CN106477065B - 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
- CN106477065B CN106477065B CN201611140374.9A CN201611140374A CN106477065B CN 106477065 B CN106477065 B CN 106477065B CN 201611140374 A CN201611140374 A CN 201611140374A CN 106477065 B CN106477065 B CN 106477065B
- Authority
- CN
- China
- Prior art keywords
- receiver
- 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.)
- Active
Links
- 239000000872 buffer Substances 0.000 claims abstract description 18
- 238000003032 molecular docking Methods 0.000 claims abstract description 13
- 238000005265 energy consumption Methods 0.000 claims abstract description 6
- 230000035939 shock Effects 0.000 claims abstract description 4
- 238000009434 installation Methods 0.000 claims description 2
- 238000000034 method Methods 0.000 abstract description 5
- 230000008569 process Effects 0.000 abstract description 4
- 230000009977 dual effect Effects 0.000 abstract 1
- 238000010586 diagram Methods 0.000 description 7
- 230000000903 blocking effect Effects 0.000 description 5
- 238000005516 engineering process Methods 0.000 description 4
- 239000000523 sample Substances 0.000 description 4
- 230000003139 buffering effect Effects 0.000 description 3
- 230000009471 action Effects 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
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 239000000243 solution Substances 0.000 description 2
- -1 12-1 Substances 0.000 description 1
- 206010000369 Accident Diseases 0.000 description 1
- 206010061876 Obstruction Diseases 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 230000015572 biosynthetic process Effects 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
- 239000002184 metal Substances 0.000 description 1
- 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 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)
- Tires In General (AREA)
- Traffic Control Systems (AREA)
Abstract
The invention discloses a kind of anti-formula carrier-borne aircrafts of throwing to block rope device, comprising: is set to the ejector of carrier-borne drive end unit and is installed on the receiver of type aircraft carrier deck；Receiver is connect with energy consumption deceleration device, and what ejector ejected, which block rope end, is provided with catcher；Catcher end is provided with the buffer for shock absorbing；After catcher pops up by ejector and enters receiver, the receptor in receiver contacts triggering signal acquisition with catcher；Bonder is bonded with the cooperation of rope end is blocked；The tightener of receiver open end setting being open for being closed receiver, operating instant tightening；And then realize docking, connection, locking, energy consumption, connection and locking process realize dual connection guarantee further through bonder and tightener, final to realize steady warship.
Description
Technical field
The present invention relates to aircraft-carrier-deck facilities, in particular to instead throw formula carrier-borne aircraft and block rope device.
Background technique
Presently, there are technology in, mostly stopped based on carrier-borne aircraft with arrester wires and barrier, by by carrier-borne aircraft and stopping
Rope links or barrier collision realizes that carrier-borne aircraft stops.If hook cannot successfully link arrester wires, stop failure or
Fatal crass or pilot go around, and prepare secondary obstruction, but success rate is very low, and risk is very big, the overwhelming majority
Carrier-borne aircraft accident all betides warship moment, and it is due to hook problem that reason is also mostly.
Summary of the invention
The present invention in view of the above technical problems, proposes a kind of safety, exempts from precisely to align, and efficient anti-formula carrier-borne aircraft of throwing blocks rope
Device.
To achieve the above objectives, it is achieved through the following technical solutions:
Anti- formula carrier-borne aircraft of throwing blocks rope device, comprising: is set to the ejector of carrier-borne drive end unit and is installed on type aircraft carrier deck
Receiver；
Wherein, receiver is connect with energy consumption deceleration device, and what ejector ejected, which block rope end, is provided with catcher；
Catcher end is provided with the buffer for shock absorbing；
Receiver includes: the shell and receptor of the hemisphere structure of plane end opening and inner hollow；
Receptor is several, and is uniformly arranged on the inner wall surface of the shell of receiver；
Bonder is set in catcher；
Wherein, receptor contacts triggering signal acquisition with catcher；Bonder is bonded with the cooperation of rope end is blocked；
Receiver open end is provided with the tightener for being closed receiver opening, and the control circuit and impression of tightener
Device contacts the control circuit connection of the signal acquisition of triggering with catcher；
Wherein, the position limiting convex ring that bitter end portion outer wall is provided with radial protrusion is blocked；
Further, tightener is that horizontal slide rail formula flygate translates clamping device, and the clamping door-plate docking of tightener
Edge preset has a docking semicircle orifice, and docks diameter after semicircle orifice docking and be more than or equal to block rope end diameter and be less than and block rope end
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 the diameter of position limiting convex ring, this structure
It docks and is realized with the position limiting convex ring for blocking rope and limited.
