CN103646602B - Simulated ship-bone aircraft take-off and landing training platform - Google Patents
Simulated ship-bone aircraft take-off and landing training platform Download PDFInfo
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- CN103646602B CN103646602B CN201310655794.0A CN201310655794A CN103646602B CN 103646602 B CN103646602 B CN 103646602B CN 201310655794 A CN201310655794 A CN 201310655794A CN 103646602 B CN103646602 B CN 103646602B
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Abstract
Disclosed in the invention is a simulated ship-bone aircraft take-off and landing training platform. Key points of the technical scheme are as follows: the simulated training platform comprises a main simulated platform body, a take-off protection platform and a commanding tower; the main simulated platform body is mainly responsible for simulating a navigation state of an aircraft carrier in the sea; the take-off protection platform is responsible for protecting an aircraft to enable the aircraft to glide continuously at the take-off protection platform for emergency under the circumstances that the aircraft fails to take off without lifting off; and the commanding tower is used for operating and controlling the state parameter of the simulated platform as well as aircraft take-off and landing information commanding. According to the invention, a plurality of high-power motors are used for driving a driving device and thus the flight deck is driven to make forth-and-back, left-and-right, and up-and-down oscillation; and a track is laid and thus the simulated platform can moves forward on land at the set speed, so that the relatively actual navigation state of the aircraft carrier in the sea can be simulated. And a good testing condition is provided for take-off and landing of the ship-bone aircraft.
Description
Technical field
The present invention relates to a kind of carrier-borne aircraft landing analog training device, be specifically related to a kind of carrier-borne aircraft landing simulative training platform.
Background technology
The development of aircraft carrier is more and more taken seriously in China, and it can increase defense force greatly, especially coast defence construction.Why severe aircraft carrier is, is because it can carry airplane carrier fighter, bomber, forms fighting capacity.But carrier-borne aircraft landing easy thing absolutely not on aircraft carrier, be the important ring in aircraft carrier technology.China's carrier-borne aircraft technology is started late, though master a skill at present, but battlefield surroundings is complicated, opportunity of combat landing affects by multiple factors, so need pilot constantly to train, skillfully to grasp the landing technology of carrier-borne aircraft, but at present carrier-borne aircraft landing training can only be carried out on the unique aircraft carrier " Liaoning " of China number.If the carrier-borne aircraft landing platform of a simulation can be built, more landing training can be carried out simultaneously, accelerate the full-fledged of China's aircraft carrier technology.
Summary of the invention
The technical matters that the present invention solves there is provided a kind of carrier-borne aircraft landing simulative training platform, and be exclusively used in simulation aircraft carrier at operational configuration marine greatly, the landing for carrier-borne aircraft provides simulated training environment.As everyone knows, carrier-borne aircraft is on aircraft carrier during landing, aircraft carrier is not static, but under sail, and aircraft carrier is jiggly in navigation marine greatly, by the impact of wave sea wind, it must be move ahead in slight left-right and front-back waves, therefore to board a plane many than airport, ground complicated condition of landing condition at aircraft carrier, this is the major reason causing carrier-borne aircraft landing difficulty large.
