-off device and aircraft landing stopping device |
| CN203428025U (en) * | 2013-07-31 | 2014-02-12 | 张大川 | Aircraft carrier-based aircraft landing stern hook and accessory device thereof |
| CN103879563A (en) * | 2012-12-23 | 2014-06-25 | 吴汉民 | Speed-reducing and stopping device for aircraft landing |
| CN204184565U (en) * | 2011-12-02 | 2015-03-04 | 达塔尼恩有限公司 | The guiding device of a kind of airship logon device and airship and logon device |
| CN104670517A (en) * | 2015-03-09 | 2015-06-03 | 许木子 | Helicopter landing fixing and takeoff ejection system |
| CN104760705A (en) * | 2015-02-15 | 2015-07-08 | 南京理工大学 | Vehicle-mounted aircraft taking-off and landing device |
| CN104960671A (en) * | 2015-06-15 | 2015-10-07 | 南京航空航天大学 | Landing electromagnetic damping system for shipboard aircraft |
-
2016
- 2016-12-12 CN CN201611140374.9A patent/CN106477065B/en not_active Expired - Fee Related
Patent Citations (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3178132A (en) * | 1962-12-06 | 1965-04-13 | Dowty Rotol Ltd | Aircraft and devices for launching same |
| GB1223374A (en) * | 1969-04-14 | 1971-02-24 | All American Eng Co | Aircraft arresting system |
| EP0497646A1 (en) * | 1991-01-29 | 1992-08-05 | Grumman Aerospace Corporation | Vtol aircraft convertible shipping container |
| JPH0577795A (en) * | 1991-09-19 | 1993-03-30 | Mitsui Eng & Shipbuild Co Ltd | Movable equipment table for flying object |
| KR20130005503A (en) * | 2011-07-06 | 2013-01-16 | 부산대학교 산학협력단 | Helicopter landing apparatus |
| CN102358430A (en) * | 2011-07-27 | 2012-02-22 | 南京航空航天大学 | Ship-borne aircraft capturing and arresting device |
| CN204184565U (en) * | 2011-12-02 | 2015-03-04 | 达塔尼恩有限公司 | The guiding device of a kind of airship logon device and airship and logon device |
| CN103507964A (en) * | 2012-06-16 | 2014-01-15 | 姜汝诚 | Aircraft catapult-assisted take-off device and aircraft landing stopping device |
| CN103879563A (en) * | 2012-12-23 | 2014-06-25 | 吴汉民 | Speed-reducing and stopping device for aircraft landing |
| CN103204245A (en) * | 2013-04-11 | 2013-07-17 | 西南交通大学 | Auxiliary landing device for shipboard aircraft of aircraft carrier |
| CN203428025U (en) * | 2013-07-31 | 2014-02-12 | 张大川 | Aircraft carrier-based aircraft landing stern hook and accessory device thereof |
| CN104760705A (en) * | 2015-02-15 | 2015-07-08 | 南京理工大学 | Vehicle-mounted aircraft taking-off and landing device |
| CN104670517A (en) * | 2015-03-09 | 2015-06-03 | 许木子 | Helicopter landing fixing and takeoff ejection system |
| CN104960671A (en) * | 2015-06-15 | 2015-10-07 | 南京航空航天大学 | Landing electromagnetic damping system for shipboard aircraft |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113086094A (en) * | 2021-04-21 | 2021-07-09 | 鹏城实验室 | Unmanned underwater vehicle recovery system and recovery method |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106477065B (en) | 2019-02-12 |
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Granted publication date: 20190212 |