The present invention by adopting the above technical scheme, carrier-borne aircraft are carried out the pop-up of tail portion ejector first and are blocked when close to aircraft carrier
The ejection of rope prepares, and has the police radar on aircraft to measure the position for being suitble to ejection to block rope, is suitble to the position launched when reaching aircraft
When setting, airplane tail group blocks rope to ejection in front of two sides, blocks the end of rope with catcher, catcher enters receiver hemisphere body shell
In body, the moment that any one receptor touches on catcher and receiver shell inner wall, signal acquisition, signal acquisition will be triggered
Control circuit handles the bonding that catcher end is bonding to by bonder simultaneously and acts, while controlling and receiving device upper opening position
Tightener tighten rapidly to be closed by track and firmly grasps the limit for blocking bitter end portion, at this point, receiver with eject to block rope close
Connection, and associated movement.If bonder fails to bond catcher completely, catcher is detached from, at this moment fast in tightener
In the case where speed closure, the docking for blocking the realization of the position limiting convex ring on rope to catcher can be still blocked.
In whole process, to prevent catcher ends points to be damaged when colliding with receiver, set in catcher end
Buffer is set, plays the role of buffer protection to catcher.
After docking successfully, reception device feedback signal, aircraft, which can reduce speed now, does landing preparation, the connection of the receiver other end
Consume energy deceleration device, carries out deceleration control against warship aircraft, final steady the warship for realizing aircraft.
To sum up, the present invention is to block rope from the included end catcher of the tail portion of carrier-borne aircraft ejection before carrier-borne aircraft landing,
Docked using catcher with receiver on carrier-borne aircraft deck, cable system is blocked in formation, thus realize carrier-borne aircraft quickly, it is accurate,
Safety type aircraft carrier deck warship.Commonly block the coupling type of rope warship mode, even if carrier-borne aircraft driver have it is very superb
Warship technology, landing mission also can be very dangerous, especially night warship, block Suo Buyi and accurately link up with, cause fatal crass's
May be very big, commonly block the coupling type of rope warship mode be current aircraft carrier a most dangerous ring for warship.And this Shen
Technical solution please avoids problem above, warship can all carry out in any environment, once occur throw connect fault, pilot can
To shift to an earlier date awareness information (catcher and receiver unmated on), provide grace time to taking off again, strong guarantee warship peace
Entirely.The device is small, easy for installation, does not occupy deck space excessively.
The above description is only an overview of the technical scheme of the present invention, in order to better understand the technical means of the present invention,
And it can be implemented in accordance with the contents of the specification, and in order to allow above and other objects, features and advantages of the invention can
It is clearer and more comprehensible, it is special below to lift preferred embodiment, and cooperate attached drawing, detailed description are as follows.
Detailed description of the invention
The present invention totally 7 width attached drawing, in which:
Fig. 1 is structural schematic diagram when rope is blocked in ejector ejection of the invention.
Fig. 2 is structural schematic diagram when carrier-borne aircraft landing of the invention is completed.
Fig. 3 is receiver open ended structure schematic diagram of the invention.
Fig. 4 is the schematic diagram of the section structure of receiver open state of the invention.
Fig. 5 is the schematic diagram of the section structure of receiver closed state of the invention.
Fig. 6 is buffer structure schematic diagram of the invention.
Fig. 7 is bonder end construction schematic diagram of the invention.
In figure: 1, type aircraft carrier deck, 2, receiver, 3, catcher, 4, block rope, 5, carrier-borne aircraft, 6, ejector, 7, tightener,
10, 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, receptor, 14, probe.
