CN103661932A - Offshore takeoff method for carrier-borne aircraft on common ship - Google Patents
Offshore takeoff method for carrier-borne aircraft on common ship Download PDFInfo
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- CN103661932A CN103661932A CN201310628338.7A CN201310628338A CN103661932A CN 103661932 A CN103661932 A CN 103661932A CN 201310628338 A CN201310628338 A CN 201310628338A CN 103661932 A CN103661932 A CN 103661932A
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- aircraft
- takeoff
- auxiliary slide
- taking
- naval vessel
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Abstract
The invention relates to an offshore takeoff method for an aircraft, in particular to an offshore takeoff method for a carrier-borne aircraft on a common ship. Before the carrier-borne aircraft takes off, an auxiliary sliding plate (1) covering front and rear wheels (2) of the aircraft are suspended on the front and rear wheels (2) and the front and rear wheels (2) extend out of wheel holes (3) formed in the auxiliary sliding plate (1); in the takeoff process, the aircraft takes the auxiliary sliding plate (1) to be started on a deck of the common ship and slide in an accelerating manner; when the running distance of the aircraft exceeds the length of the deck, the aircraft leaves the deck to enter the sea surface, the aircraft slides to the water surface at a suitable inclination angle, the auxiliary sliding plate (1) kicks water on the water surface and is bounced when the aircraft is in contact with the water surface, and the aircraft is separated from the water surface to be continuously accelerated; the aircraft is bounced and accelerated on the sea surface for once or repeatedly; when reaching the takeoff speed, the aircraft flies away from the sea surface; and after the aircraft takes off and enters a stable state, the auxiliary sliding plate (1) falls off and is recovered by the ship and the aircraft retracts an undercarriage and normally flies. The offshore takeoff method adopts the unique characteristic that the auxiliary sliding plate kicks water and is bounced on the sea surface, and realizes short-runway sliding takeoff of the carrier-borne aircraft on the common ship.
Description
Technical field
The present invention is the method for taking off in a kind of aircraft sea, particularly relates to a kind of method of the carrier-borne aircraft that takes off at sea, common naval vessel.
Background technology
At sea taking off of aircraft generally has two kinds of methods, and the first is to have the aircraft of going straight up to the ability of taking off, as: autogyro, jet vertical take-off and landing aircraft (VTOL aircraft) etc., utilize the ability of going straight up to of oneself to rolling takeoff; The second is to utilize aircraft carrier platform, adds that some launch or the deck technology realization of tilting is taken off.
But these two kinds of modes are all limited to.The former, can only be applied to the aircraft that can vertical lift rises and falls, for need, has the fighter plane of certain take-off run speed to use.That the latter must have is broad, taking off of carrier-borne aircraft could be realized in long-distance running road.So greatly limited the use of high-speed flight carrier-borne aircraft.If can realize the flap running take off of carrier-borne aircraft on common naval vessel, by being, the revolutionary character of this area is changed, by greatly expanding the range of use of marine carrier-borne aircraft, greatly improve military capability of the country.
Summary of the invention
The present invention intends providing a kind of can realize the method for taking off in ship-board aircraft sea on common naval vessel, to reach, reduces the carrier-borne aircraft requirement of taking off, and improves the ability of common naval vessel carrying carrier-borne aircraft, strengthens the object of naval vessel fighting capacity.
Object of the present invention is solved by following technical scheme:
The marine takeoff method of ship-board aircraft on common naval vessel, is characterized in that:
Before taking off:
On the front and rear wheel of aircraft, hang an auxiliary slide that covers two-wheeled, in the wheel hole that front and rear wheel is offered from auxiliary slide, expose;
In taking off:
1. aircraft, with auxiliary slide, starts accelerated slip on the deck on common naval vessel;
2. aircraft operating range enters sea over sailing out of deck after deck length, does not reach the lift that takes off, and aircraft slides to the water surface with suitable inclination angle, and when the contact water surface, auxiliary slide and the water surface are fetched water and upspring, and aircraft departs from the water surface to be continued to accelerate;
3. aircraft is through the one or many acceleration of bouncing across the sea;
4. aircraft reaches takeoff speed and flies away from sea;
After taking off:
After taking off, enter stabilized conditions, auxiliary slide is come off, by naval vessel, reclaimed, aircraft is packed up alighting gear and is entered normal flight state.
