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 PDF

Info

Publication number
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
Authority
CN
China
Prior art keywords
aircraft
domatic
landing
runway section
takeoff
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN 200510061339
Other languages
Chinese (zh)
Inventor
梁嘉麟
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to CN 200510061339 priority Critical patent/CN1955071A/en
Publication of CN1955071A publication Critical patent/CN1955071A/en
Pending legal-status Critical Current

Links

Landscapes

  • Road Paving Structures (AREA)

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

The domatic takeoff and landing plane track and the using method thereof of adapted aircraft carrier
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).
CN 200510061339 2005-10-30 2005-10-30 Slope aircraft landing taxi-track on aircraft-carrier deck and its using method Pending CN1955071A (en)

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

ID=38062683

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
CN (1) CN1955071A (en)

Cited By (10)

* Cited by examiner, † Cited by third party
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

Cited By (12)

* Cited by examiner, † Cited by third party
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

Similar Documents

Publication Publication Date Title
CN1955071A (en) Slope aircraft landing taxi-track on aircraft-carrier deck and its using method
WO2009036302A3 (en) Play set for toy vehicles
WO2004041640A8 (en) Slotted aircraft wing
WO2006022813A3 (en) High-lift, low-drag dual fuselage aircraft
CN203975236U (en) The runway device that slope underriding Xiang row auxiliary ship carrier aircraft is taken off
CN200985093Y (en) Water-driving arrangement for ground effect aircraft
CN1804220A (en) Slope-shaped airplane runway covering small area and use method thereof
CN205034192U (en) Double -deck diffuser of cycle racing
CN204688240U (en) A kind of automobile spoiler draw off gear of fluid control
CN205340140U (en) Track toy
CN1955070A (en) Arc aircraft landing taxi-track on aircraft-carrier deck and its using method
CN207153070U (en) A kind of folding portable body-building skis
CN201296149Y (en) Amphibious catamaran hydrofoil sightseeing boat
CN101070067A (en) Air-cushion ship based on air stabilizer fin
CN202186377U (en) Driver control console for railcar
CN207311000U (en) A kind of amphibian automobile that can be travelled on ice-snow field
CN1792715A (en) Wingless aircraft and implementing thereof
CN204587057U (en) A kind of automobile-used deployable and collapsible falls and obstructs stream plate structure
CN2510132Y (en) Human-body emitting amusement machine
CN202295290U (en) Novel separating channel structure of air inlet channel
CN108176055A (en) A kind of roller coaster track
CN103349838B (en) Simulated dragon boat toy
Schwind et al. Effects of blowing spanwise from the tips of low-aspect ratio wings of varying taper ratio, with application to improving STOL capability of fighter aircraft[Final Report, 1 Apr. 1982- 30 Sep. 1982]
CN208641732U (en) The device of cable bridge in a kind of simulation wind
CN107458578A (en) Imitative flying fish formula flight bus

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
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