Specific embodiment
As shown in Figure 1, Figure 2, Fig. 3, Fig. 4, Fig. 5, Fig. 6 and anti-throwing formula carrier-borne aircraft shown in Fig. 7 block rope device, comprising: are set to
The ejector 6 of carrier-borne drive end unit and the receiver 2 for being installed on type aircraft carrier deck；
Wherein, receiver 2 is connect with energy consumption deceleration device, and what ejector 6 ejected, which block 4 end of rope, is provided with catcher
3；
3 end of catcher is provided with the buffer 12 for shock absorbing；
Wherein, as shown in fig. 6, buffer 12 includes: the buffer base 12-3 fixed with catcher 3, it is set to buffering
Spring buffer cylinder 12-2 on the device pedestal 12-3 and buffer header 12-1 for being set to the front end spring buffer cylinder 12-2；
Buffer header 12-1 first with i.e. contacts collision object, is then realized by spring buffer cylinder 12-2 flexible
Buffering in the process (buffering is main to be realized by spring)；
Receiver 2 includes: the shell and receptor 13 of the hemisphere structure of plane end opening and inner hollow；
Receptor 13 is several, and is uniformly arranged on the inner wall surface of the shell of receiver 2；
Bonder 11 is set in catcher 3；
Wherein, receptor 13 contacts triggering signal acquisition with catcher 3；Bonder 11 is bonded with the cooperation of 4 end of rope is blocked, this
Place's bonder 11 uses electromagnetic adsorption type structure and blocks 4 end of rope to be connected again with magnetic or adsorbable metal combination absorption
It connects；
As shown in fig. 7, bonder end 11-1 is the cylinder base for having cavity for placing the inside of probe 4, bonding
Setting signal transmitter inside the 11-2 of device bottom；
Probe is located at bonder end, and when carrier-borne aircraft landing, ejector 6 pops up catcher 3, contains in catcher 3 slow
Device 12 and bonder 11 are rushed, wherein there is probe 4 in the end of bonder 11, and receptor 13 on receiver 2 is facilitated to incude catcher 3
Position, and issued by signal projector to induction signal, final accurate reception catcher 3；
2 open end of receiver be provided with for be closed receiver 2 opening tightener 7, and the control circuit of tightener 7 with
Receptor 13 contacts the control circuit connection of the signal acquisition of triggering with catcher 3；
Wherein, the position limiting convex ring 10 that 4 end outer wall of rope is provided with radial protrusion is blocked；
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 it is last less than rope 4 is blocked more than or equal to 4 end diameter of rope is blocked to dock diameter after semicircle orifice docks
The diameter of the position limiting convex ring 10 at end, this structure will make pair of two clamping door-plates by the closed action of the clamping door-plate of tightener 7
It connects semicircle orifice docking and is realized with the position limiting convex ring 10 for blocking rope 4 and limited.
The present invention by adopting the above technical scheme, carrier-borne aircraft are carried out the pop-up of tail portion ejector 6 first and are blocked when close to aircraft carrier
The ejection of rope 4 prepares, and has the police radar on aircraft to measure the position for being suitble to ejection to block rope 4, is suitble to ejection when reaching aircraft
When position, airplane tail group blocks rope 4 to ejection in front of two sides, blocks the end of rope 4 with catcher 3, catcher 3 enters receiver 2
In hemisphere shell, the moment that any one receptor 13 touches on catcher 3 and 2 inner walls of receiver captures triggering
Signal, signal acquisition control circuit handles the bonding that 3 end of catcher is bonding to by bonder 11 simultaneously and acts, while control connects
The tightener 7 for receiving 2 upper opening position of device tightens rapidly closure by track and firmly grasps the limit for blocking 4 end of rope, at this point, receiver
2 closely connect with the rope 4 that blocks ejected, and associated movement.If bonder 11 fails to bond catcher completely, catcher 3
It is detached from, at this moment in the case where 7 rapid closing of tightener, can still block the realization pair of position limiting convex ring 10 blocked on rope 4
The docking of catcher.
In whole process, to prevent 3 ends points of catcher to be damaged when colliding with receiver 2, in 3 end of catcher
Buffer 12 is set, plays the role of buffer protection to catcher 3.
After docking successfully, reception device feedback signal, aircraft, which can reduce speed now, does landing preparation, and 2 other end of receiver connects
Energy consumption deceleration device is connect, carries out deceleration control against warship aircraft, final steady the warship for realizing aircraft.
The above described is only a preferred embodiment of the present invention, be not intended to limit the present invention in any form, though
So the present invention has been disclosed as a preferred embodiment, and however, it is not intended to limit the invention, any technology people for being familiar with this profession
Member without departing from the scope of the present invention, when the technology contents using the disclosure above are modified or are modified to
The equivalent embodiment of equivalent variations, but anything that does not depart from the technical scheme of the invention content, it is right according to the technical essence of the invention
Any simple modification, equivalent change and modification made for any of the above embodiments, all of which are still within the scope of the technical scheme of the invention.
