CN102514721A - Aircraft (or rocket or guided missile) take-off (launching) and landing aid - Google Patents
Aircraft (or rocket or guided missile) take-off (launching) and landing aid Download PDFInfo
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- CN102514721A CN102514721A CN2011104238015A CN201110423801A CN102514721A CN 102514721 A CN102514721 A CN 102514721A CN 2011104238015 A CN2011104238015 A CN 2011104238015A CN 201110423801 A CN201110423801 A CN 201110423801A CN 102514721 A CN102514721 A CN 102514721A
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Abstract
The invention relates to an aircraft (or rocket or guided missile) take-off (launching) and landing aid and belongs to the technology of aircraft (or rocket or guided missile) take-off (launching) and landing. An aircraft is located on a rail, runs forwards when the rail moves backwards, and the aircraft takes off and the rail slows down after the aircraft and the rail run at a certain speed. Or, a rocket (or aircraft or guided missile) is located on a railcar which is located on a rail, the railcar runs forwards when the rail moves backwards, the rocket (or aircraft or guided missile) is separated from the railcar after the railcar runs at a certain speed, and simultaneously an engine is ignited to start, and then the rocket takes off or is launched. When in landing, the aircraft lands on a runway behind the rail to slide onto the rail and then slides forwards while the rail moves backwards so that the rail and the aircraft run synchronously. Further, the rail decelerates along with deceleration of the aircraft, and the aircraft slides off the rail and stops on the runway in front of the rail when the rail stops running.
Description
Technical field
The present invention relates to aircraft (or rocket, guided missile) lift-off technology; Relate to the aircraft landing technology.
Background technology
One, aircraft takes off on runway, needs a runway; Rocket, guided missile are launched on launcher, need a launcher.Aircraft, large-scale more aircraft, the aircraft that speed is fast more, the runway that needs is long more, and the result just needs a large amount of the input: runway, beacon light etc.; And aircraft (or rocket, guided missile) accelerates to (or emission) speed of taking off from zero velocity, accelerates to desirable flying speed again, and this just needs to consume a large amount of fuel; Simultaneously, these fuel all are loaded in the aircraft (or rocket, guided missile), have increased the weight of aircraft (or rocket, guided missile), the weight of these increases, and the fuel that need increase consumption again promotes.
Two, during aircraft landing, need runway equally, and large-scale more aircraft, the aircraft that speed is fast more, the runway that needs is long more, and the result needs a large amount of the input: runway, beacon light etc.; Moreover, ice, snow is to the influence of runway, causes the aircraft can't landing, and, need a large amount of human and material resources remove the ice and snow on the runway again.
Summary of the invention
The objective of the invention is: one, a kind of device is provided, assists aircraft (or rocket, guided missile) take off (or emission); Two, a kind of device is provided, shortens airstrip, assist aircraft landing.
Technical scheme of the present invention: first, the technical scheme of aircraft (or rocket, guided missile) take off (or emission) assisted; Second, the technical scheme of shortening airstrip, assistance aircraft landing.
First assists the technical scheme of aircraft (or rocket, guided missile) take off (or emission), and can be divided into two methods again: first method: a track is set, and aircraft orbits and takes off; Second method: a track, rail vehicle are set, and rocket (or aircraft, guided missile) is placed on the rail vehicle, and (or emission) then orbits and take off.
First method a: track is set, aircraft orbits and take off: as shown in Figure 1; A track (1) is set; Aircraft (2) is seated on the track (1), and track (1) is fall back (accompanying drawing is shown as to left) backward, the operation (accompanying drawing is shown as to right-hand) of advancing forward of aircraft (2) retrofire; And track (1) is more and more faster with the speed of aircraft (2).Track (1) is drawn back and the progressive speed of aircraft (2), and both carry out synchronously; Why track (1) is drawn back to march forward with aircraft (2) and is carried out synchronously, is because can keep aircraft (2) all the time at the certain position of track (1) like this.After aircraft (2) runs to certain speed (desirable takeoff speed), track (1) reduces speed now, and aircraft (2) de-orbits (1) to airflight, and track (1) is just out of service after aircraft (2) takes off.
