CN203616935U - Shipboard aircraft taking-off and landing simulation training platform - Google Patents
Shipboard aircraft taking-off and landing simulation training platform Download PDFInfo
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- CN203616935U CN203616935U CN201320799100.6U CN201320799100U CN203616935U CN 203616935 U CN203616935 U CN 203616935U CN 201320799100 U CN201320799100 U CN 201320799100U CN 203616935 U CN203616935 U CN 203616935U
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- 238000004088 simulation Methods 0.000 title claims abstract description 20
- 230000005540 biological transmission Effects 0.000 claims abstract 19
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 23
- 230000007246 mechanism Effects 0.000 claims description 22
- 229910052742 iron Inorganic materials 0.000 claims description 12
- 238000005516 engineering process Methods 0.000 description 5
- 230000008878 coupling Effects 0.000 description 4
- 238000010168 coupling process Methods 0.000 description 4
- 238000005859 coupling reaction Methods 0.000 description 4
- 241001310793 Podium Species 0.000 description 3
- 241000209094 Oryza Species 0.000 description 2
- 235000007164 Oryza sativa Nutrition 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 235000009566 rice Nutrition 0.000 description 2
- 230000000153 supplemental effect Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007123 defense Effects 0.000 description 1
- 150000002505 iron Chemical class 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
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Abstract
本实用新型公开了一种舰载机起降模拟训练平台。本实用新型的技术方案要点为：一种舰载机起降模拟训练平台，包括模拟平台主体、起飞保护平台和指挥塔，其中模拟平台主体主要负责模拟航空母舰在大海中航行状态，起飞保护平台负责保护飞机在起飞失败没有升空的情况下，紧急在起飞保护平台上继续滑行，指挥塔操作控制模拟平台的状态参数以及飞机起降信息指挥。本实用新型利用多台大功率电机带动传动装置，驱动飞行甲板前后左右上下摆动，并铺设铁轨使模拟平台能够按照设定速度在陆地上前行，相对真实地模拟航母在大海中的航行状态，为舰载机的起降提供了良好的试验条件。
The utility model discloses a simulation training platform for take-off and landing of carrier-based aircraft. The key points of the technical scheme of the utility model are: a carrier-based aircraft take-off and landing simulation training platform, including a simulation platform main body, a take-off protection platform and a command tower, wherein the simulation platform main body is mainly responsible for simulating the navigation state of an aircraft carrier in the sea, and the take-off protection platform is responsible for Protect the aircraft from taking off and fail to take off, and continue taxiing on the takeoff protection platform in an emergency. The control tower operates and controls the state parameters of the simulation platform and the aircraft takeoff and landing information command. The utility model utilizes a plurality of high-power motors to drive the transmission device, drives the flight deck to swing up and down, and lays rails so that the simulation platform can move forward on the land according to the set speed, relatively realistically simulating the sailing state of the aircraft carrier in the sea. The take-off and landing of carrier-based aircraft provides good test conditions.
Description
Technical field
The utility model relates to a kind of carrier-borne aircraft landing analog training device, is 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.But carrier-borne aircraft 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 complexity, 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, but 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 utility model 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 when 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.
The technical solution of the utility model 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, be equipped with iron tyre 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, 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 control platform and second layer control 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 composition, 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, connect flight-deck by rotating shaft link, 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,
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 composition, 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, connect middle deck by rotating shaft link, 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 taking off, and 2-3 road check cable is installed at the middle part of the protecting platform that takes off on protecting platform.
The utility model utilizes many heavy-duty motors to drive gearing, drive flight-deck to swing up and down all around, and lay rail make simulative training platform can according to set speed move ahead on land, true simulation aircraft carrier is at large marine operational configuration, for the landing of carrier-borne aircraft provides good test condition, the utlity model has following beneficial effect: 1, simulation aircraft carrier platform cost is relatively low, easily manufactures; 2, the utility model 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 utility model, 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 utility model, and Fig. 2 is the structural representation of the utility model ground floor control 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, 7, the first drive link, 8, the 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; take off protecting platform 2 for the protection of aircraft in the situation that the failure of taking off is not gone up to the air; promptly on protecting platform 2, continue to slide taking off, 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 control platform and second layer control 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, second layer control platform can fluctuate left and right, mainly by deck of cellar 16 and be arranged at middle deck 17 and deck of cellar 16 between actuating unit, 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 rail 21 that entirety is laid by ground 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, place one every 5-7 rice, be arranged on motor supporting table 6, the rotor of motor 5 connects the first drive link 7, connect the second drive link 8 by drive link rotating shaft 9, the second drive link 8 is connected with flight-deck 18 by link 10, motor 5 rotates by drive link and just can drive flight-deck 18 front and back to swing up and down, 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, connect flight-deck 18 by rotating shaft link 12, several heavy bearings 13 are installed in platform rotating shaft 11, heavy bearing 13 connects support 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, in the time that 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, place one every 5-7 rice, be arranged on motor supporting table 6, the rotor of motor 5 connects the first drive link 7, connect the second drive link 8 by drive link rotating shaft 9, the second drive link 8 is connected with middle deck 17 by link 10, motor 5 rotates by drive link and just can drive 17 left and right, middle deck to swing up and down, 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, connect middle deck 17 by rotating shaft link 12, several heavy bearings 13 are installed in platform rotating shaft 11, heavy bearing 13 connects support 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, in the time that motor 5 rotates, middle deck 17 just can swing up and down around platform rotating shaft 11 left and right.
Ground floor control platform is identical with second layer control working platform principle, 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 protecting platform 2, be equipped with runway 19 taking off; 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 in the situation that the failure of taking off is gone up to the air; can on protecting platform 2, continue to slide taking off; 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 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 to move ahead or fall back by setting speed on the rail 21 of laying; rail 21 amounts to 2-3 road, and length is 2000-3000m.
Claims (1)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320799100.6U CN203616935U (en) | 2013-12-09 | 2013-12-09 | Shipboard aircraft taking-off and landing simulation training platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320799100.6U CN203616935U (en) | 2013-12-09 | 2013-12-09 | Shipboard aircraft taking-off and landing simulation training platform |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203616935U true CN203616935U (en) | 2014-05-28 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320799100.6U Expired - Lifetime CN203616935U (en) | 2013-12-09 | 2013-12-09 | Shipboard aircraft taking-off and landing simulation training platform |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203616935U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103646602A (en) * | 2013-12-09 | 2014-03-19 | 河南师范大学 | Simulated ship-bone aircraft take-off and landing training platform |
| CN105836151A (en) * | 2015-10-23 | 2016-08-10 | 范云生 | Shipboard aircraft stable taking-off and landing device and control method |
-
2013
- 2013-12-09 CN CN201320799100.6U patent/CN203616935U/en not_active Expired - Lifetime
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103646602A (en) * | 2013-12-09 | 2014-03-19 | 河南师范大学 | Simulated ship-bone aircraft take-off and landing training platform |
| CN105836151A (en) * | 2015-10-23 | 2016-08-10 | 范云生 | Shipboard aircraft stable taking-off and landing device and control method |
| CN105836151B (en) * | 2015-10-23 | 2018-01-16 | 范云生 | A kind of ship carries the stable lifting gear of aircraft and control method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20140528 Effective date of abandoning: 20150701 |
|
| RGAV | Abandon patent right to avoid regrant |