Claims (1)
1. instead throwing formula carrier-borne aircraft blocks rope device, it is characterised in that: including being set to ejector (6) and the installation of carrier-borne drive end unit
In the receiver (2) of type aircraft carrier deck；
Wherein, receiver (2) is connect with energy consumption deceleration device, and what ejector (6) ejected, which block rope (4) end, is provided with capture
Device (3)；
Catcher (3) end is provided with the buffer (12) for shock absorbing；
The receiver (2) includes: the shell and receptor (13) of the hemisphere structure of plane end opening and inner hollow；
The receptor (13) is several, and is uniformly arranged on the inner wall surface of the shell of receiver (2)；
Bonder (11) is set in catcher (3)；
Wherein, receptor (13) contacts triggering signal acquisition with catcher (3)；Bonder (11) is glued with the cooperation of rope (4) end is blocked
Knot；
Receiver (2) open end is provided with the tightener (7) for being closed receiver (2) opening, and the control of tightener (7)
Circuit processed contacts the control circuit connection of the signal acquisition of triggering with receptor (13) with catcher (3)；
Wherein, the position limiting convex ring (10) that rope (4) end outer wall is provided with radial protrusion is blocked；
The tightener (7) is that horizontal slide rail formula flygate translates clamping device, and the clamping door-plate abutting edge of tightener (7)
It is preset with docking semicircle orifice, and docks diameter after semicircle orifice docking and be more than or equal to block rope (4) end diameter and be less than and block rope (4) end
Position limiting convex ring (10) diameter.
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 CN106477065A (en) | 2017-03-08 |
| CN106477065B true CN106477065B (en) | 2019-02-12 |
Family
ID=58284726
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611140374.9A Active 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) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113086094B (en) * | 2021-04-21 | 2022-04-19 | 鹏城实验室 | Unmanned underwater vehicle recovery system and recovery method |
Citations (12)
| 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 |
| CN102358430A (en) * | 2011-07-27 | 2012-02-22 | 南京航空航天大学 | Ship-borne aircraft capturing and arresting device |
| 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 |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2767506B2 (en) * | 1991-09-19 | 1998-06-18 | 三井造船株式会社 | Aircraft mobile equipment platform |
| KR101265784B1 (en) * | 2011-07-06 | 2013-05-20 | 부산대학교 산학협력단 | Helicopter landing apparatus |
-
2016
- 2016-12-12 CN CN201611140374.9A patent/CN106477065B/en active Active
Patent Citations (12)
| 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 |
| 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 |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106477065A (en) | 2017-03-08 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN104760705B (en) | Vehicle-mounted aircraft lifting gear | |
| EP0227229B1 (en) | Helicopter rapid securing and traversing system | |
| CN202609086U (en) | Downwards-throwing popup type parachute opening device of unmanned plane | |
| WO2016203322A3 (en) | Search and rescue drone arrangement | |
| CN106477065B (en) | Anti- formula carrier-borne aircraft of throwing blocks rope device | |
| CN203305949U (en) | Window breaking device | |
| CN201777389U (en) | Aircraft loading bridge capable of carrying out chain breakage detection and protection | |
| CN202609087U (en) | Downward dropping type flexible-connection cabin cover parachute-opening device of push-back type mini-sized pilotless plane | |
| CN106081778A (en) | A kind of bidirectional braking device of the band warning function for elevator | |
| CN106005363A (en) | Aircraft with air crash lifesaving function | |
| US20190047702A1 (en) | Aerial vehicle | |
| CN103802700B (en) | A kind of automotive seat buffer device for collision | |
| CN106628223B (en) | Naval vessels unmanned plane recyclable device | |
| US6789766B2 (en) | Cargo drop system with cargo parachute and process for stabilization of a cargo drop system by means of a cargo parachute following the drop from the aircraft | |
| CN103350754B (en) | The delivery device of the plug-in load of a kind of pneumatic type | |
| UA108839C2 (en) | METHOD AND DEVICE FOR TRANSPORTING MATERIALS SUITABLE FOR TRANSPORT | |
| CN206589837U (en) | A kind of automobile with collision ejecting type driving cabin | |
| CN106742018B (en) | Recyclable device on a kind of unmanned plane warship | |
| CN103863560A (en) | Automatic shipboard aircraft forced landing tail hook with adjustable arm length | |
| CN203078761U (en) | Capture anchor used for shipboard aircraft landing | |
| CN103809280B (en) | Pilot's night vision goggles pin rod formula arming mechanism | |
| CN203698019U (en) | Vehicle seat collision buffering device | |
| EP3362362B1 (en) | Low engagement force aerial refueling coupling | |
| CN216332808U (en) | Unmanned aerial vehicle flight buffer stop | |
| CN106950993A (en) | The controllable unmanned plane of headroom spatial domain flight path |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | 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 |