CN107856873A - Tail end buckle montant blocks the carrier landing device that rope grabs company with gate-type frame - Google Patents
Tail end buckle montant blocks the carrier landing device that rope grabs company with gate-type frame Download PDFInfo
- Publication number
- CN107856873A CN107856873A CN201711063485.9A CN201711063485A CN107856873A CN 107856873 A CN107856873 A CN 107856873A CN 201711063485 A CN201711063485 A CN 201711063485A CN 107856873 A CN107856873 A CN 107856873A
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- CN
- China
- Prior art keywords
- carrier
- support frame
- hook
- walking dolly
- rope
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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
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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—Arresting gear; Liquid barriers
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Tires In General (AREA)
Abstract
The invention discloses a kind of tail end buckle montant and gate-type frame to block the carrier landing device that rope grabs company, including：Two support rails being set in parallel in type aircraft carrier deck, support frame, block rope and be arranged on the hook of carrier-borne machine tail end；The walking dolly coordinated with it is provided with each support rail, a damper is provided with below each support rail, a support frame is fixed with each walking dolly, support frame is hinged with walking dolly, and the drive device that driving support frame upset raises up is provided with walking dolly；Block rope both ends to be connected with two dampers respectively, be oriented to and assembled finally between two support rails by support frame；Link up with and linked up with to be flexible, and telescopic direction is vertically upward, card fixation to be hooked rapidly when hook hook blocks Suo Houke；Using the present invention of above-mentioned technical proposal, when carrier-borne aircraft is when close to aircraft carrier, the drive device driving support frame upset of walking dolly will block Suo Zhiqi, walking dolly adjustment position on its track, be prepared with the interception that this type aircraft carrier deck is carried out to carrier-borne aircraft.
Description
Technical field
The present invention relates to carrier-borne aircraft landing blocking apparatus, more particularly to a kind of tail end buckle montant blocks rope with gate-type frame and grabs company
Carrier landing device.
Background technology
The arrester wires technology that presently, there are be linked after carrier-borne aircraft landing with the arrester wires in type aircraft carrier deck realize it is carrier-borne
Machine is stopped, and carrier-borne aircraft is possible in hooking process to be occurred to hook the situation for unsuccessfully needing to go around, it is also possible to is occurred because aligning not
Caused by accurate, there is very big danger in the situation of collision type aircraft carrier deck.Carrier-borne aircraft land initially due to flying speed still
It is very high, therefore pintle is hung when blocking rope, is very easy to make with the problems such as spring because the flight of excessive velocities or aircraft is unstable
Arrester wires can not be successfully linked into hook, then stops failure, otherwise fatal crass, or pilot is gone around, prepares secondary
Stop, but success rate is very low, and dangerous very big, most carrier-borne aircraft accidents all betide warship moment, it can be seen that
Hook the importance of success rate.
The content of the invention
The present invention is directed to above-mentioned technical problem, proposes that a kind of higher tail end buckle montant of security blocks rope with gate-type frame and grabbed
Carrier landing device even.
To achieve the above objectives, it is achieved through the following technical solutions：
A kind of tail end buckle montant blocks the carrier landing device that rope grabs company with gate-type frame, including：Two are set in parallel in
Support rail, support frame in type aircraft carrier deck, block rope and be arranged on the hook of carrier-borne machine tail end；
The walking dolly coordinated with it is provided with each support rail, one is provided with below each support rail
Damper, a support frame is fixed with each walking dolly, support frame is hinged with walking dolly, and is set on walking dolly
There is the drive device that driving support frame upset raises up；
Block rope both ends to be connected with two dampers respectively, assembling is oriented to finally across two support rails by support frame
Between；
Link up with and be made up of for flexible hook, this hook gib head, hook arm and longitudinal damper, and telescopic direction be vertically to
On.
Using the carrier aircraft of the present invention of above-mentioned technical proposal when close to aircraft carrier, the drive device driving support frame of walking dolly
Upset, will block Suo Zhiqi (block rope and pass through support frame connection damper), walking dolly adjustment position on its track, with this aircraft carrier
The interception that deck carries out to carrier-borne aircraft prepares.When carrier-borne aircraft prepare land when, carrier-borne aircraft stretch out afterbody hook, make hook vertically to
On, adjustment height and flight angle are from blocking below rope by while catching hook and hanging up and block rope.After success hook blocks rope, with
Carrier-borne aircraft drop to decelerating flight in type aircraft carrier deck, and support frame gradually fell, and what grapple snatch was lived, which blocks rope, will drive deck of sub-cellar
The damping system work of upper setting.In above procedure, support block rope and support frame be adjusted flexibly can cause it is carrier-borne
The hook of machine catches hook, and to block Suo Gengjia accurate, while can also avoid old-fashioned obstruction mode to ensure that successfully hook may produce
The collision of carrier-borne drive end unit and type aircraft carrier deck infringement.