The characteristics of first method: (first), because aircraft (2) moves on track (1) and takes off, shortened runway; (second), be particularly suitable under particular surroundings (runway that such length can't be arranged) utilization, for example on aircraft carrier, use; (the third), corresponding minimizing simultaneously drops in a large number: runway, beacon light etc.(fourth), alleviate the influence of ice and snow to runway.Track (1), as long as an operation just can be gone up ice and snow with track (1) and eliminated, human and material resources, the time of cost are much littler than existing runway.
Second method: a track (1), rail vehicle (3) are set, and rocket (or aircraft, guided missile) (4) is loaded on the rail vehicle (3), goes up operation at track (1) then, and is as shown in Figure 2.Why to add again and put a rail vehicle (3); Rocket (or aircraft, guided missile) (4) is loaded on the rail vehicle (3); Because rocket, guided missile (4) can't directly be gone up the operation emission at track (1); Therefore only be loaded on the rail vehicle (3), aircraft (2) also can be loaded on the rail vehicle (3) certainly.Equally; Track (1) is fall back (accompanying drawing is shown as to left) backward; Advance the forward operation (accompanying drawing is shown as to right-hand) of the rail vehicle (3) of having put rocket (or aircraft, guided missile) (4), and track (1) is more and more faster with the speed of rail vehicle (3).Track (1) is drawn back and the progressive speed of rail vehicle (3), and both have so just ensured that with the speed operation rail vehicle (3) operates in the certain position of track (1).After rail vehicle (3) runs to certain speed (being the desirable emission rate of desirable takeoff speed, rocket and the guided missile of aircraft)); Rocket on the rail vehicle (3) (or aircraft, guided missile) (4) separates with rail vehicle (3); Rocket (or aircraft, guided missile) (4) car (3) that de-orbits is to airflight.
Rocket on the rail vehicle (3) (or aircraft, guided missile) (4) separates with rail vehicle (3); Can there be two kinds: (A) after rail vehicle (3) runs to certain speed (being the desirable emission rate of desirable takeoff speed, rocket and the guided missile of aircraft); The engine ignition of rocket (or aircraft, guided missile) (4) starts; Simultaneously the rocket on the rail vehicle (3) (or aircraft, guided missile) (4) separates with rail vehicle (3), and rocket (or aircraft, guided missile) (4) flies; (B) or also can rocket the driving engine elder generation retrofire of (or aircraft, guided missile) (4), the rocket on the rail vehicle (3) (or aircraft, guided missile) (4) separates with rail vehicle (3) more then, rocket (or aircraft, guided missile) (4) flies.Retrofire has a time difference with separating, and separation should be after igniting.Can increase the running velocity (speed that under original vehicle track running speed, increases) of rail vehicle (3) because rocket after (or aircraft, guided missile) (4) igniting; At this moment rail vehicle (3) just can not remain on the fixed position on the track (1); But displacement forward; In order to guarantee that rail vehicle (3) remains on the fixed position on the track (1), at this moment will increase the running velocity that track (1) is drawn back.
In addition, explain in conjunction with Fig. 3-6.First, second method all can have a bont (5) at the front end (being right-hand shown in the figure) of track (1), the lifting that can make progress gradually, and its degree of dip is 0
0--90
0Between, wherein Fig. 4, Fig. 6 are the condition diagram of bont after promoting.When aircraft (2) or the rail vehicle (3) that loading rocket (or aircraft, guided missile) and track (1) when bringing into operation; Bont (5); Just beginning gradually upwards to promote, rising to certain degree of dip, will help taking off of aircraft (or rocket, guided missile).
The characteristics of second method are: except first method " because aircraft take off in orbit, shortened runway " waits outside four characteristics, also increased by two following characteristics.
The speed of taking off of (first), rocket (or aircraft, guided missile) (4) is: " inertia+acceleration/accel "; Rather than existing rocket (or aircraft, guided missile) (4) " quiescence+acceleration/accel " that take off; This " inertia " is after rail vehicle (3) runs to certain speed; Cause " inertia " of the rocket that is seated on the rail vehicle (3) (or aircraft, guided missile) (4); Rocket (or aircraft, guided missile) (4) takes off at " inertia " state down-firing, " acceleration/accel " that engine ignition produces.At this moment, the flight of rocket (or aircraft, guided missile) (4) is in " inertia+acceleration/accel " flight down, will be much faster than the speed of " quiescence+acceleration/accel ", will reduce the fuel of rocket between this section gap (or aircraft, guided missile) (4) simultaneously.