Principle of the present invention is: under the alighting gear of aircraft, install the auxiliary slide that takes off additional, with the effect of fetching water on take off auxiliary slide and sea, realize aircraft one or many spring across the sea and accelerate to take off.The auxiliary slide that will take off again after taking off comes off, and by naval vessel, is reclaimed, and aircraft enters normal flight state.Its principle is the same by the tile principle that squanders with in life in fact, and difference is that tile does not have power, can not when jumping, accelerate, so finally still fall into the water; And aircraft is dynamic, when jumping, can accelerate, accelerate to a certain degree, finally realize the object that the acceleration of jumping is taken off.
Further, described auxiliary slide is overlooked and is ellipticity, the length of aircraft that front and back length equals 0.5-0.8 times.
Further, the distance of at least exposing 0.3 times of wheel diameter in the wheel hole (3) that described front and rear wheel is offered from auxiliary slide.
Further, in taking off described in, an inclination angle is the angle horizontal by 10-30 degree.
Advantage of the present invention: 1. this takeoff method is the unique mode of taking off in this area, can realize the marine flap of ship-board aircraft on common naval vessel and take off; 2. cost is lower; 3. make common military boats and ships have the long-range attack ability that aircraft carrier just has; Marine fighting capacity and the marine military capabilities of common military boats and ships have greatly been improved.4. a kind of sea that the can be used as unmanned aerial vehicle mode of taking off.5. aspect civilian, can be on large-scale pleasure boat or general cargo carrier, equipment emergency survival aircraft or the aircraft of going sightseeing.
Accompanying drawing explanation
Fig. 1 is a kind of embodiment of the marine takeoff method of a kind of common naval vessel of the present invention ship-board aircraft, wherein aircraft configuration the constructional drawing of auxiliary slide;
Fig. 2 is a kind of embodiment of the marine takeoff method of a kind of common naval vessel of the present invention ship-board aircraft, before taking off, the neutralization of taking off take off after the view of three condition, before taking off, on naval vessel, slide, in taking off, spring is accelerated across the sea, after taking off, leaves sea, rises up into sky;
Fig. 3 is the birds-eye view of Fig. 1 aircraft, and wherein auxiliary slide shows with dotted line.
In figure, the 1st, auxiliary slide, the 2nd, front and rear wheel, the 3rd, wheel hole, the 4th, naval vessel, the 5th, sea.
I be before taking off, on naval vessel, slide, II is that slide across the sea, bounce in taking off acceleration, III is to accelerate to certain speed, leaves sea lift-off.
The specific embodiment
Below in conjunction with accompanying drawing, further describe the present invention.
The marine takeoff method of ship-board aircraft on common naval vessel, is characterized in that:
Before taking off:
On the front and rear wheel 2 of aircraft, hang an auxiliary slide 1 that covers two-wheeled, in the wheel hole 3 that front and rear wheel 2 is offered from auxiliary slide 1, expose;
In taking off:
1. aircraft, with auxiliary slide 1, starts accelerated slip on the deck on common naval vessel;
2. aircraft operating range enters sea over sailing out of deck after deck length, does not reach the lift that takes off, and aircraft slides to the water surface with an inclination angle, and when the contact water surface, auxiliary slide 1 is fetched water and upspring with the water surface, and aircraft departs from the water surface and continues acceleration;
3. aircraft is through the one or many acceleration of bouncing across the sea;
4. aircraft reaches takeoff speed and flies away from sea;
After taking off:
After taking off, enter stabilized conditions, auxiliary slide 1 is come off, by naval vessel, reclaimed, aircraft is packed up alighting gear and is entered normal flight state.