Technical scheme of the present invention is: a kind of carrier-borne aircraft landing simulative training platform, it is characterized in that primarily of analog platform main body, take off protecting platform and conning-tower formation, described analog platform main body is connected with the protecting platform that takes off by coupling assembling, iron tyre is equipped with in analog platform main body and the bottom of the protecting platform that takes off, electric motor is equipped with in the inside of this iron tyre, be arranged on same rail by iron tyre by analog platform main body and the protecting platform that takes off, described conning-tower is arranged in analog platform main body;
Described analog platform main body is followed successively by flight-deck from top to bottom, ground floor parametric controller and second layer parametric controller, ground floor parametric controller is primarily of middle deck and the actuating unit that is arranged between flight-deck and middle deck, supporting mechanism and support spring composition, the parallel longitudinal both sides being arranged at middle deck of described actuating unit, comprise motor, motor supporting table, first drive link, second drive link, drive link rotating shaft and link, wherein motor supporting table is fixed on middle deck, motor on middle deck is installed on motor supporting table, the rotor of motor connects the first drive link, first drive link connects the second drive link by drive link rotating shaft, second drive link is connected with flight-deck by link, electric machine rotation just can be driven before and after flight-deck by drive link and swing up and down, supporting mechanism on middle deck is longitudinally arranged at the middle part of middle deck, comprise platform rotating shaft, rotating shaft link, heavy bearing and pillar, wherein platform rotating shaft is installed on the positive middle part of flight-deck, flight-deck is connected by rotating shaft link, platform rotating shaft is provided with heavy bearing, heavy bearing connects support by pillar, this pillar is installed on middle deck, for supporting flight-deck, support spring on middle deck is arranged between actuating unit and supporting mechanism, one end of this support spring is connected to flight-deck, the other end is connected to middle deck, the elasticity coefficient of support spring is 2000-3000N/m,
Described second layer parametric controller is primarily of deck of cellar and the actuating unit that is arranged between middle deck and deck of cellar, supporting mechanism and support spring composition, wherein actuating unit is laterally set in parallel in the both sides of deck of cellar, comprise motor, motor supporting table, first drive link, second drive link, drive link rotating shaft and link, wherein motor supporting table is fixed on deck of cellar, motor on deck of cellar is installed on motor supporting table, the rotor of motor connects the first drive link, first drive link connects the second drive link by drive link rotating shaft, second drive link is connected with middle deck by link, electric machine rotation swings up and down about just can driving middle deck by drive link, supporting mechanism on deck of cellar is horizontally set at the middle part of deck of cellar, comprise platform rotating shaft, rotating shaft link, heavy bearing and pillar, wherein platform rotating shaft is installed on the positive middle part of middle deck, middle deck is connected by rotating shaft link, platform rotating shaft is provided with heavy bearing, heavy bearing connects support by pillar, pillar is installed on deck of cellar, for supporting middle deck, support spring on deck of cellar is arranged between actuating unit and supporting mechanism, one end of this support spring is connected to middle deck, the other end is connected to deck of cellar, the elasticity coefficient of support spring is 2000-3000N/m,
Be provided with gap between the flight-deck of described take off protecting platform and analog platform main body, be equipped with runway taking off on protecting platform, and at the middle part of the protecting platform that takes off, 2-3 road check cable be installed.
The present invention utilizes multiple stage heavy-duty motor to drive gearing, flight-deck is driven to swing up and down all around, and lay rail enable simulative training platform according to setting speed move ahead on land, true simulation aircraft carrier is at operational configuration marine greatly, landing for carrier-borne aircraft provides good test condition, the present invention has following beneficial effect: 1, simulate aircraft carrier platform advantage of lower cost, easily manufacture; 2, the present invention just can launch carrier-borne aircraft landing training in terrestrial environment, can accelerate to carry out China carrier-borne aircraft pilot landing training mission; 3, simulative training platform of the present invention is with the protecting platform that takes off, and can reduce accident rate, protection pilot and aircraft safety.
Accompanying drawing explanation
Fig. 1 is structural representation of the present invention, and Fig. 2 is the structural representation of ground floor parametric controller of the present invention, and Fig. 3 is the structural representation of second layer parametric controller of the present invention.
Drawing illustrates: 1, analog platform main body, 2, take off protecting platform, 3, conning-tower, 4, coupling assembling; 5, motor, 6, motor supporting table, the 7, first drive link, the 8, second drive link; 9, drive link rotating shaft, 10, link, 11, platform rotating shaft, 12, rotating shaft link; 13, heavy bearing, 14, pillar, 15, support spring, 16, deck of cellar; 17, middle deck, 18, flight-deck, 19, runway; 20, check cable, 21, rail, 22, iron tyre.
