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Withdrawn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
English (en)
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/de
Application filed by Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of FR2254481A1 publication Critical patent/FR2254481A1/fr
Withdrawn legal-status Critical Current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)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Mechanical Control Devices (AREA)
  • Toys (AREA)
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with canards and twin fin tailplane - has stable control afforded by canards anhedrally and fins dihedrally arranged Withdrawn FR2254481A1 (en)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 (de) 1973-12-13 Steuer- und Stabilisierungseinrichtung für ein Flugzeug künstlicher Stabilität

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 (enrdf_load_html_response)
SE (1) SE7414920L (enrdf_load_html_response)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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 (zh) * 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 一种v形尾翼倾角与面积优化设计方法
CN110395389A (zh) * 2019-06-28 2019-11-01 中国航天空气动力技术研究院 一种改善高超声速飞行器横侧向耦合特性的气动布局

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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 (zh) * 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 一种v形尾翼倾角与面积优化设计方法
CN110395389A (zh) * 2019-06-28 2019-11-01 中国航天空气动力技术研究院 一种改善高超声速飞行器横侧向耦合特性的气动布局

Also Published As

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

Similar Documents

Publication Publication Date Title
US4466586A (en) Directional control device for aircraft
NO145314C (no) Mateanordning for roer eller liknende, saerlig en roerstreng som skal inn eller ut av en broenn
GB1153747A (en) Toy Airplane with Folding Wings
FR2254481A1 (en) Aircraft with canards and twin fin tailplane - has stable control afforded by canards anhedrally and fins dihedrally arranged
US3370810A (en) Stall control device for swept wings
GB1024103A (en) Aircraft with flexible wings
GB1086044A (en) Kites
GB1100376A (en) Improvements in aircraft
US1767966A (en) Wing system with stabilizing vanes for aircraft
GB987792A (en) Improvements in and relating to aircraft wings
GB425645A (en) Improvements in or relating to aircraft
Spearman et al. Some effects of aircraft configuration on static longitudinal and directional stability characteristics at supersonic Mach numbers below 3
GB834532A (en) Improvements in or relating to wings and other main support aerofoils in aircraft
NELMS Aerodynamic characteristics of an all-body hypersonic aircraft configuration at Mach numbers from 0. 65 to 10. 6(Aerodynamic characteristics of wind tunnel model of hypersonic aircraft)
GB1220055A (en) Fixed wing aeroplanes
GB595464A (en) Improvements in aeroplanes
GB628684A (en) Improvements in aircraft control surfaces
GB741720A (en) Improvements in aeroplanes
SMITH Effect of wing aspect ratio and flap span on aerodynamic characteristics of an externally blown jet-flap STOL model(Effect of wing aspect ratio and flap span on aerodynamic characteristics of short takeoff model with externally blown jet flap)
Staudacher et al. Aerodynamic characteristics of a fighter-type configuration during and beyond stall
Menees et al. An Experimental Investigation of the Effect of a Canard Control on the Lift, Drag, and Pitching Moment of an Aspect-Ratio 2.0 Triangular Wing Incorporating a Form of Conical Camber
GB791423A (en) High-lift airplane with all-moving tail plane
GB1417653A (en) Aircraft
CZARNECKI Spanwise loadings and aerodynamic characteristics for a series of trailing- edge controls on a 40 deg sweptback wing at Mach numbers of 1. 61 and 2. 01(Spanwise loadings and aerodynamic characteristics for trailing-edge controls on 40 deg sweptback wing at Mach numbers 1. 61 and 2. 01)
FR2272893A1 (en) Powered aircraft with small front wing - has freely rotating tabs on front wing forming elevators

Legal Events

Date Code Title Description
ST Notification of lapse