(second), also reduce the weight of rocket (or aircraft, guided missile) (4) because fuel is to be stored in the rocket (or aircraft, guided missile) (4), the weight of increase then need increase the fuel of take off (or emission).
Second, the technical scheme of shortening airstrip, assistance aircraft landing.
As shown in Figure 1.A track (1) is set, and is one section runway 1 (7) (being shown as left among the figure) in the rear end of track (1), is one section runway 2 (8) (being shown as right-hand among the figure) at the front end of track (1).In aircraft (2) when landing, drop to earlier on the runway 1 (7) behind the track, after slide on the track (1); Track (1) moves (being shown as to left among the figure) backward, and aircraft (2) slides (being shown as among the figure to right-hand) forward; Along with aircraft (2) runs slowly, track (1) also slowly runs slowly simultaneously, and both all slow down synchronously, can keep aircraft (2) to remain on the certain position of track (1) like this.When aircraft (2) when decelerating to certain speed, when track (1) was out of service, aircraft (2) still had certain velocity inertial, skidded off track (1), the runway 2 (8) of injection (1) front end, and stop on the runway 2 (8).
The characteristics of present technique scheme are: 1, shortened runway, simultaneously, large, medium and small type aircraft all can land.In general, the runway of the aircraft needs that large-scale aircraft, speed are fast more is long more, and the large aircraft of operation this programme, the time that fireballing aircraft slides are only in orbit grown a little; 2, be particularly suitable under particular surroundings (runway that such length can't be arranged), for example on aircraft carrier, use; 3, also corresponding minimizing simultaneously drops in a large number: runway, beacon light etc.; 4, alleviate the influence of ice and snow to runway.Track is as long as an operation just can be eliminated ice and snow on the track; Runway in that track is forward and backward is not long, and human and material resources, the time of eliminating ice and snow are much littler than existing runway.
First scheme can combine with alternative plan, and aircraft (2) both can take off on track (1) like this, can on track (1), land again.
Description of drawings
Fig. 1: aircraft orbits and flight-ready longitudinal sectional view.
Fig. 2: the rail vehicle that is loading rocket (or aircraft, guided missile) orbits and the longitudinal sectional view of standby for takeoff (or emission).
Fig. 3: the longitudinal sectional view that the track of bont is arranged.
Fig. 4: the track condition (longitudinal sectional view) after bont promotes.
Fig. 5: the track of bont is arranged and the longitudinal sectional view of rail vehicle is arranged.
Fig. 6: track condition (longitudinal sectional view) after bont promotes and that rail vehicle is arranged.
Fig. 7: be birds-eye view.Demonstrate a plurality of tracks and (show 4 tracks among the figure) side by side, and front and back runway, i.e. runway 2, runway 1.
Among the figure: (1) track; (2) aircraft; (3) rail vehicle; (4) rocket (or aircraft, guided missile); (5) bont; (6) electrical motor of bont; (7) runway 1; (8) runway 2.
The specific embodiment
First embodiment: the scheme that aircraft orbits and takes off.
Explain in conjunction with accompanying drawing 1.The forward and backward of track (1) is runway 2 (8) (being shown as right-hand among the figure), runway 1 (7) (being shown as left among the figure); Track (1) is absorbed in underground; Top and runway 1 (7), the runway 2 (8) of track (1) flush; Like this, be convenient to aircraft (2), or get into runway 2 (8) from track (1) from runway 1 (7) injection (1).Track (1) can drive operation by electrical motor (or combustion engine).Survey the running velocity of aircraft (2) on track (1) by knotmeter, control the running velocity of track (1) thus, can keep aircraft (2) so all the time at the certain position of track (1).
Can be a plurality of tracks (1) side by side, accompanying drawing 7 is its birds-eye vieies, shows 4 tracks among the figure, and before and after runway, i.e. runway 2 (8), runway 1 (8).Can move many airplanes simultaneously takes off.
Operation procedure is following:
The first step: aircraft (2) is pulled (or aircraft sails into voluntarily) runway 1 (7) into by trailer;
Second step: aircraft is again by runway 1 (7) injection (1);
The 3rd step: track (1) is fall back (accompanying drawing is shown as to left) backward, aircraft (2) operation (accompanying drawing is shown as to right-hand) of advancing forward, and also the speed of track (1) and aircraft (2) is more and more faster.Track (1) is drawn back and the progressive speed of aircraft (2), and both carry out synchronously, remain the certain position of aircraft (2) in track (1);
The 4th step: track (1) slows down, and still in continuing speedup, aircraft (2) flies away from track (1) to aircraft (2), to airflight.
