CN103129743A - Warship landing stopping device - Google Patents
Warship landing stopping device Download PDFInfo
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- CN103129743A CN103129743A CN2011103810115A CN201110381011A CN103129743A CN 103129743 A CN103129743 A CN 103129743A CN 2011103810115 A CN2011103810115 A CN 2011103810115A CN 201110381011 A CN201110381011 A CN 201110381011A CN 103129743 A CN103129743 A CN 103129743A
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- cylinder
- pipe
- damper tube
- warship
- gas return
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Abstract
A warship landing stopping device is mainly composed of a left sliding block 1, a right sliding block 2, a left damping pipe cylinder 5, a right damping pipe cylinder 6, a sliding air return pipe 7, a sliding air return pipe regulating valve 10 and the like. Two ends of a stopping cable 15 are respectively connected with a left rope winding device 3 inside the left sliding block 1 and a right rope winding device 4 inside the right sliding block 2. After an airplane is landed on a warship, the stopping cable 15 is hooked by a tail hook to push the left sliding block 1 and the right sliding block 2 to respectively obtain gradually-increased and changed resistance in the left damping pipe cylinder 5 and the right damping pipe cylinder 6 to slide forwards, the airplane is decelerated and stopped, therefore purposes of simplicity, convenience and practicality are achieved, factors restricting aircraft carrier and airport design manufacture are reduced, and more functions of a naval vessel and an airport are explored.
Description
Technical field
The present invention relates to a kind of warship arresting gear, be a kind of be mainly used in aircraft landing warship arresting gear scheme, be mainly the coasting distance when reducing the aircraft landing, be applicable on the airstrip on aircraft carrier, airport, application is set.
Background technology
At present, also do not have this pattern the warship arresting gear, along with reinforcement and the Sovereignty of Territorial Sea of the international defence responsibilities of China are nibbled gradually, it is one of main problem of building by aircraft carrier that the security situation that on naval vessels, flight is risen and fallen more and more becomes problem, the particularly aircraft safe falling on naval vessels.In view of this situation is necessary to invent a kind of applicable, advanced warship arresting gear, is used for being arranged on the airstrip on aircraft carrier, airport, thereby can reduces the factor that Restriction Design is made aircraft carrier, airport, the more flexible function of excavating out naval vessels, airport.
Summary of the invention
The objective of the invention is to provide a kind of warship arresting gear, be a kind of be mainly used in aircraft landing warship arresting gear scheme, it is mainly the coasting distance when reducing the aircraft landing, be used for being arranged on the airstrip on aircraft carrier, airport, thereby energy is simple and practical, the minimizing Restriction Design is made the factor on aircraft carrier, airport, excavate out the greater functionality on naval vessels, airport, this device scheme is also this base model of warship arresting gear.
the objective of the invention is to complete as follows: when landing due to carrier-borne aircraft, speed is larger, the flight deck length of aircraft carrier can not satisfy the coasting distance requirement of aircraft landing fully, therefore, must assist its landing by the resistance that the warship arresting gear produces, basic mode is mainly when aircraft warship, prop check cable 15 to the height that is fit to by the device that arches on check cable guide piece 16, check cable 15 two ends be respectively with left slider 1, left rope winder 3 in right slide block 2, right rope winder 4 is connected respectively, be provided with pintle with reference to its afterbody of U.S.'s aircraft carrier, when preparing warship, aircraft puts down pintle, after aircraft warship, pintle tangles check cable 15, drive check cable 15 and drag left slider 1, right slide block 2 obtains the pneumatics resistance that increases gradually and/or change respectively simultaneously and aircraft is slowed down and stop to front slide in left damper tube cylinder 5 and right damper tube cylinder 6.the ante-chamber of left damper tube cylinder 5 and right damper tube cylinder 6 is connected to left damper tube cylinder 5 and right damper tube cylinder 6 back cavities by sliding gas return pipe 7, on sliding gas return pipe 7, sliding gas return pipe control cock 10 is arranged, before the ante-chamber difference connection pipe cylinder of left damper tube cylinder 5 and right damper tube cylinder 6,, there is the front control cock 12 of pipe cylinder at adjustable pipe 9 two ends on adjustable pipe 9 before the pipe cylinder, the back cavity of left damper tube cylinder 5 and right damper tube cylinder 6 is adjustable pipe 8 two ends after the connection pipe cylinder respectively, and control cock 13 after the pipe cylinder is arranged on adjustable pipe 8 after the pipe cylinder, left slider 1, right slide block 2 compensates to left damper tube cylinder 5 at the air-flow of left damper tube cylinder 5 and the 6 slip discharges of right damper tube cylinder by sliding gas return pipe 7 respectively simultaneously, right damper tube cylinder 6 back cavities or discharge by side valve 11 before sliding gas return pipe, sliding gas return pipe control cock 10, side valve 11 before sliding gas return pipe, after sliding gas return pipe, side valve 14 can be regulated the resistance that blocks of controlling aircraft slip needs by the mode that air-flow is controlled in adjustings, managing in case of necessity after the front control cock of cylinder 12 pipe cylinders after control cock 13 and the sliding gas return pipe of front the side valve 11 of sliding gas return pipe the side valve 14 outside devices that arrange in addition of associating calms the anger or bleeds and coordinate the above-mentioned effect of apparatus of the present invention work reinforcement, can obtain more preferably and block, after aircraft is blocked shutdown, pintle and check cable 15 take off hook.After check cable 15 takes off and hooks, after the front control cock 12 of pipe cylinder and pipe cylinder, control cock 13 is started working and is driven left slider 1, right slide block 2 affects and returns to check cable 15, simultaneously can interior elasticity or electronic left rope winder 3 be set at the right slide block 2 of left slider 1, some check cables 15 of right rope winder 4 wraparounds are returned to the home position, prepare to receive to block next airplane landing.
