CN1955071A - Slope aircraft landing taxi-track on aircraft-carrier deck and its using method - Google Patents
Slope aircraft landing taxi-track on aircraft-carrier deck and its using method Download PDFInfo
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- CN1955071A CN1955071A CN 200510061339 CN200510061339A CN1955071A CN 1955071 A CN1955071 A CN 1955071A CN 200510061339 CN200510061339 CN 200510061339 CN 200510061339 A CN200510061339 A CN 200510061339A CN 1955071 A CN1955071 A CN 1955071A
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- aircraft
- domatic
- landing
- runway section
- takeoff
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Abstract
An arc runway on aircraft carrier for the taking off or landing of aircraft is composed of a straight runway segment and a slope runway segment. For the taking off, said slope segment is used for the taxi and beginning acceleration and said straight segment is used for further acceleration. For the landing, said straight segment is used for the landing and deceleration sliding and said slope segment is used for further deceleration.
Description
Technical field:
The present invention relates to ship-board aircraft landing plane track technology and using method thereof.
Background technology:
As everyone knows, existing huge aircraft carrier overall volume mainly is because the landing plane track that its ship-board aircraft must use determines.At present, for the landing plane track of ship-board aircraft adapted all is positioned on the horizontal surface, can't be when takeoff and landing are slided by the aircraft power-assisted of this runway to landing, and because this runway is long, it is very big to take plan area, adopt the takeoff and landing plane track of pure flat of traditional like this linear on land, problem is little, yet, the also same traditional takeoff and landing plane track of adapted on aircraft carrier, just force the bodily form design-calculated of aircraft carrier very huge, make its manufacture difficulty and manufacturing cost considerablely all big.
Summary of the invention:
The present invention's purpose: the domatic takeoff and landing plane track technology and the using method that propose a kind of adapted aircraft carrier.
In order to realize goal of the invention, intend adopting following technology:
Takeoff and landing plane track of the present invention is an on-plane surface: it comprises end to end linear runway section and domatic runway section; This domatic be straight line or form by radian; Platform is taken off in the high-order bit setting of domatic runway section.
Using method of the present invention: take off when sliding, at first begin descending and quicken (aircraft obtains the acceleration propulsive force of outside domatic runway simultaneously) and slide, begin to do to quicken by a larger margin to slide to take off after entering linear runway section up to liftoff from the shutdown platform of domatic runway section; During aircraft landing, at first begin landing and do to slow down to slide from linear runway section, entering begins to go up a slope after the domatic runway section do to slow down by a larger margin (the deceleration resistance that aircraft obtains outside domatic runway simultaneously) slide up to arriving and shut down platform.
The present invention's characteristics compared with the prior art:
Because allowing ship-board aircraft slide the period at low speed, the present invention can utilize the external force that the domatic runway gives to quicken propulsive force or external force deceleration resistance, this has just created condition for saving the plan area (dwindling warship body volume) that runway takies on the aircraft carrier significantly, thereby has created condition again for the manufacture difficulty and the manufacturing cost that reduce aircraft carrier significantly.
Description of drawings:
Figure has illustrated one embodiment of the present of invention with plan view forms.
1: horizontal surface; 2: the takeoff and landing plane track; 3: shut down platform; 4: the deck, plane of aircraft carrier; 5: the warship body of aircraft carrier; L: linear runway section; S: domatic runway section.
The specific embodiment:
Because takeoff and landing plane track 2 of the present invention is made up of end to end linear runway section L and this two part of domatic runway section S (the road face is arcs of recesses along its length), the part on deck, plane 4 is exactly linear runway section L, and carrier-borne building is arranged on the deck, plane 4 of takeoff and landing plane track 2 sides.
During the aircraft built on stilts or the place of landing during kiss the earth all should be set in above the linear runway section L; and aircraft leaves aircraft after starting and shuts down the descending of platform 3 and quicken to slide behind highway section or the aircraft landing to slow down at the upward slope when shutting down platform 3 and slide the highway section and all be set in the domatic runway section S scope; at this moment; domatic runway section S just will inevitably produce the external force of impelling its acceleration or slowing down that aircraft is applied; as long as its gradient design-calculated is (example: increase its inclined degree) rationally, this auxiliary external force that aircraft is applied quickens or deceleration effort is immeasurable.
This can be increased considerably the effect that external force run-up acceleration or external force damping are slowed down, and be shortened acceleration or the deceleration of aircraft on domatic runway section S significantly with this and slide distance by the external force effect to aircraft that domatic runway section S forms.This will cause the shortening significantly of takeoff and landing plane track 2, and then the design plan that makes the total length design of aircraft carrier also can be shortened significantly becomes realization.
Obviously, the present invention has played vital function for the design of the aircraft carrier bulkiness of the magnitude that reduces to fight on an equal basis.
Claims (4)
1. the domatic takeoff and landing plane track of an adapted aircraft carrier has ship-board aircraft landing plane track, it is characterized in that:
Takeoff and landing plane track (2) is an on-plane surface, and it comprises end to end linear runway section (L) and domatic runway section (S) composition.
2. the domatic takeoff and landing plane track of an adapted aircraft carrier as claimed in claim 1 is characterized in that: described domatic runway section (S) be straight line or form by radian.