Embodiment
Describe embodiment in detail by reference to the accompanying drawings.A kind of carrier-borne aircraft landing simulative training platform; comprise analog platform main body 1; take off protecting platform 2 and conning-tower 3; wherein analog platform main body 1 is mainly used in simulation aircraft carrier at operational configuration marine greatly; take off protecting platform 2 for the protection of aircraft when failure of taking off is not gone up to the air; promptly continue to slide taking off on protecting platform 2, conning-tower 3 is for operating state parameter and the takeoff and landing information commander of control simulation platform.Analog platform main body 1 is connected with the protecting platform 2 that takes off by coupling assembling 4, conning-tower 3 is seated in analog platform main body 1, described analog platform main body 1 is followed successively by flight-deck from top to bottom, ground floor parametric controller and second layer parametric controller, wherein ground floor parametric controller can fluctuate front and back, primarily of middle deck 17 and the actuating unit that is arranged between flight-deck 18 and middle deck 17, supporting mechanism and support spring 15 are formed, second layer parametric controller can fluctuate left and right, primarily of deck of cellar 16 and the actuating unit that is arranged between middle deck 17 and deck of cellar 16, supporting mechanism and support spring 15 are formed, described actuating unit comprises motor 5, motor supporting table 6, first drive link 7, second drive link 8, drive link rotating shaft 9 and link 10, described supporting mechanism comprises platform rotating shaft 11, rotating shaft link 12, heavy bearing 13 and pillar 14, protecting platform 2 top of taking off is provided with runway 19 and check cable 20, conning-tower 3 is seated the side of flight-deck 18, described analog platform main body 1 and the bottom of the protecting platform 2 that takes off all are provided with iron tyre 22, inside is equipped with electric motor and is driven iron tyre 22, the overall rail 21 laid by ground supports, can move ahead on rail 21 or fall back.
In the actuating unit of ground floor parametric controller, motor supporting table 6 is installed on middle deck 17, motor 5 is some, power is 5-10kw, the parallel longitudinal both sides being arranged in middle deck 17, one is placed every 5-7 rice, be arranged on motor supporting table 6, the rotor of motor 5 connects the first drive link 7, the second drive link 8 is connected by drive link rotating shaft 9, second drive link 8 is connected with flight-deck 18 by link 10, motor 5 rotates through drive link and just can drive before and after flight-deck 18 and swing up and down, motor 5 rotating speed is controlled, for 20-40 per minute turns, the platform rotating shaft 11 of described supporting mechanism is installed on the positive middle part of flight-deck 18, flight-deck 18 is connected by rotating shaft link 12, platform rotating shaft 11 is provided with several heavy bearings 13, heavy bearing 13 connects support by pillar 14, pillar 14 is arranged on middle deck 17, for supporting flight-deck 18, belong to Hard link, middle deck 17 is also provided with some support springs 15, connection middle deck, one end 17, one end connects flight-deck 18, side by side parallel is installed, play the effect of supplemental support, the elasticity coefficient of support spring 15 is 2000-3000N/m, height is identical with parametric controller height, when motor 5 rotates, flight-deck 18 just can swing up and down around before and after platform rotating shaft 11.
In the actuating unit of second layer parametric controller, motor supporting table 6 is installed on deck of cellar 17, motor 5 is some, power is 5-10kw, laterally be parallel to the both sides of deck of cellar 16, one is placed every 5-7 rice, be arranged on motor supporting table 6, the rotor of motor 5 connects the first drive link 7, the second drive link 8 is connected by drive link rotating shaft 9, second drive link 8 is connected with middle deck 17 by link 10, motor 5 rotates through drive link and middle deck about 17 just can be driven to swing up and down, motor 5 rotating speed is controlled, for 20-40 per minute turns, the platform rotating shaft 11 of described supporting mechanism is arranged on positive middle part, middle deck 17, middle deck 17 is connected by rotating shaft link 12, platform rotating shaft 11 is provided with several heavy bearings 13, heavy bearing 13 connects support by pillar 14, pillar 14 is arranged on deck of cellar 16, for supporting middle deck 17, belong to Hard link, deck of cellar 16 is also provided with some support springs 15, connection deck of cellar, one end 16, connection middle deck, one end 17, side by side parallel is installed, play the effect of supplemental support, the elasticity coefficient of support spring 15 is 2000-3000N/m, height is identical with parametric controller height, when motor 5 rotates, middle deck 17 just can swing up and down around platform rotating shaft about 11.