The present invention is to provide a kind of warship arresting gear, due to be adopt check cable 15 two ends respectively with left slider 1, right slide block 2 in left rope winder 3, right rope winder 4 be connected respectively, after aircraft warship, pintle tangles check cable 15, driving check cable 15 drags left slider 1, right slide block 2 and obtains the resistance that increases gradually and change simultaneously in left damper tube cylinder 5 and right damper tube cylinder 6 respectively and aircraft is slowed down and stop to front slide, thereby energy is simple and practical, the minimizing Restriction Design is made the factor on aircraft carrier, airport, excavates out the greater functionality on naval vessels, airport.
Description of drawings: Fig. 1 is a kind of principle schematic of the present invention, and the present invention mainly contains the compositions such as control cock 13 after control cock 12 before side valve 14 after side valve 11 before adjustable pipe 9 before adjustable pipe 8 after left slider 1, right slide block 2, left rope winder 3, right rope winder 4, left damper tube cylinder 5, right damper tube cylinder 6, sliding gas return pipe 7, pipe cylinder, pipe cylinder, sliding gas return pipe control cock 10, sliding gas return pipe, sliding gas return pipe, pipe cylinder, pipe cylinder, check cable 15, check cable guide piece 16 with reference to Fig. 1.
the specific embodiment: when aircraft warship, prop check cable 15 to the height that is fit to by the device that arches on check cable guide piece 16, check cable 15 two ends respectively with left slider 1, left rope winder 3 in right slide block 2, right rope winder 4 is connected respectively, be provided with pintle with reference to its afterbody of U.S.'s aircraft carrier, close in airplane tail after taking off, put down pintle when preparing warship, after aircraft warship, pintle tangles check cable 15, drive check cable 15 and drag left slider 1, right slide block 2 obtains the air pressure resistance that increases gradually and/or change respectively simultaneously in left damper tube cylinder 5 and right damper tube cylinder 6 makes rapidly aircraft slow down and stop.left slider 1, right slide block 2 compensates to left damper tube cylinder 5 at the ante-chamber air-flow of left damper tube cylinder 5 and the 6 slip discharges of right damper tube cylinder by sliding gas return pipe 7 respectively simultaneously, right damper tube cylinder 6 back cavities or discharge by side valve 11 before sliding gas return pipe, sliding gas return pipe control cock 10, side valve 11 before sliding gas return pipe, after sliding gas return pipe, side valve 14 regulates by controlling streamer mode the power of blocking that aircraft slides to be needed of controlling, manage in case of necessity after the front control cock of cylinder 12 pipe cylinders side valve after control cock 13 and the sliding gas return pipe of front the side valve 11 of sliding gas return pipe 14 associating outsides supporting calm the anger or the air extractor cooperating obtains ideal and blocks state, after aircraft is blocked shutdown, pintle and check cable 15 take off hook, after check cable 15 takes off the front control cock 12 of the rear pipe of hook cylinder and manages cylinder, control cock 13 is worked and is driven left sliders 1, right slide block 2 affects back check cable 15, simultaneously can be at interior elasticity or the electronic left rope winder 3 of arranging of the right slide block 2 of left slider 1, right some check cables 15 of rope winder 4 wraparounds are returned to original position, prepare reception and block next airplane landing.Check cable 15 is propped from the part of runway floor level less than the aircraft tyre diameter, and in the time of aircraft landing, the wheel tire pressure is crossed check cable 15 and also increased and block effect.Left slider 1, right slide block 2 can be ellipsoid shape, column etc., it is combined into ellipsoid shape, column etc. after can split manufacturing and designing, left rope winder 3, right rope winder 4 in it is generally that the cylinder sampling device mainly rises fixing or/and around check cable 15, can adopt in the cylinder sampling device clock and watch shape Spring driving around check cable 15 or also electronic or other modes around check cable 15 or only the fixing rope winder that do not arrange all determine as required.Check cable guide piece 16 is arranged on check cable 15 two ends and does not relate to apparatus of the present invention itself, and its device mode, mode of operation require to determine according to himself.Other parts of apparatus of the present invention arrange not circumscribed as required.