Second embodiment: the improvement on the first embodiment basis.
Explain in conjunction with Fig. 3, Fig. 4.Front end (being right-hand shown in the figure) in track (1) has increased a bont (5), drives by electrical motor (6), and the lifting that can make progress gradually, its degree of dip is 0
0--90
0Between, but general as long as 10
0--60
0When aircraft (2) and track (1) when bringing into operation, bont (5) just beginning upwards to promote gradually, rises to certain degree of dip, will help taking off of aircraft (2).
Operation procedure is identical with first embodiment basically, but when the 3rd step, when track (1) moved with aircraft (2), bont (5) also upwards promoted gradually.
The 3rd embodiment: the improvement on first, second embodiment basis.
Explain in conjunction with Fig. 2.Increased a rail vehicle (3); Mainly be to consider that rocket, guided missile (4) can't directly upward move at track (1); Therefore; Set up a rail vehicle (3), let rocket, guided missile (4) be seated in rail vehicle (3) and go up (aircraft also can be seated on the rail vehicle certainly), rail vehicle (3) is gone up operation at track (1).Orbit car (3) can be by electric power or combustion engine as power.
Operation procedure is identical with second embodiment basically; Preceding two examples are that aircraft (2) is gone up operation at track (2); Present embodiment is that rail vehicle (3) is gone up operation at track (1); But change into the time in the 4th step: when running to rocket (or aircraft, guided missile) (4) desirable takeoff speed, rail vehicle (3) and rocket (or aircraft, guided missile) (4) separate, and rocket (or aircraft, guided missile) (4) takes off.
Accompanying drawing 7 is birds-eye vieies.A plurality of tracks (1) (among the figure show 4 tracks) are side by side arranged, can move taking off, launching of many airplanes (or rocket, guided missile) simultaneously.
The 4th embodiment: the scheme that shortens airstrip, assistance aircraft landing.
Explain in conjunction with accompanying drawing 1.The forward and backward of track (1) is runway 2 (8) (being the right-hand of accompanying drawing), runway 1 (7) (being the left of accompanying drawing), and track (1) is absorbed in underground, and top and runway 1 (7), the runway 2 (8) of track (1) flush.
Accompanying drawing 7 is birds-eye vieies.There are a plurality of tracks (1) (to show 4 tracks among the figure) side by side, can move many airplane landing simultaneously.
Operation procedure is following:
The first step: aircraft (2) drops to runway 1 (7);
Second step: aircraft (2) slides on the track (1);
The 3rd step: aircraft (2) ahead running (being shown in the figure) to right-hand; Track (1) moves (being to left shown in the figure) backward; Both are with the speed operation; Along with the inertia deceleration of aircraft (2), track (1) also slows down with constant velocity, remains the certain position of aircraft (2) in track (1);
The 4th step: track (1) is out of service, and aircraft (2) skids off track (1), gets into runway 2 (8), and is parked on the runway 2 (8).
First, second, the 4th embodiment, the three can combine, like this, aircraft (2) track both capable of using (1) takes off, track also capable of using (1) lands.
Second, third, the 4th embodiment, the three can combine, like this, but both aircraft (2) took off and land at track (1), can use also that rail vehicle (3) is fired a rocket, guided missile (or the aircraft that takes off).
Claims (8)
1. the device of an assistance aircraft (or rocket, guided missile) take off (emission) is provided with track (1), rail vehicle (3), it is characterized in that: aircraft (2) directly moves and takes off at track (1); Rocket (or aircraft, guided missile) (4) is loaded on the rail vehicle (3), and rail vehicle (3) is gone up operation and emission (taking off) at track (1).
2.. a device of assisting aircraft landing is provided with track (1), it is characterized in that: the forward and backward of track (1) is runway 2 (8), runway 1 (7); Track (1) is absorbed in underground, and top and runway 1 (7), the runway 2 (8) of track (1) flush.
