CN103646602A - 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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- CN103646602A CN103646602A CN201310655794.0A CN201310655794A CN103646602A CN 103646602 A CN103646602 A CN 103646602A CN 201310655794 A CN201310655794 A CN 201310655794A CN 103646602 A CN103646602 A CN 103646602A
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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, especially coast defence construction greatly.Why severe aircraft carrier is, is because it can carry airplane carrier fighter, bomber, forms fighting capacity.Yet carrier-borne aircraft is a landing easy thing absolutely not on aircraft carrier, is 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 is affected by multiple factors, so need pilot constantly to train, skillfully to grasp the landing technology of carrier-borne aircraft, yet at present carrier-borne aircraft landing training can only be carried out on the unique aircraft carrier of China " Liaoning " number.If can build the carrier-borne aircraft landing platform of a simulation, can carry out more landing training simultaneously, accelerate the full-fledged of China's aircraft carrier technology.
Summary of the invention
The technical matters that the present invention solves has been to provide a kind of carrier-borne aircraft landing simulative training platform, is exclusively used in simulation aircraft carrier at large marine operational configuration, for the landing of 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 large marine navigation, is subject to the impact of wave sea wind, and it must be to move ahead in slight left-right and front-back waves, therefore aircraft carrier many than airport, ground complicated condition of landing condition that board a plane, this is a major reason that causes 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 mainly being formed by analog platform main body, take off protecting platform and conning-tower, described analog platform main body is connected with the protecting platform that takes off by coupling assembling, in analog platform main body and the bottom of the protecting platform that takes off, be equipped with iron tyre, electric motor is equipped with in the inside of this iron tyre, by iron tyre, analog platform main body and the protecting platform that takes off are arranged on same rail, 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 controls platform and the second layer is controlled platform, ground floor control platform mainly by middle deck and be arranged at flight-deck and middle deck between actuating unit, supporting mechanism and support spring form, described actuating unit parallel longitudinal is arranged at the both sides of middle deck, comprise motor, motor supporting table, the first drive link, the second drive link, drive link rotating shaft and link, wherein motor supporting table is fixed on middle deck, described motor is installed on motor supporting table, the rotor of motor connects the first drive link, the first drive link connects the second drive link by drive link rotating shaft, the second drive link is connected with flight-deck by link, electric machine rotation swings up and down before and after just can driving flight-deck by drive link, described supporting mechanism 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, by rotating shaft link, connect flight-deck, in platform rotating shaft, heavy bearing is installed, heavy bearing is connected and is supported by pillar, this pillar is installed on middle deck, be used for supporting flight-deck, described support spring is arranged between actuating unit and supporting mechanism, one end of this support spring is connected in flight-deck, the other end is connected in middle deck, the elasticity coefficient of support spring is 2000-3000N/m,
The described second layer control platform mainly by deck of cellar and be arranged at middle deck and deck of cellar between actuating unit, supporting mechanism and support spring form, wherein actuating unit is laterally set in parallel in the both sides of deck of cellar, comprise motor, motor supporting table, the first drive link, the second drive link, drive link rotating shaft and link, wherein motor supporting table is fixed on deck of cellar, described motor is installed on motor supporting table, the rotor of motor connects the first drive link, the first drive link connects the second drive link by drive link rotating shaft, the second drive link is connected with middle deck by link, electric machine rotation just can drive left and right, middle deck to swing up and down by drive link, described supporting mechanism 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, by rotating shaft link, connect middle deck, in platform rotating shaft, heavy bearing is installed, heavy bearing is connected and is supported by pillar, pillar is installed on deck of cellar, be used for supporting middle deck, described support spring is arranged between actuating unit and supporting mechanism, one end of this support spring is connected in middle deck, the other end is connected in deck of cellar, the elasticity coefficient of support spring is 2000-3000N/m,
Described taking off is provided with gap between protecting platform and the flight-deck of analog platform main body, is equipped with runway, and at the middle part of the protecting platform that takes off, 2-3 road check cable is installed on the protecting platform that takes off.
