CN103204245A - Auxiliary landing device for shipboard aircraft of aircraft carrier - Google Patents
Auxiliary landing device for shipboard aircraft of aircraft carrier Download PDFInfo
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- CN103204245A CN103204245A CN 201310145881 CN201310145881A CN103204245A CN 103204245 A CN103204245 A CN 103204245A CN 201310145881 CN201310145881 CN 201310145881 CN 201310145881 A CN201310145881 A CN 201310145881A CN 103204245 A CN103204245 A CN 103204245A
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- elastic rope
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Abstract
The invention discloses an auxiliary landing device for a shipboard aircraft of an aircraft carrier. The auxiliary landing device comprises intercept gates, a baffle, a hook and an elastic rope, wherein the intercept gates are made of metal, arranged in a fork-shaped manner, and fixed on the outer side of the edge of a deck; one end of each intercept gate, extending out of the outer side of the edge of the deck, tilts down; the baffle is made of plastic or rubber, and fixed on the external surface of a side plate of the aircraft carrier below the intercept gates; the hook is fixed at the tail end of the elastic rope; the width of the hook is greater than interval widths of the forked intercept gates; and the elastic rope is tied at the tail part of the shipboard aircraft. The auxiliary landing device is simple in structure; the elastic rope is put down when the shipboard aircraft approaches to the aircraft carrier in a using process, and the hook can be clamped below the intercept gates as long as the horizontal height of the hook is lower than those of the intercept gates, so that a purpose of reducing the speed of the shipboard aircraft is achieved by stretching and deformation of the elastic rope after the shipboard aircraft is landed on the carrier; the smoothness of the surface of the deck of the aircraft carrier is not destroyed; multiple shipboard aircrafts can land simultaneously; and the auxiliary landing device is suitable for all the aircraft carriers.
Description
Technical field the present invention relates to a kind of landing auxiliary device, especially the landing auxiliary device of the carrier-borne aircraft that uses at aircraft carrier.
Background technology and airfield are compared, and the airstrip length on the aircraft carrier shortens greatly.Carrier-borne aircraft when landing speed very fast and runway on the aircraft carrier deck is shorter, therefore need the landing of auxiliary ship carrier aircraft to slow down, reach the purpose of safe falling.At present, the main employing tackled rope auxiliary ship carrier aircraft landing deceleration on the aircraft carrier.The interception rope has not only influenced the profile pattern on aircraft carrier deck, and interception efficient is very low.After each interception, the interception rope all needs slowly to be returned to original position, delays a lot of times.
Chinese patent CN102530210A number disclosed " device is blocked in the aircraft carrier landing " patent (application number: 201110407296), comprise that at least three are blocked the device assembly, each blocks the device assembly and comprises two groups of dampers that are symmetricly set on aircraft landing runway both sides, damper comprises: fixed frame, damping cylinder, piston, pitch brace, movable pulley and fixed pulley group, wherein, the two ends of check cable are connected with damper, the check cable intermediate lateral is arranged in the middle of the landing runway, damper comprises fixed frame, tracheae, high pressure gas holder, several damping cylinders, be provided with piston in each damping cylinder, piston is connected with pitch brace, the external part of pitch brace is connected with movable pulley, one group of fixed pulley is connected with fixed frame, one end and the fixed frame of check cable are fixed, the other end of check cable and opposed damper fixed frame are fixed, and wear around between movable pulley and the fixed pulley centre of check cable.The weak point of this patent is: similar to prior art, not only influenced the profile pattern on aircraft carrier deck, and interception efficient is lower.