The device of (emission) 3.. assistance aircraft according to claim 1 (or rocket) takes off is characterized in that: the forward and backward of track (1) is runway 2 (8), runway 1 (7); Track (1) is absorbed in underground, and top and runway 1 (7), the runway 2 (8) of track (1) flush.
4.. the device of assistance aircraft according to claim 1 (or rocket, guided missile) take off (emission), it is characterized in that: aircraft (2) ahead running (accompanying drawing is shown as to right-hand), track (1) move (accompanying drawing is shown as to left) backward.
The device of (emission) 5.. assistance aircraft according to claim 1 (or rocket) takes off is characterized in that: rail vehicle (3) ahead running (accompanying drawing is shown as to right-hand), track (1) move (accompanying drawing is shown as to left) backward.
6.. the device of assistance aircraft according to claim 1 (or rocket, guided missile) take off (emission); It is characterized in that: the front end (accompanying drawing is shown as right-hand) of track (1) has increased a bont (5); The lifting that can make progress gradually, its degree of dip is 0
0--90
0Between.
7.. the device of assistance aircraft according to claim 1 (or rocket, guided missile) take off (emission) is characterized in that: rail vehicle (3) can separate with rocket (or aircraft, guided missile) (4) on being loaded in rail vehicle (3).
8. the device of assistance aircraft landing according to claim 2 is characterized in that: the front end (accompanying drawing is depicted as right-hand) of track (1) has increased a bont (5), the lifting that can make progress gradually, and its degree of dip is 0
0--90
0Between.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011104238015A CN102514721A (en) | 2011-12-18 | 2011-12-18 | Aircraft (or rocket or guided missile) take-off (launching) and landing aid |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011104238015A CN102514721A (en) | 2011-12-18 | 2011-12-18 | Aircraft (or rocket or guided missile) take-off (launching) and landing aid |
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| Publication Number | Publication Date |
|---|---|
| CN102514721A true CN102514721A (en) | 2012-06-27 |
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|---|---|---|---|
| CN2011104238015A Pending CN102514721A (en) | 2011-12-18 | 2011-12-18 | Aircraft (or rocket or guided missile) take-off (launching) and landing aid |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103587711A (en) * | 2013-04-28 | 2014-02-19 | 叶元华 | Arresting device and runway being provided with arresting device |
| CN105667822A (en) * | 2016-03-30 | 2016-06-15 | 代翔 | Aircraft cyclic transfer traction system |
| CN107933945A (en) * | 2017-12-12 | 2018-04-20 | 杨富云 | Aircraft carrier rises and falls method and its device |
| CN108408075A (en) * | 2017-02-09 | 2018-08-17 | 陈云桥 | Aircraft carrier landing high-speed annular mobile device |
| CN109341416A (en) * | 2018-11-26 | 2019-02-15 | 姚黎明 | Increase a kind of facility of rocket launching thrust |
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| CN201712792U (en) * | 2009-10-19 | 2011-01-19 | 刘克良 | Airplane taking-off and landing platform |
| CN102120493A (en) * | 2010-01-08 | 2011-07-13 | 徐清华 | Method and structure for assisting takeoff, landing and flying-unrelated operations of airplanes by using locomotive and railcar |
| CN102198864A (en) * | 2011-02-22 | 2011-09-28 | 和近建 | Power rotation runway and take-off and landing operation method thereof |
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| FR2762292A1 (en) * | 1997-04-18 | 1998-10-23 | Hubert Mourer | Take off assist drive for aircraft from short runways |
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Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103587711A (en) * | 2013-04-28 | 2014-02-19 | 叶元华 | Arresting device and runway being provided with arresting device |
| CN105667822A (en) * | 2016-03-30 | 2016-06-15 | 代翔 | Aircraft cyclic transfer traction system |
| CN105667822B (en) * | 2016-03-30 | 2018-07-27 | 成都天空营地科技有限公司 | A kind of aircraft cyclic transfer trailer system |
| CN108408075A (en) * | 2017-02-09 | 2018-08-17 | 陈云桥 | Aircraft carrier landing high-speed annular mobile device |
| CN107933945A (en) * | 2017-12-12 | 2018-04-20 | 杨富云 | Aircraft carrier rises and falls method and its device |
| CN109341416A (en) * | 2018-11-26 | 2019-02-15 | 姚黎明 | Increase a kind of facility of rocket launching thrust |
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Application publication date: 20120627 |