The present invention utilizes many heavy-duty motors to drive gearing, drive flight-deck to swing up and down all around, and lay rail simulative training platform can be moved ahead on land according to the speed of setting, true simulation aircraft carrier is at large marine operational configuration, for the landing of carrier-borne aircraft provides good test condition, the present invention has following beneficial effect: 1, simulation aircraft carrier platform cost is relatively low, easily manufactures; 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, with the protecting platform that takes off, 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 that ground floor of the present invention is controlled platform, and Fig. 3 is the structural representation that the second layer of the present invention is controlled platform.
Drawing explanation: 1, analog platform main body, 2, the protecting platform that takes off, 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 by reference to the accompanying drawings embodiment in detail.A kind of carrier-borne aircraft landing simulative training platform; comprise analog platform main body 1; protecting platform 2 and conning-tower 3 take off; wherein analog platform main body 1 is mainly used in simulating aircraft carrier at large marine operational configuration; the protecting platform 2 that takes off does not have in the failure of taking off the in the situation that of lift-off for the protection of aircraft; promptly on the protecting platform 2 that takes off, continue to slide, 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, 3 of conning-towers are 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 controls platform and the second layer is controlled platform, wherein ground floor control platform can fluctuate front and back, mainly by middle deck 17 and be arranged at flight-deck 18 and middle deck 17 between actuating unit, supporting mechanism and support spring 15 form, the second layer is controlled platform and can be fluctuated left and right, main by deck of cellar 16 be arranged at the actuating unit between 17Yu deck of cellar, middle deck 16, supporting mechanism and support spring 15 form, described actuating unit comprises motor 5, motor supporting table 6, the first drive link 7, the 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 tops of taking off are provided with runway 19 and check cable 20, conning-tower 3 is seated a side of flight-deck 18, described analog platform main body 1 and the bottom of the protecting platform 2 that takes off are all provided with iron tyre 22, inside is equipped with electric motor and is driven iron tyre 22, the whole rail of being laid by ground 21 supports, can on rail 21, move ahead or fall back.
In the actuating unit of ground floor control platform, motor supporting table 6 is installed on middle deck 17, motor 5 is some, power is 5-10kw, parallel longitudinal is arranged in the both sides of middle deck 17, every 5-7 rice, place one, be arranged on motor supporting table 6, the rotor of motor 5 connects the first drive link 7, by drive link rotating shaft 9, connect the second drive link 8, the second drive link 8 is connected with flight-deck 18 by link 10, motor 5 rotates and just can drive flight-deck 18 front and back to swing up and down by drive link, motor 5 rotating speeds are controlled, for per minute, 20-40 turns, the platform rotating shaft 11 of described supporting mechanism is installed on the positive middle part of flight-deck 18, by rotating shaft link 12, connect flight-deck 18, several heavy bearings 13 are installed in platform rotating shaft 11, heavy bearing 13 is connected and is supported by pillar 14, pillar 14 is arranged on middle deck 17, be used for supporting flight-deck 18, belong to hard connection, some support springs 15 are also installed on middle deck 17, connection middle deck, one end 17, one end connects flight-deck 18, parallel installation side by side, play the effect of supplemental support, the elasticity coefficient of support spring 15 is 2000-3000N/m, height is identical with control podium level, when motor 5 rotates, flight-deck 18 just can swing up and down around platform rotating shaft 11 front and back.
In the actuating unit of second layer control platform, motor supporting table 6 is installed on middle deck 17, motor 5 is some, power is 5-10kw, laterally be parallel to the both sides of deck of cellar 16, every 5-7 rice, place one, be arranged on motor supporting table 6, the rotor of motor 5 connects the first drive link 7, by drive link rotating shaft 9, connect the second drive link 8, the second drive link 8 is connected with middle deck 17 by link 10, motor 5 rotates and just can drive 17 left and right, middle deck to swing up and down by drive link, motor 5 rotating speeds are controlled, for per minute, 20-40 turns, the platform rotating shaft 11 of described supporting mechanism is arranged on positive middle part, middle deck 17, by rotating shaft link 12, connect middle deck 17, several heavy bearings 13 are installed in platform rotating shaft 11, heavy bearing 13 is connected and is supported by pillar 14, pillar 14 is arranged on deck of cellar 16, be used for supporting middle deck 17, belong to hard connection, some support springs 15 are also installed on deck of cellar 16, connection deck of cellar, one end 16, connection middle deck, one end 17, parallel installation side by side, play the effect of supplemental support, the elasticity coefficient of support spring 15 is 2000-3000N/m, height is identical with control podium level, when motor 5 rotates, middle deck 17 just can swing up and down around platform rotating shaft 11 left and right.