Chinese patent CN101348166 number disclosed " taking off and landing method and device thereof of aircraft carrier-based aircraft " patent (application number: 200810196042), comprise the windmill-shaped rotating mechanism that is arranged on the aircraft carrier warship body, be provided with one group of extension arm at rotating mechanism, the external part of extension arm is provided with landing platform and the launch pad of inclined angle-adjustable; Before taking off aircraft is fixed on the launch pad; Start rotating mechanism, reach when taking off height and speed at aircraft, the release anchor fitting flies out aircraft automatically along tangent line, finish taking off of aircraft; During landing, the landing platform floats on the sea, aircraft is during near the landing platform of rotating mechanism, flying height and the speed of launch pad inclination angle and aircraft are complementary, use arrester that aircraft is directly landed on the landing platform, progressively the slow down rotative speed of rotating mechanism until stopping, being finished the landing of aircraft; The present invention changes existing warship bodily form formula, can reduce warship body build, strengthens alerting ability, reduce use cost.The weak point of this patent is: the mobility of rotational structure self adds that the mobility of carrier-borne aircraft adds the mobility of aircraft carrier, makes the landing process be full of danger.
Summary of the invention purpose of the present invention is exactly that a kind of aircraft carrier simple in structure landing auxiliary device will be provided, and makes it simple and practical when slowing down for the carrier-borne aircraft landing.
In order to achieve the above object, aircraft carrier landing auxiliary device provided by the invention is made up of interception grid, baffle plate, hook and elastic rope, and wherein, the interception grid are by the metal manufacturing, and the interception grid are fork-shaped and arrange; The interception grid are fixed on the outside, edge, deck, and an end in the outside, interception grid sponson deck edge is downward-sloping; Baffle plate is by plastics or rubber manufacturing, and baffle plate is fixed on the aircraft carrier side plate outside face of interception grid below, the impulsive force when baffle plate can cushion the hook bump; Hook is fixed on the end of elastic rope; The width of hook is greater than the interval width of fork-shaped interception grid; Elastic rope ties up to the carrier-borne aircraft afterbody, and the manufactured materials of elastic rope is consistent with existing interception rope.In addition, hook and storage and the retractable operation of elastic rope on carrier-borne aircraft belong to general knowledge, repeat no more here.When the present invention used, carrier-borne aircraft put down elastic rope near aircraft carrier the time, as long as the level height of hook is lower than the interception grid, hook will be stuck in interception grid below, and after carrier-borne aircraft warship, elastic rope was reached for the purpose that carrier-borne aircraft slows down by stretching and distortion.
Aircraft carrier acceleration and deceleration device provided by the invention has positive effect: interception grid, baffle plate, hook and elastic rope are formed, and be simple in structure; Carrier-borne aircraft puts down elastic rope during use near aircraft carrier the time, as long as the level height of hook is lower than the interception grid, hook will be stuck in interception grid below, after carrier-borne aircraft warship, elastic rope is reached for the purpose that carrier-borne aircraft slows down by stretching and being out of shape, neither destroy the planarization of aircraft carrier deck surface, can realize that again many carrier-borne aircrafts land simultaneously, are applicable to all aircraft carriers.
Description of drawings the present invention will be further described by reference to the accompanying drawings, please referring to accompanying drawing:
Accompanying drawing 1 expression scheme drawing of the present invention.
Structure shown in the accompanying drawing 1 comprises: carrier-borne aircraft 1, elastic rope 2, interception grid 3, hook 4, baffle plate 5, aircraft carrier 6, deck 7.
Specific embodiment aircraft carrier landing provided by the invention auxiliary device is made up of interception grid 3, baffle plate 5, hook 4 and elastic rope 2, and wherein, interception grid 3 are by the metal manufacturing, and interception grid 3 are fork-shaped and arrange; Interception grid 3 are fixed on the outside, 7 edges, deck, and an end in the outside, interception grid 3 sponson decks, 7 edges is downward-sloping; Baffle plate 5 is by plastics or rubber manufacturing, and baffle plate 5 is fixed on the aircraft carrier 6 side plate outside faces of interception grid 3 belows, the impulsive force when baffle plate 5 can cushion hook 4 bumps; Hook 4 is fixed on the end of elastic rope 2; The width of hook 4 is greater than the interval width of fork-shaped interception grid 3; Elastic rope 2 ties up to carrier-borne aircraft 1 afterbody, and the manufactured materials of elastic rope 2 is consistent with existing interception rope.In addition, hook 4 and storage and the retractable operation of elastic rope 2 on carrier-borne aircraft belong to general knowledge, repeat no more here.When the present invention uses, carrier-borne aircraft 1 puts down elastic rope 2 near aircraft carrier 6 time, as long as the level height of hook 4 is lower than interception grid 3, hook 4 will be stuck in interception grid 3 belows, carrier-borne aircraft 1 behind the warship, elastic rope 2 is by stretching and distortion is reached for the purpose that carrier-borne aircraft 1 slows down.