A kind of marine safety takeoff method of realizing ship-board aircraft on common naval vessel.This method is that the auxiliary slide that takes off is installed under undercarriage, aircraft is from slightly taking off on the deck at inclination angle with sea level, although aircraft is when leaving deck, also do not reach the required lift that takes off, but there is certain initial velocity, aircraft meeting and sea interact across the sea, utilize the auxiliary slide that takes off of aircraft, with the water surface phenomenon of fetching water, fetch water and can produce lift, make aircraft on the water surface, produce jump, if the digging angle of initial velocity and the water surface is suitable, aircraft can bounce, after once or for several times spring is accelerated, aircraft reaches takeoff speed, the realization lift-off of taking off.Aircraft is after realization is taken off, and the auxiliary slide that takes off that comes off, is reclaimed by naval vessel, and packs up alighting gear, enters normal flight pattern.
Certainly, the present invention is not suitable for taking off in having the weather of high sea, and needs aviator to have certain driving technique to be grasped.To unmanned aerial vehicle, need design automatic takeoff program.
Described auxiliary slide 1 is overlooked and is ellipticity, the length of aircraft that front and back length equals 0.5-0.8 times.Oval Sliding Resistance of Vehicle Slide is little, easily accelerates, and reaches spring object.The length of auxiliary slide 1 is long or too short is all unfavorable for that aircraft slides across the sea, accelerates, bounces, and the coming off and reclaim of auxiliary slide after the lift-off of being convenient to take off.
The distance of at least exposing 0.3 times of wheel diameter in the wheel hole 3 of offering from auxiliary slide 1 at described front and rear wheel 2.Distance described herein, the size that front and rear wheel 2 exposes, exposes too smallly, slides above deck, accelerates motion and be unreliable, easily wipes and touches deck.Expose too much, entering sea does not affect accelerated slip at sea, just will consider that the reliable in action that comes off of being convenient to after lift-off realizes.
In described taking off, an inclination angle is the angle horizontal by 10-30 degree, to obtain across the sea " spring ", different aircrafts are selected corresponding angle within the scope of this, obtain better effect.
Up to the present the deck running take off that board a plane in common naval vessel can't realize, reason is that common naval vessel does not have sufficiently long skid deck, the present invention has made up the problem of deck length deficiency, to sea, extend, the characteristic that adopts unique auxiliary slide to slide, bounce on sea, has realized the running take off of carrier-borne aircraft on common naval vessel.
Claims (4)
1. the marine takeoff method of ship-board aircraft on common naval vessel, is characterized in that:
Before taking off:
The upper auxiliary slide (1) that hangs a covering two-wheeled of front and rear wheel (2) at aircraft, exposes in the wheel hole (3) that front and rear wheel (2) is offered from auxiliary slide (1);
In taking off:
1. aircraft, with auxiliary slide (1), starts accelerated slip on the deck on common naval vessel;
2. aircraft operating range enters sea over sailing out of deck after deck length, does not reach the lift that takes off, and aircraft slides to the water surface with an inclination angle, and when the contact water surface, auxiliary slide (1) is fetched water and upspring with the water surface, and aircraft departs from the water surface and continues acceleration;
3. aircraft is through the one or many acceleration of bouncing across the sea;
4. aircraft reaches takeoff speed and flies away from sea;
After taking off:
After taking off, enter stabilized conditions, auxiliary slide (1) is come off, by naval vessel, reclaimed, aircraft is packed up alighting gear and is entered normal flight state.
2. the marine takeoff method of ship-board aircraft on common naval vessel according to claim 1, is characterized in that described auxiliary slide (1) is overlooked and is ellipticity, the length of aircraft that front and back length equals 0.5-0.8 times.