It is identical with second layer control working platform principle that ground floor is controlled platform, uses parts also identical, and two-layer control podium level 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 stop; keep relative distance constant; on the protecting platform 2 that takes off, be equipped with runway 19; and at the middle part of the protecting platform 2 that takes off, 2-3 road check cable 20 is installed; the in the situation that protection aircraft not going up to the air in the failure of taking off; can on the protecting platform 2 that takes off, continue to slide; by check cable 22, stop aircraft, protection pilot and aircraft safety, improve safety coefficient.
Whole carrier-borne aircraft landing simulative training platform is supported by the iron tyre 22 that is installed on analog platform main body 1 deck of cellar 16 and protecting platform 2 belows of taking off; the electric motor that drives iron tyre 22 is equipped with in inside; drive iron tyre 22 by setting speed, to move ahead or fall back on the rail 21 of laying; 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 mainly being formed by analog platform main body, take off protecting platform and conning-tower, described analog platform main body is connected with the protecting platform that takes off by coupling assembling, in analog platform main body and the bottom of the protecting platform that takes off, be equipped with iron tyre, electric motor is equipped with in the inside of this iron tyre, by iron tyre, analog platform main body and the protecting platform that takes off are arranged on same rail, 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 controls platform and the second layer is controlled platform, ground floor control platform mainly by middle deck and be arranged at flight-deck and middle deck between actuating unit, supporting mechanism and support spring form, described actuating unit parallel longitudinal is arranged at the both sides of middle deck, comprise motor, motor supporting table, the first drive link, the second drive link, drive link rotating shaft and link, wherein motor supporting table is fixed on middle deck, described motor is installed on motor supporting table, the rotor of motor connects the first drive link, the first drive link connects the second drive link by drive link rotating shaft, the second drive link is connected with flight-deck by link, electric machine rotation swings up and down before and after just can driving flight-deck by drive link, described supporting mechanism 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, by rotating shaft link, connect flight-deck, in platform rotating shaft, heavy bearing is installed, heavy bearing is connected and is supported by pillar, this pillar is installed on middle deck, be used for supporting flight-deck, described support spring is arranged between actuating unit and supporting mechanism, one end of this support spring is connected in flight-deck, the other end is connected in middle deck, the elasticity coefficient of support spring is 2000-3000N/m,
The described second layer control platform mainly by deck of cellar and be arranged at middle deck and deck of cellar between actuating unit, supporting mechanism and support spring form, wherein actuating unit is laterally set in parallel in the both sides of deck of cellar, comprise motor, motor supporting table, the first drive link, the second drive link, drive link rotating shaft and link, wherein motor supporting table is fixed on deck of cellar, described motor is installed on motor supporting table, the rotor of motor connects the first drive link, the first drive link connects the second drive link by drive link rotating shaft, the second drive link is connected with middle deck by link, electric machine rotation just can drive left and right, middle deck to swing up and down by drive link, described supporting mechanism 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, by rotating shaft link, connect middle deck, in platform rotating shaft, heavy bearing is installed, heavy bearing is connected and is supported by pillar, pillar is installed on deck of cellar, be used for supporting middle deck, described support spring is arranged between actuating unit and supporting mechanism, one end of this support spring is connected in middle deck, the other end is connected in deck of cellar, the elasticity coefficient of support spring is 2000-3000N/m,
Described taking off is provided with gap between protecting platform and the flight-deck of analog platform main body, is equipped with runway, and at the middle part of the protecting platform that takes off, 2-3 road check cable is installed on the protecting platform that takes off.
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 |
Publications (2)
| Publication Number | Publication Date |
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| CN103646602A true CN103646602A (en) | 2014-03-19 |
| CN103646602B 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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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112435531A (en) * | 2020-10-29 | 2021-03-02 | 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 |
| CN115457833A (en) * | 2022-09-15 | 2022-12-09 | 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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| CN112435531A (en) * | 2020-10-29 | 2021-03-02 | 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 |
| CN115457833A (en) * | 2022-09-15 | 2022-12-09 | 吉林大学 | Traction robot track control experiment table of offshore operation helicopter |
| 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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| CN103646602B (en) | 2015-07-01 |
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