Protection domain of the present invention relates to all changes form recited above.
Claims (1)
1. aircraft carrier landing auxiliary device, it is characterized in that: is made up of interception grid (3), baffle plate (5), hook (4) and elastic rope (2), wherein, interception grid (3) are tackled grid (3) and are the fork-shaped arrangement by the metal manufacturing; Interception grid (3) are fixed on the outside, edge, deck (7), and an end in the outside, interception grid (3) sponson decks (7) edge is downward-sloping; Baffle plate (5) is by plastics or rubber manufacturing, and baffle plate (5) is fixed on aircraft carrier (6) the side plate outside face of interception grid (3) below; Hook (4) is fixed on the end of elastic rope (2); The width of hook (4) is tackled the interval width of grid (3) greater than fork-shaped; Elastic rope (2) ties up to carrier-borne aircraft (1) afterbody.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201310145881 CN103204245A (en) | 2013-04-11 | 2013-04-11 | Auxiliary landing device for shipboard aircraft of aircraft carrier |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201310145881 CN103204245A (en) | 2013-04-11 | 2013-04-11 | Auxiliary landing device for shipboard aircraft of aircraft carrier |
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| Publication Number | Publication Date |
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| CN103204245A true CN103204245A (en) | 2013-07-17 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201310145881 Pending CN103204245A (en) | 2013-04-11 | 2013-04-11 | Auxiliary landing device for shipboard aircraft of aircraft carrier |
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| CN (1) | CN103204245A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103434648A (en) * | 2013-07-26 | 2013-12-11 | 严振华 | Device for guiding tail hook to hook arresting cable during landing of plane |
| CN106477065A (en) * | 2016-12-12 | 2017-03-08 | 大连理工大学 | Anti- formula carrier-borne aircraft of throwing blocks rope device |
| CN107323657A (en) * | 2017-08-24 | 2017-11-07 | 河南师范大学 | A kind of carrier-borne aircraft pintle device |
| CN107444667A (en) * | 2017-08-24 | 2017-12-08 | 河南师范大学 | A kind of carrier-borne aircraft landing system |
| CN109319100A (en) * | 2018-11-02 | 2019-02-12 | 中国航空工业集团公司西安飞机设计研究所 | A kind of ship-board aircraft buffer-type method for arresting and stop formation |
-
2013
- 2013-04-11 CN CN 201310145881 patent/CN103204245A/en active Pending
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103434648A (en) * | 2013-07-26 | 2013-12-11 | 严振华 | Device for guiding tail hook to hook arresting cable during landing of plane |
| CN106477065A (en) * | 2016-12-12 | 2017-03-08 | 大连理工大学 | Anti- formula carrier-borne aircraft of throwing blocks rope device |
| CN106477065B (en) * | 2016-12-12 | 2019-02-12 | 大连理工大学 | Anti- formula carrier-borne aircraft of throwing blocks rope device |
| CN107323657A (en) * | 2017-08-24 | 2017-11-07 | 河南师范大学 | A kind of carrier-borne aircraft pintle device |
| CN107444667A (en) * | 2017-08-24 | 2017-12-08 | 河南师范大学 | A kind of carrier-borne aircraft landing system |
| CN109319100A (en) * | 2018-11-02 | 2019-02-12 | 中国航空工业集团公司西安飞机设计研究所 | A kind of ship-board aircraft buffer-type method for arresting and stop formation |
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| PB01 | Publication | ||
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| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20130717 |