CN104002982A - Rapid taking-off device for aircraft carrier plane - Google Patents

Rapid taking-off device for aircraft carrier plane Download PDF

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Publication number
CN104002982A
CN104002982A CN201310068128.7A CN201310068128A CN104002982A CN 104002982 A CN104002982 A CN 104002982A CN 201310068128 A CN201310068128 A CN 201310068128A CN 104002982 A CN104002982 A CN 104002982A
Authority
CN
China
Prior art keywords
aircraft
aircraft carrier
carrier plane
rapid taking
runway
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
CN201310068128.7A
Other languages
Chinese (zh)
Inventor
邓先勇
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 CN201310068128.7A priority Critical patent/CN104002982A/en
Publication of CN104002982A publication Critical patent/CN104002982A/en
Pending legal-status Critical Current

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Abstract

The invention relates to a rapid taking-off device for an aircraft carrier plane. The device comprises a movable slope runway, a hydraulic unit, a winch and a stopping plate. The device is characterized in that the plane takes off downwards by the aid of the inertia force on the downward slope runway, the hydraulic unit is retracted when not used, and a deck is free of a slope state.

Description

The quick launching apparatus of aircraft carrier ship-board aircraft
One, technical field
The present invention is the quick launching apparatus of a kind of carrier ship-board aircraft.
Two, background technology
Current aircraft carrier takes off fast as the steam ejection of the U.S. takes off, its technical sophistication, and energy consumption is large, use inconvenience, and single sortie consumption time of taking off is long.
Three, summary of the invention
The object of the present invention is to provide that a kind of technology is simple, energy consumption is extremely low, single short aircraft carrier launching device of sortie aircraft time takes off.
Four, detailed description of the invention:
When use, first 2. 1. movable runway is risen by hydraulic compressor, keep gradient state.3. aircraft is pulled back again to the top of upper movable runway with winch.Finally 4. fix aircraft with shifting board, and remove the drag hook of winch.Open shifting board 4. time, aircraft slides downwards fast, thereby now aircraft puts into high gear to reach the effect of taking off fast.

Claims (1)

1. the quick launching apparatus of aircraft carrier ship-board aircraft, 1. it comprise movable domatic runway, and 3. 2. hydraulic compressor, be placed in the winch at movable runway top, and shifting board is 4..
CN201310068128.7A 2013-02-26 2013-02-26 Rapid taking-off device for aircraft carrier plane Pending CN104002982A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201310068128.7A CN104002982A (en) 2013-02-26 2013-02-26 Rapid taking-off device for aircraft carrier plane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201310068128.7A CN104002982A (en) 2013-02-26 2013-02-26 Rapid taking-off device for aircraft carrier plane

Publications (1)

Publication Number Publication Date
CN104002982A true CN104002982A (en) 2014-08-27

Family

ID=51363945

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201310068128.7A Pending CN104002982A (en) 2013-02-26 2013-02-26 Rapid taking-off device for aircraft carrier plane

Country Status (1)

Country Link
CN (1) CN104002982A (en)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4195962A (en) * 1976-01-29 1980-04-01 The United States Of America As Represented By The Secretary Of The Navy Platform loading system
EP0394534A1 (en) * 1989-04-28 1990-10-31 MAN Gutehoffnungshütte Aktiengesellschaft Tractor for aircraft without a towing bar (rotating blade)
CN1557678A (en) * 2004-02-10 2004-12-29 通 刘 Airplane inertial taking off and landing technology
CN1955071A (en) * 2005-10-30 2007-05-02 梁嘉麟 Slope aircraft landing taxi-track on aircraft-carrier deck and its using method
CN202219842U (en) * 2011-09-07 2012-05-16 刘建平 Auxiliary taking-off system of airplane
CN102826231A (en) * 2012-08-31 2012-12-19 赵天烁 Slope downward-sliding takeoff platform for carrier-based aircraft, application aircraft carrier and realization method

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4195962A (en) * 1976-01-29 1980-04-01 The United States Of America As Represented By The Secretary Of The Navy Platform loading system
EP0394534A1 (en) * 1989-04-28 1990-10-31 MAN Gutehoffnungshütte Aktiengesellschaft Tractor for aircraft without a towing bar (rotating blade)
CN1557678A (en) * 2004-02-10 2004-12-29 通 刘 Airplane inertial taking off and landing technology
CN1955071A (en) * 2005-10-30 2007-05-02 梁嘉麟 Slope aircraft landing taxi-track on aircraft-carrier deck and its using method
CN202219842U (en) * 2011-09-07 2012-05-16 刘建平 Auxiliary taking-off system of airplane
CN102826231A (en) * 2012-08-31 2012-12-19 赵天烁 Slope downward-sliding takeoff platform for carrier-based aircraft, application aircraft carrier and realization method

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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

Application publication date: 20140827