3. the domatic takeoff and landing plane track of an adapted aircraft carrier as claimed in claim 1 is characterized in that: the high-order bit of described domatic runway section (S) is provided with aircraft and shuts down platform (3).
4. the using method of the domatic takeoff and landing plane track of an adapted aircraft carrier as claimed in claim 1 is characterized in that:
Take off when sliding, at first quicken to slide, begin to do to quicken by a larger margin to slide to take off after entering linear runway section (L) up to liftoff from the shutdown platform (3) of domatic runway section (S) beginning descending; During aircraft landing, at first begin landing and do to slow down to slide, enter and begin to go up a slope that doing slows down by a larger margin slides up to arriving and shut down platform (3) after the domatic runway section (S) from linear runway section (L).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200510061339 CN1955071A (en) | 2005-10-30 | 2005-10-30 | Slope aircraft landing taxi-track on aircraft-carrier deck and its using method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200510061339 CN1955071A (en) | 2005-10-30 | 2005-10-30 | Slope aircraft landing taxi-track on aircraft-carrier deck and its using method |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN1955071A true CN1955071A (en) | 2007-05-02 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 200510061339 Pending CN1955071A (en) | 2005-10-30 | 2005-10-30 | Slope aircraft landing taxi-track on aircraft-carrier deck and its using method |
Country Status (1)
| Country | Link |
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| CN (1) | CN1955071A (en) |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102556361A (en) * | 2012-02-22 | 2012-07-11 | 北京科实医学图像技术研究所 | All-weather environment-friendly airport |
| CN102765468A (en) * | 2012-06-29 | 2012-11-07 | 北京科实医学图像技术研究所 | Novel design scheme for aircraft carrier runways |
| WO2013034054A1 (en) * | 2011-09-07 | 2013-03-14 | Liu Jianping | Assisted takeoff system for aircraft |
| CN104002982A (en) * | 2013-02-26 | 2014-08-27 | 邓先勇 | Rapid taking-off device for aircraft carrier plane |
| CN104554750A (en) * | 2014-08-24 | 2015-04-29 | 李浩昌 | Land-based, sea-based and seaborne civil airports capable of realizing takeoff on slideway and landing on rampway |
| CN105083579A (en) * | 2014-05-10 | 2015-11-25 | 徐延明 | Landing deck of aircraft carrier |
| CN108791938A (en) * | 2018-05-08 | 2018-11-13 | 西北工业大学 | A kind of fixed-wing UAV launched by warship method |
| CN110588930A (en) * | 2019-09-16 | 2019-12-20 | 青岛度丘新能源技术有限公司 | Aircraft take-off and landing platform of aircraft carrier or large ship |
| CN110606168A (en) * | 2019-09-12 | 2019-12-24 | 青岛度丘新能源技术有限公司 | Suspension steel cable type offshore airplane take-off and landing platform |
| CN112896539A (en) * | 2021-03-19 | 2021-06-04 | 北京空天技术研究所 | Ground assisted take-off runway and method for wheel type horizontal take-off and landing carrier |
-
2005
- 2005-10-30 CN CN 200510061339 patent/CN1955071A/en active Pending
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2013034054A1 (en) * | 2011-09-07 | 2013-03-14 | Liu Jianping | Assisted takeoff system for aircraft |
| CN102556361A (en) * | 2012-02-22 | 2012-07-11 | 北京科实医学图像技术研究所 | All-weather environment-friendly airport |
| CN102765468A (en) * | 2012-06-29 | 2012-11-07 | 北京科实医学图像技术研究所 | Novel design scheme for aircraft carrier runways |
| CN104002982A (en) * | 2013-02-26 | 2014-08-27 | 邓先勇 | Rapid taking-off device for aircraft carrier plane |
| CN105083579A (en) * | 2014-05-10 | 2015-11-25 | 徐延明 | Landing deck of aircraft carrier |
| CN104554750A (en) * | 2014-08-24 | 2015-04-29 | 李浩昌 | Land-based, sea-based and seaborne civil airports capable of realizing takeoff on slideway and landing on rampway |
| CN108791938A (en) * | 2018-05-08 | 2018-11-13 | 西北工业大学 | A kind of fixed-wing UAV launched by warship method |
| CN108791938B (en) * | 2018-05-08 | 2021-09-28 | 西北工业大学 | Shipborne launching method of fixed-wing unmanned aircraft |
| CN110606168A (en) * | 2019-09-12 | 2019-12-24 | 青岛度丘新能源技术有限公司 | Suspension steel cable type offshore airplane take-off and landing platform |
| CN110588930A (en) * | 2019-09-16 | 2019-12-20 | 青岛度丘新能源技术有限公司 | Aircraft take-off and landing platform of aircraft carrier or large ship |
| CN112896539A (en) * | 2021-03-19 | 2021-06-04 | 北京空天技术研究所 | Ground assisted take-off runway and method for wheel type horizontal take-off and landing carrier |
| CN112896539B (en) * | 2021-03-19 | 2023-01-10 | 北京空天技术研究所 | Ground assisted take-off runway and method for wheel type horizontal take-off and landing carrier |
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| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |