FR2405869A1 - Procede et installation pour le controle de l'efficacite des surfaces aerodynamiques d'un aeronef - Google Patents

Procede et installation pour le controle de l'efficacite des surfaces aerodynamiques d'un aeronef

Info

Publication number
FR2405869A1
FR2405869A1 FR7731121A FR7731121A FR2405869A1 FR 2405869 A1 FR2405869 A1 FR 2405869A1 FR 7731121 A FR7731121 A FR 7731121A FR 7731121 A FR7731121 A FR 7731121A FR 2405869 A1 FR2405869 A1 FR 2405869A1
Authority
FR
France
Prior art keywords
supersonic
aircraft
canard
stabiliser
disconnected
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.)
Granted
Application number
FR7731121A
Other languages
English (en)
Other versions
FR2405869B1 (fr
Inventor
Philippe Poisson-Quinton
Amedee Bevert
Hung Le Thuy
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.)
Office National dEtudes et de Recherches Aerospatiales ONERA
Original Assignee
Office National dEtudes et de Recherches Aerospatiales ONERA
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 Office National dEtudes et de Recherches Aerospatiales ONERA filed Critical Office National dEtudes et de Recherches Aerospatiales ONERA
Priority to FR7731121A priority Critical patent/FR2405869A1/fr
Publication of FR2405869A1 publication Critical patent/FR2405869A1/fr
Application granted granted Critical
Publication of FR2405869B1 publication Critical patent/FR2405869B1/fr
Granted legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/10—Stabilising surfaces adjustable

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

a. Contrôle de la stabilité des aéronefs en vol à l'aide de surfaces aérodynamiques auxiliaires orientables. b. Les surfaces sont reliées à leurs moyens d'action par l'intermédiaire d'un dispositif réalisant à la demande une condition de couplage ou une condition de débrayage. c. Avions subsoniques, supersoniques et avions laboratoires.
FR7731121A 1977-10-17 1977-10-17 Procede et installation pour le controle de l'efficacite des surfaces aerodynamiques d'un aeronef Granted FR2405869A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR7731121A FR2405869A1 (fr) 1977-10-17 1977-10-17 Procede et installation pour le controle de l'efficacite des surfaces aerodynamiques d'un aeronef

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7731121A FR2405869A1 (fr) 1977-10-17 1977-10-17 Procede et installation pour le controle de l'efficacite des surfaces aerodynamiques d'un aeronef

Publications (2)

Publication Number Publication Date
FR2405869A1 true FR2405869A1 (fr) 1979-05-11
FR2405869B1 FR2405869B1 (fr) 1982-10-29

Family

ID=9196566

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7731121A Granted FR2405869A1 (fr) 1977-10-17 1977-10-17 Procede et installation pour le controle de l'efficacite des surfaces aerodynamiques d'un aeronef

Country Status (1)

Country Link
FR (1) FR2405869A1 (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2449592A1 (fr) * 1979-02-22 1980-09-19 Ver Flugtechnische Werke Avion muni de surfaces de gouverne disposees devant et derriere le centre de gravite
FR2973509A1 (fr) * 2011-03-29 2012-10-05 Airbus Operations Sas Procede et systeme d'interpolation du coefficient d'interaction d'une combinaison de surfaces de controle d'un avion.

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE259357C (fr) *
US2049188A (en) * 1933-09-15 1936-07-28 Alfaro Heraclio Aeroplane
DE654692C (de) * 1935-05-14 1937-12-28 Willy Messerschmitt Dipl Ing Flugzeugsteuerung, deren Zwangslaeufigkeit im Falle der UEberbeanspruchung ausschaltbar ist
US2112757A (en) * 1935-03-03 1938-03-29 Billioque Elie Jean Henri Stabilizing device for aeroplanes
US2681776A (en) * 1950-07-08 1954-06-22 Ben O Howard Floating rudder for aircraft
GB711637A (en) * 1952-01-01 1954-07-07 Jerzy Dabrowski Improvements relating to adjustable stabilisers or tailplanes for aircraft
GB874845A (en) * 1957-03-07 1961-08-10 Hispano Aviacion S A Means for controlling the stability of an aircraft
FR1605011A (fr) * 1967-04-27 1972-08-28

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE259357C (fr) *
US2049188A (en) * 1933-09-15 1936-07-28 Alfaro Heraclio Aeroplane
US2112757A (en) * 1935-03-03 1938-03-29 Billioque Elie Jean Henri Stabilizing device for aeroplanes
DE654692C (de) * 1935-05-14 1937-12-28 Willy Messerschmitt Dipl Ing Flugzeugsteuerung, deren Zwangslaeufigkeit im Falle der UEberbeanspruchung ausschaltbar ist
US2681776A (en) * 1950-07-08 1954-06-22 Ben O Howard Floating rudder for aircraft
GB711637A (en) * 1952-01-01 1954-07-07 Jerzy Dabrowski Improvements relating to adjustable stabilisers or tailplanes for aircraft
GB874845A (en) * 1957-03-07 1961-08-10 Hispano Aviacion S A Means for controlling the stability of an aircraft
FR1605011A (fr) * 1967-04-27 1972-08-28

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2449592A1 (fr) * 1979-02-22 1980-09-19 Ver Flugtechnische Werke Avion muni de surfaces de gouverne disposees devant et derriere le centre de gravite
FR2973509A1 (fr) * 2011-03-29 2012-10-05 Airbus Operations Sas Procede et systeme d'interpolation du coefficient d'interaction d'une combinaison de surfaces de controle d'un avion.

Also Published As

Publication number Publication date
FR2405869B1 (fr) 1982-10-29

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ST Notification of lapse