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 specification, 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 of the drawings
Totally 5 width accompanying drawing of the invention, wherein：
Fig. 1 is the rough package drawing of the present invention；
The preparation that Fig. 2 is the present invention intercepts view；
Schematic diagram when Fig. 3 is the interception of the present invention；
Fig. 4 is top view after interception of the invention；
Fig. 5 is the hook of the present invention and blocks rope cooperation schematic diagram.
In figure：1st, type aircraft carrier deck, 2, support rail, 3, block rope, 4, support frame, 5, damper, 6, carrier-borne aircraft, 7, hang
Hook.
Embodiment
As shown in Figure 1, Figure 2, a kind of two support rails being set in parallel in type aircraft carrier deck 1 shown in Fig. 3, Fig. 4 and Fig. 5
2nd, support frame 4, the hook 7 for blocking rope 3 and being arranged on the tail end of carrier-borne aircraft 6；
The walking dolly coordinated with it is provided with each support rail 2, each lower section of support rail 2 is provided with one
Individual damper 5, a support frame 4 is fixed with each walking dolly, support frame 4 is hinged with walking dolly, and walking dolly
On be provided with driving support frame 4 and overturn the drive device that raises up；
Block the both ends of rope 3 to be connected with two dampers 5 respectively, assembling is oriented to finally across two support frames by support frame 4
Between track 2；
Hook 7 is flexible hook, and this hook is made up of gib head, hook arm and longitudinal damper, and telescopic direction is vertical
Upwards.
Using the carrier aircraft of the present invention of above-mentioned technical proposal when close to aircraft carrier, the drive device driving support frame of walking dolly
4 upsets, will block rope 3 and prop and (block rope 3 and pass through the connection damper 5 of support frame 4), walking dolly adjustment position on its track, with
The interception that this type aircraft carrier deck carries out to carrier-borne aircraft prepares.When carrier-borne aircraft 6 prepares to land, carrier-borne aircraft stretches out afterbody hook 7, makes extension
Straight up, adjustment height and flight angle are from the lower section of rope 3 is blocked by the way that while arresting hook hangs up and blocks rope for hook.Success hook blocks rope 3
Afterwards, as carrier-borne aircraft drop to decelerating flight in type aircraft carrier deck, support frame 4 gradually fell, and what grapple snatch was lived, which will block rope, to drive
The damping system work set on deck of sub-cellar.In above procedure, being adjusted flexibly with blocking rope and support frame for supporting can be with
So that the hook of carrier-borne aircraft catches hook, to block Suo Gengjia accurate, while can also avoid old-fashioned obstruction mode to ensure that successfully hook can
Can carrier-borne drive end unit caused by meeting and the infringement of type aircraft carrier deck collision.
The above described is only a preferred embodiment of the present invention, any formal limitation not is made to the present invention, though
So the present invention is disclosed above with preferred embodiment, but is not limited to the present invention, any to be familiar with this professional technology people
Member without departing from the scope of the present invention, when the technology contents using the disclosure above make it is a little change or be modified to
The equivalent embodiment of equivalent variations, as long as being the content without departing from technical solution of the present invention, the technical spirit pair according to the present invention
Any simple modification, equivalent change and modification made for any of the above embodiments, in the range of still falling within technical solution of the present invention.