Apparatus of the present invention can also coordinate the flight landing retardance runway that the inventor invents to be used in conjunction with, take full advantage of terrestrial gravitation to the aircraft landing deceleration/decel or come to taking off acceleration/accel, if utilizing the warship arresting gear to take off for the aircraft power-assisted, the direction of taking off of aircraft should be landed with flight, and each runway tape running direction of retardance runway is consistent, speed can increase gradually, in order to accelerate the takeoff speed of aircraft.
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Claims (4)
- one kind the warship arresting gear, mainly contain left slider (1), right slide block (2), left rope winder (3), right rope winder (4), left damper tube cylinder (5), right damper tube cylinder (6), sliding gas return pipe (7), adjustable pipe (8) after the pipe cylinder, adjustable pipe (9) before the pipe cylinder, sliding gas return pipe control cock (10), side valve (11) before sliding gas return pipe, side valve (14) after sliding gas return pipe, control cock (12) before the pipe cylinder, control cock (13) after the pipe cylinder, check cable (15), the compositions such as check cable guide piece (16), it is characterized in that: check cable (15) two ends respectively with left slider (1), left rope winder (3) in right slide block (2), right rope winder (4) is connected respectively.
- 2. warship arresting gear according to claim 1, it is characterized in that: the ante-chamber of left damper tube cylinder (5) and right damper tube cylinder (6) is connected to left damper tube cylinder (5) and right damper tube cylinder (6) back cavity by sliding gas return pipe (7), on sliding gas return pipe (7), sliding gas return pipe control cock (10) is arranged.
- 3. warship arresting gear according to claim 2 is characterized in that: the ante-chamber of left damper tube cylinder (5) and right damper tube cylinder (6) is adjustable pipe (9) two ends before the connection pipe cylinder respectively, and control cock (12) before the pipe cylinder is arranged on adjustable pipe (9) before the pipe cylinder.
- 4. warship arresting gear according to claim 2 is characterized in that: the back cavity of left damper tube cylinder (5) and right damper tube cylinder (6) is adjustable pipe (8) two ends after the connection pipe cylinder respectively, and control cock (13) after the pipe cylinder is arranged on adjustable pipe (8) after the pipe cylinder.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201110381011.5A CN103129743B (en) | 2011-11-25 | 2011-11-25 | Warship arresting gear |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201110381011.5A CN103129743B (en) | 2011-11-25 | 2011-11-25 | Warship arresting gear |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103129743A true CN103129743A (en) | 2013-06-05 |
| CN103129743B CN103129743B (en) | 2016-08-03 |
Family
ID=48490307
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201110381011.5A Expired - Fee Related CN103129743B (en) | 2011-11-25 | 2011-11-25 | Warship arresting gear |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103129743B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107226215A (en) * | 2017-05-22 | 2017-10-03 | 成都飞机工业（集团）有限责任公司 | The rotary cross bar of unmanned plane blocks recovery system and recovery method |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB886274A (en) * | 1957-05-23 | 1962-01-03 | Acme Prec Products Inc | Vehicle decelerating apparatus |
| CN1032645A (en) * | 1988-10-18 | 1989-05-03 | 黄泽荣 | Stol device for ultralight aircraft |
| CN1146414A (en) * | 1994-09-05 | 1997-04-02 | 朱炎 | Airplane catapult and recovery system |
| CN201856898U (en) * | 2010-09-10 | 2011-06-08 | 上海市南洋模范中学 | Buffer tripping cable |
| CN202429358U (en) * | 2011-11-25 | 2012-09-12 | 孙善骏 | Device for stopping landing aircraft |
-
2011
- 2011-11-25 CN CN201110381011.5A patent/CN103129743B/en not_active Expired - Fee Related
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB886274A (en) * | 1957-05-23 | 1962-01-03 | Acme Prec Products Inc | Vehicle decelerating apparatus |
| CN1032645A (en) * | 1988-10-18 | 1989-05-03 | 黄泽荣 | Stol device for ultralight aircraft |
| CN1146414A (en) * | 1994-09-05 | 1997-04-02 | 朱炎 | Airplane catapult and recovery system |
| CN201856898U (en) * | 2010-09-10 | 2011-06-08 | 上海市南洋模范中学 | Buffer tripping cable |
| CN202429358U (en) * | 2011-11-25 | 2012-09-12 | 孙善骏 | Device for stopping landing aircraft |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107226215A (en) * | 2017-05-22 | 2017-10-03 | 成都飞机工业（集团）有限责任公司 | The rotary cross bar of unmanned plane blocks recovery system and recovery method |
| CN107226215B (en) * | 2017-05-22 | 2023-08-04 | 成都飞机工业（集团）有限责任公司 | Unmanned aerial vehicle rotary cross bar arresting recovery system and recovery method |
Also Published As
| Publication number | Publication date |
|---|---|
| CN103129743B (en) | 2016-08-03 |
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Granted publication date: 20160803 Termination date: 20181125 |