Ground floor parametric controller is identical with second layer parametric controller principle of work, and use parts also identical, two-layer parametric controller height is identical, is between 4-6m, and just swaying direction changes.
The described protecting platform 2 that takes off is separate with analog platform main body 1 top; certain interval is left in centre; bottom is connected by coupling assembling 4; realize synchronizing moving or stopping; keep relative distance constant; be equipped with runway 19 taking off on protecting platform 2; and at the middle part of the protecting platform 2 that takes off, 2-3 road check cable 20 is installed; protection aircraft is not when failure of taking off is gone up to the air; can continue to slide taking off on protecting platform 2; stop aircraft by check cable 22, protection pilot and aircraft safety, improve safety coefficient.
Whole carrier-borne aircraft landing simulative training platform is supported by the iron tyre 22 be installed on below analog platform main body 1 deck of cellar 16 and the protecting platform 2 that takes off; the electric motor driving iron tyre 22 is equipped with in inside; iron tyre 22 is driven to move ahead by setting speed on the rail 21 laid or fall back; rail 21 amounts to 2-3 road, and length is 2000-3000m.
Claims (1)
1. a carrier-borne aircraft landing simulative training platform, it is characterized in that primarily of analog platform main body, take off protecting platform and conning-tower formation, described analog platform main body is connected with the protecting platform that takes off by coupling assembling, iron tyre is equipped with in analog platform main body and the bottom of the protecting platform that takes off, electric motor is equipped with in the inside of this iron tyre, be arranged on same rail by iron tyre by analog platform main body and the protecting platform that takes off, described conning-tower is arranged in analog platform main body;
Described analog platform main body is followed successively by flight-deck from top to bottom, ground floor parametric controller and second layer parametric controller, ground floor parametric controller is primarily of middle deck and the actuating unit that is arranged between flight-deck and middle deck, supporting mechanism and support spring composition, the parallel longitudinal both sides being arranged at middle deck of described actuating unit, comprise motor, motor supporting table, first drive link, second drive link, drive link rotating shaft and link, wherein motor supporting table is fixed on middle deck, motor on middle deck is installed on motor supporting table, the rotor of motor connects the first drive link, first drive link connects the second drive link by drive link rotating shaft, second drive link is connected with flight-deck by link, electric machine rotation just can be driven before and after flight-deck by drive link and swing up and down, supporting mechanism on middle deck is longitudinally arranged at the middle part of middle deck, comprise platform rotating shaft, rotating shaft link, heavy bearing and pillar, wherein platform rotating shaft is installed on the positive middle part of flight-deck, flight-deck is connected by rotating shaft link, platform rotating shaft is provided with heavy bearing, heavy bearing connects support by pillar, this pillar is installed on middle deck, for supporting flight-deck, support spring on middle deck is arranged between actuating unit and supporting mechanism, one end of this support spring is connected to flight-deck, the other end is connected to middle deck, the elasticity coefficient of support spring is 2000-3000N/m,