3. the marine takeoff method of common naval vessel ship-board aircraft according to claim 1, is characterized in that at least exposing in wheel hole (3) that described front and rear wheel (2) offers from auxiliary slide (1) distance of 0.3 times of wheel diameter.
4. the marine takeoff method of ship-board aircraft on common naval vessel according to claim 1, in taking off described in it is characterized in that, an inclination angle is the angles horizontal by 10-30 degree.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201310628338.7A CN103661932B (en) | 2013-11-29 | 2013-11-29 | A kind of Offshore takeoff method for carrier-borne aircraft on common ship |
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CN201310628338.7A CN103661932B (en) | 2013-11-29 | 2013-11-29 | A kind of Offshore takeoff method for carrier-borne aircraft on common ship |
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CN103661932A true CN103661932A (en) | 2014-03-26 |
CN103661932B CN103661932B (en) | 2016-02-10 |
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Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105151302A (en) * | 2015-10-22 | 2015-12-16 | 葛渠农 | Sliding plate type water surface taking-off and landing device of light airplane, and using method |
CN105752303A (en) * | 2015-12-29 | 2016-07-13 | 深圳前海联合邮轮有限公司 | Method for assisting short takeoff of fixed wing aircraft and ship form |
CN107132853A (en) * | 2017-04-27 | 2017-09-05 | 上海大学 | A kind of seaplane landing system cooperateed with based on many unmanned boats and method |
Citations (5)
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US4462560A (en) * | 1982-01-26 | 1984-07-31 | The United States Of America As Represented By The Secretary Of The Air Force | Airplane take-off system |
JP2001354199A (en) * | 2000-06-09 | 2001-12-25 | Mitsubishi Heavy Ind Ltd | Method and device for taking off/landing of unmanned aircraft |
JP2002284100A (en) * | 2001-03-23 | 2002-10-03 | Yukio Fujimoto | Runway and terminal separation type offshore airport |
US20080283661A1 (en) * | 2006-08-02 | 2008-11-20 | Bruce Hyndman Henley | Remote Controlled Mobile Platform |
CN202345921U (en) * | 2011-10-13 | 2012-07-25 | 王力丰 | Shipboard aircraft lifting system for aircraft carrier |
-
2013
- 2013-11-29 CN CN201310628338.7A patent/CN103661932B/en not_active Expired - Fee Related
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4462560A (en) * | 1982-01-26 | 1984-07-31 | The United States Of America As Represented By The Secretary Of The Air Force | Airplane take-off system |
JP2001354199A (en) * | 2000-06-09 | 2001-12-25 | Mitsubishi Heavy Ind Ltd | Method and device for taking off/landing of unmanned aircraft |
JP2002284100A (en) * | 2001-03-23 | 2002-10-03 | Yukio Fujimoto | Runway and terminal separation type offshore airport |
US20080283661A1 (en) * | 2006-08-02 | 2008-11-20 | Bruce Hyndman Henley | Remote Controlled Mobile Platform |
CN202345921U (en) * | 2011-10-13 | 2012-07-25 | 王力丰 | Shipboard aircraft lifting system for aircraft carrier |
Non-Patent Citations (1)
Title |
---|
张磊等: "有浪条件下舰载机弹射起飞建模研究", 《科学技术与工程》, vol. 12, no. 3, 31 January 2012 (2012-01-31), pages 601 - 606 * |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105151302A (en) * | 2015-10-22 | 2015-12-16 | 葛渠农 | Sliding plate type water surface taking-off and landing device of light airplane, and using method |
CN105752303A (en) * | 2015-12-29 | 2016-07-13 | 深圳前海联合邮轮有限公司 | Method for assisting short takeoff of fixed wing aircraft and ship form |
CN107132853A (en) * | 2017-04-27 | 2017-09-05 | 上海大学 | A kind of seaplane landing system cooperateed with based on many unmanned boats and method |
CN107132853B (en) * | 2017-04-27 | 2020-04-03 | 上海大学 | Water plane landing system and method based on cooperation of multiple unmanned boats |
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