FR2254481A1 - Aircraft with canards and twin fin tailplane - has stable control afforded by canards anhedrally and fins dihedrally arranged - Google Patents

Aircraft with canards and twin fin tailplane - has stable control afforded by canards anhedrally and fins dihedrally arranged

Info

Publication number
FR2254481A1
FR2254481A1 FR7440848A FR7440848A FR2254481A1 FR 2254481 A1 FR2254481 A1 FR 2254481A1 FR 7440848 A FR7440848 A FR 7440848A FR 7440848 A FR7440848 A FR 7440848A FR 2254481 A1 FR2254481 A1 FR 2254481A1
Authority
FR
France
Prior art keywords
aircraft
canards
dihedrally
fins
anhedrally
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.)
Withdrawn
Application number
FR7440848A
Other languages
French (fr)
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.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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
Priority claimed from DE19732361888 external-priority patent/DE2361888C3/en
Application filed by Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of FR2254481A1 publication Critical patent/FR2254481A1/en
Withdrawn legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Mechanical Control Devices (AREA)
  • Toys (AREA)

Abstract

The aircraft has a pair of conventional wings arranged one on either side of the fuselage for generating lift. Canard wings with pronounced anhedral are mounted on the nose of the aircraft to form an inverted V-shape and twin tail fins are dihedrally arranged at the tail of the aircraft to form an upwardly diverging V. An electrical control circuit trims the canards and the tail fins in response to measured deviations of the aircraft from the demanded path thereby controlling pitch and yaw and correcting the path stability of the aircraft.
FR7440848A 1973-12-13 1974-12-11 Aircraft with canards and twin fin tailplane - has stable control afforded by canards anhedrally and fins dihedrally arranged Withdrawn FR2254481A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19732361888 DE2361888C3 (en) 1973-12-13 Control and stabilization device for an aircraft with artificial stability

Publications (1)

Publication Number Publication Date
FR2254481A1 true FR2254481A1 (en) 1975-07-11

Family

ID=5900576

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7440848A Withdrawn FR2254481A1 (en) 1973-12-13 1974-12-11 Aircraft with canards and twin fin tailplane - has stable control afforded by canards anhedrally and fins dihedrally arranged

Country Status (2)

Country Link
FR (1) FR2254481A1 (en)
SE (1) SE7414920L (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0084686A2 (en) * 1982-01-25 1983-08-03 Industrie Aeronautiche e Meccaniche RINALDO Piaggio S.p.A. Improved aircraft
EP0193442A1 (en) * 1985-02-15 1986-09-03 Grumman Aerospace Corporation Automatic camber control
CN109598025A (en) * 2018-11-02 2019-04-09 中国航空工业集团公司西安飞机设计研究所 A kind of rudder-vator inclination angle and area-saving design method
CN110395389A (en) * 2019-06-28 2019-11-01 中国航天空气动力技术研究院 A kind of aerodynamic arrangement improving the horizontal side-coupled characteristic of hypersonic aircraft

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0084686A2 (en) * 1982-01-25 1983-08-03 Industrie Aeronautiche e Meccaniche RINALDO Piaggio S.p.A. Improved aircraft
EP0084686A3 (en) * 1982-01-25 1984-05-30 Piaggio Rinaldo Ind Aeronaut Improved aircraft
EP0193442A1 (en) * 1985-02-15 1986-09-03 Grumman Aerospace Corporation Automatic camber control
CN109598025A (en) * 2018-11-02 2019-04-09 中国航空工业集团公司西安飞机设计研究所 A kind of rudder-vator inclination angle and area-saving design method
CN110395389A (en) * 2019-06-28 2019-11-01 中国航天空气动力技术研究院 A kind of aerodynamic arrangement improving the horizontal side-coupled characteristic of hypersonic aircraft

Also Published As

Publication number Publication date
DE2361888A1 (en) 1975-06-19
DE2361888B2 (en) 1976-06-10
SE7414920L (en) 1975-06-16

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Legal Events

Date Code Title Description
ST Notification of lapse