Described second layer parametric controller is primarily of deck of cellar and the actuating unit that is arranged between middle deck and deck of cellar, supporting mechanism and support spring composition, wherein actuating unit is laterally set in parallel in the both sides of deck of cellar, comprise motor, motor supporting table, first drive link, second drive link, drive link rotating shaft and link, wherein motor supporting table is fixed on deck of cellar, motor on deck of cellar is installed on motor supporting table, the rotor of motor connects the first drive link, first drive link connects the second drive link by drive link rotating shaft, second drive link is connected with middle deck by link, electric machine rotation swings up and down about just can driving middle deck by drive link, supporting mechanism on deck of cellar is horizontally set at the middle part of deck of cellar, comprise platform rotating shaft, rotating shaft link, heavy bearing and pillar, wherein platform rotating shaft is installed on the positive middle part of middle deck, middle deck is connected by rotating shaft link, platform rotating shaft is provided with heavy bearing, heavy bearing connects support by pillar, pillar is installed on deck of cellar, for supporting middle deck, support spring on deck of cellar is arranged between actuating unit and supporting mechanism, one end of this support spring is connected to middle deck, the other end is connected to deck of cellar, the elasticity coefficient of support spring is 2000-3000N/m,
Be provided with gap between the flight-deck of described take off protecting platform and analog platform main body, be equipped with runway taking off on protecting platform, and at the middle part of the protecting platform that takes off, 2-3 road check cable be installed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310655794.0A CN103646602B (en) | 2013-12-09 | 2013-12-09 | Simulated ship-bone aircraft take-off and landing training platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310655794.0A CN103646602B (en) | 2013-12-09 | 2013-12-09 | Simulated ship-bone aircraft take-off and landing training platform |
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| Publication Number | Publication Date |
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| CN103646602A CN103646602A (en) | 2014-03-19 |
| CN103646602B true CN103646602B (en) | 2015-07-01 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201310655794.0A Expired - Fee Related CN103646602B (en) | 2013-12-09 | 2013-12-09 | Simulated ship-bone aircraft take-off and landing training platform |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN112435531B (en) * | 2020-10-29 | 2021-11-16 | 燕山大学 | Traction simulation platform for ship-based helicopter |
| CN114582196A (en) * | 2022-03-17 | 2022-06-03 | 孟竹 | Training device suitable for take-off and landing of carrier-based aircraft |
| CN115457833B (en) * | 2022-09-15 | 2024-04-19 | 吉林大学 | Traction robot track control experiment table of offshore operation helicopter |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN2365133Y (en) * | 1999-01-15 | 2000-02-23 | 胡瑞生 | Aircraft trouble landing rescue tender |
| CN1629040A (en) * | 2003-12-19 | 2005-06-22 | 上海凡纳加服饰有限公司 | Airplane forced landing device |
| CN100395160C (en) * | 2004-12-02 | 2008-06-18 | 陈琪 | Movable runway for plane landing |
| CN101830288B (en) * | 2009-03-09 | 2014-01-08 | 滕世进 | Synchronously following type aircraft forced landing platform |
| KR101241531B1 (en) * | 2010-07-27 | 2013-03-08 | (주)트윈테크 | Simulator with 4 dof |
| CN201980380U (en) * | 2010-12-13 | 2011-09-21 | 天津工程机械研究院 | Swinging ascending and sinking simulation test device for ships and warships |
| CN103043220B (en) * | 2011-10-13 | 2015-07-01 | 王力丰 | Taking-off and landing system of shipboard aircraft of aircraft carrier and taking-off and landing method thereof |
| CN103050047B (en) * | 2012-12-11 | 2014-12-24 | 燕山大学 | Self-balanced parallel movement simulator of two-freedom degree closed loop |
| CN103050046B (en) * | 2012-12-11 | 2015-04-08 | 燕山大学 | Parallel motion simulation platform with load-bearing mechanism |
| CN103426356B (en) * | 2013-07-16 | 2015-09-16 | 燕山大学 | A kind of coupled mode four-degree-of-freedom motion simulation platform |
| CN203616935U (en) * | 2013-12-09 | 2014-05-28 | 河南师范大学 | Shipboard aircraft taking-off and landing simulation training platform |
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