Claims (1)
1. a kind of tail end buckle montant blocks the carrier landing device that rope grabs company with gate-type frame, its feature includes：
Two support rails (2) being set in parallel in type aircraft carrier deck, support frame (4), block rope (3) and be arranged on carrier-borne aircraft
The hook (7) of tail end；
The walking dolly coordinated with it is provided with each support rail (2), one is provided with below each support rail (2)
Individual damper (5), a support frame (4) is fixed with each walking dolly, support frame (4) is hinged with walking dolly, and row
Walk to be provided with the drive device that driving support frame (4) upset raises up on dolly；
Described rope (3) both ends of blocking are connected with two dampers (5) respectively, and assembling is oriented to finally across two by support frame (4)
Between support rail (2)；
The hook (7) is flexible hook, and this hook is made up of gib head, hook arm and longitudinal damper, and telescopic direction is vertical
It is straight upward.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711063485.9A CN107856873A (en) | 2017-11-02 | 2017-11-02 | Tail end buckle montant blocks the carrier landing device that rope grabs company with gate-type frame |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711063485.9A CN107856873A (en) | 2017-11-02 | 2017-11-02 | Tail end buckle montant blocks the carrier landing device that rope grabs company with gate-type frame |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107856873A true CN107856873A (en) | 2018-03-30 |
Family
ID=61699983
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711063485.9A Pending CN107856873A (en) | 2017-11-02 | 2017-11-02 | Tail end buckle montant blocks the carrier landing device that rope grabs company with gate-type frame |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107856873A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110589005A (en) * | 2018-06-12 | 2019-12-20 | 王振牛 | Rescue method for injured fighter aircraft abnormal deflection aircraft carrier |
| CN112373711A (en) * | 2020-11-20 | 2021-02-19 | 哈尔滨工业大学 | Self-adaptive active blocking type recovery adjusting device for fixed-wing unmanned aerial vehicle |
| CN113212784A (en) * | 2021-06-28 | 2021-08-06 | 天津大学 | Meeting butt joint device for ferry airship |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2824877A1 (en) * | 1978-06-07 | 1979-12-20 | Messerschmitt Boelkow Blohm | Aircraft arrester gear - has extending fuselage and mounting to bring braking load through aircraft centre of gravity |
| CN202848037U (en) * | 2012-10-23 | 2013-04-03 | 成都纵横自动化技术有限公司 | Recovery device of cable-hanging type unmanned aerial vehicle |
| CN104002980A (en) * | 2013-02-21 | 2014-08-27 | 上海市南洋模范中学 | Carrier-based aircraft landing assist device |
| CN205203416U (en) * | 2015-11-13 | 2016-05-04 | 中国人民解放军国防科学技术大学 | Formula unmanned aerial vehicle recovery system is retired to carrier -borne track that receive and releases |
| CN205256690U (en) * | 2015-12-08 | 2016-05-25 | 东北大学 | Unmanned aerial vehicle transmission and recovery unit |
| US20170021943A1 (en) * | 2013-03-14 | 2017-01-26 | Aurora Flight Sciences Corporation | Capturing Hook for Aerial System |
| CN205952314U (en) * | 2016-08-11 | 2017-02-15 | 深圳光启空间技术有限公司 | Unmanned aerial vehicle launching appliance |
-
2017
- 2017-11-02 CN CN201711063485.9A patent/CN107856873A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2824877A1 (en) * | 1978-06-07 | 1979-12-20 | Messerschmitt Boelkow Blohm | Aircraft arrester gear - has extending fuselage and mounting to bring braking load through aircraft centre of gravity |
| CN202848037U (en) * | 2012-10-23 | 2013-04-03 | 成都纵横自动化技术有限公司 | Recovery device of cable-hanging type unmanned aerial vehicle |
| CN104002980A (en) * | 2013-02-21 | 2014-08-27 | 上海市南洋模范中学 | Carrier-based aircraft landing assist device |
| US20170021943A1 (en) * | 2013-03-14 | 2017-01-26 | Aurora Flight Sciences Corporation | Capturing Hook for Aerial System |
| CN205203416U (en) * | 2015-11-13 | 2016-05-04 | 中国人民解放军国防科学技术大学 | Formula unmanned aerial vehicle recovery system is retired to carrier -borne track that receive and releases |
| CN205256690U (en) * | 2015-12-08 | 2016-05-25 | 东北大学 | Unmanned aerial vehicle transmission and recovery unit |
| CN205952314U (en) * | 2016-08-11 | 2017-02-15 | 深圳光启空间技术有限公司 | Unmanned aerial vehicle launching appliance |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110589005A (en) * | 2018-06-12 | 2019-12-20 | 王振牛 | Rescue method for injured fighter aircraft abnormal deflection aircraft carrier |
| CN110589005B (en) * | 2018-06-12 | 2022-12-06 | 王振牛 | Rescue method for injured fighter aircraft abnormal deflection aircraft carrier |
| CN112373711A (en) * | 2020-11-20 | 2021-02-19 | 哈尔滨工业大学 | Self-adaptive active blocking type recovery adjusting device for fixed-wing unmanned aerial vehicle |
| CN112373711B (en) * | 2020-11-20 | 2022-06-24 | 哈尔滨工业大学 | Self-adaptive active blocking type recovery adjusting device for fixed-wing unmanned aerial vehicle |
| CN113212784A (en) * | 2021-06-28 | 2021-08-06 | 天津大学 | Meeting butt joint device for ferry airship |
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| PB01 | Publication | ||
| PB01 | Publication | ||
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| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180330 |
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| RJ01 | Rejection of invention patent application after publication |