JPS5459798A - Aircraft that direction of empennage can be varied - Google Patents

Aircraft that direction of empennage can be varied

Info

Publication number
JPS5459798A
JPS5459798A JP12632877A JP12632877A JPS5459798A JP S5459798 A JPS5459798 A JP S5459798A JP 12632877 A JP12632877 A JP 12632877A JP 12632877 A JP12632877 A JP 12632877A JP S5459798 A JPS5459798 A JP S5459798A
Authority
JP
Japan
Prior art keywords
flight
takeoff
aircraft
minimum
tail
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
JP12632877A
Other languages
Japanese (ja)
Inventor
Hideaki Omiya
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.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries Ltd
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 Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP12632877A priority Critical patent/JPS5459798A/en
Publication of JPS5459798A publication Critical patent/JPS5459798A/en
Pending legal-status Critical Current

Links

Landscapes

  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

PURPOSE: To raise up an airframe wihout troubles when the takeoff of an aircraft while reducing flight resistance by drawing in variable wings during flight, by providing the aircraft with the variable wings, which freely extend along tail planes with minimum area suffiicient for flight.
CONSTITUTION: Portions shown by hatching in tail planes 2, 2, which are projected in a left and right symmetrical shape from a rear drum 1 of an aircraft and have the minimum area sufficient for flight, are extended to the rear or the side by means of actuators 4 only when takeoff, and the areas of the tail planes necessary for takeoff are integrally maintained with the tail plane 2 while being provided with a variably wing 3 or 3' that makes flight resistacne minimum by drawing in the wing when flight. Consequently, since the wing area of the tail plane 2 is expanded when takeoff in this manner the efficiency of the raising-up of an airframe becomes large and takeoff can easily be done, thus resulting in the minimum of the flight resistance during flight, then improving flight performance .
COPYRIGHT: (C)1979,JPO&Japio
JP12632877A 1977-10-20 1977-10-20 Aircraft that direction of empennage can be varied Pending JPS5459798A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP12632877A JPS5459798A (en) 1977-10-20 1977-10-20 Aircraft that direction of empennage can be varied

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP12632877A JPS5459798A (en) 1977-10-20 1977-10-20 Aircraft that direction of empennage can be varied

Publications (1)

Publication Number Publication Date
JPS5459798A true JPS5459798A (en) 1979-05-14

Family

ID=14932457

Family Applications (1)

Application Number Title Priority Date Filing Date
JP12632877A Pending JPS5459798A (en) 1977-10-20 1977-10-20 Aircraft that direction of empennage can be varied

Country Status (1)

Country Link
JP (1) JPS5459798A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH06101999A (en) * 1992-09-17 1994-04-12 Nissan Motor Co Ltd Missile with stabilizing wings
FR2911113A1 (en) * 2007-01-04 2008-07-11 Airbus France Sa Horizontal tail for aircraft, has edge parts slide with respect to intermediate part, where tail presents area assuring stability of aircraft in coasting flight when edge parts are in retracted position
WO2010063868A3 (en) * 2008-12-04 2010-07-29 Airbus Operations, S.L. Aircraft directional control and stabilizing surface
FR2962971A1 (en) * 2010-07-20 2012-01-27 Airbus Operations Sas DEVICE AND METHOD FOR LATERAL STABILIZATION OF AN AIRCRAFT
EP2368793A3 (en) * 2010-03-23 2014-05-07 Deutsches Zentrum für Luft- und Raumfahrt e. V. Manned aircraft
CN109625243A (en) * 2018-12-24 2019-04-16 湖南云箭集团有限公司 A kind of folded surface expansion Aeroassisted driving device

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3065938A (en) * 1960-05-25 1962-11-27 Eugene M Calkins Telescoping sectional airplane wing
US3184187A (en) * 1963-05-10 1965-05-18 Isaac Peter Retractable airfoils and hydrofoils

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3065938A (en) * 1960-05-25 1962-11-27 Eugene M Calkins Telescoping sectional airplane wing
US3184187A (en) * 1963-05-10 1965-05-18 Isaac Peter Retractable airfoils and hydrofoils

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH06101999A (en) * 1992-09-17 1994-04-12 Nissan Motor Co Ltd Missile with stabilizing wings
FR2911113A1 (en) * 2007-01-04 2008-07-11 Airbus France Sa Horizontal tail for aircraft, has edge parts slide with respect to intermediate part, where tail presents area assuring stability of aircraft in coasting flight when edge parts are in retracted position
US8196863B2 (en) 2007-01-04 2012-06-12 Airbus Operations Sas Aircraft horizontal stabilizer
WO2010063868A3 (en) * 2008-12-04 2010-07-29 Airbus Operations, S.L. Aircraft directional control and stabilizing surface
CN102239083A (en) * 2008-12-04 2011-11-09 空中客车运作有限公司 Aircraft directional control and stabilizing surface
ES2382062A1 (en) * 2008-12-04 2012-06-05 Airbus Operations, S.L. Aircraft directional control and stabilizing surface
EP2368793A3 (en) * 2010-03-23 2014-05-07 Deutsches Zentrum für Luft- und Raumfahrt e. V. Manned aircraft
FR2962971A1 (en) * 2010-07-20 2012-01-27 Airbus Operations Sas DEVICE AND METHOD FOR LATERAL STABILIZATION OF AN AIRCRAFT
WO2012017152A1 (en) * 2010-07-20 2012-02-09 Airbus Operations (Sas) Method and device for the lateral stabilization of an aircraft
US8888039B2 (en) 2010-07-20 2014-11-18 Airbus Operations Sas Method and device for the lateral stabilization of an aircraft
CN109625243A (en) * 2018-12-24 2019-04-16 湖南云箭集团有限公司 A kind of folded surface expansion Aeroassisted driving device
CN109625243B (en) * 2018-12-24 2021-08-17 湖南云箭集团有限公司 Pneumatic auxiliary driving device for unfolding of folding wing surface

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