FR2425380A1 - Installation de commande automatique pour avion a decollage et atterrissage courts (adac) - Google Patents

Installation de commande automatique pour avion a decollage et atterrissage courts (adac)

Info

Publication number
FR2425380A1
FR2425380A1 FR7814024A FR7814024A FR2425380A1 FR 2425380 A1 FR2425380 A1 FR 2425380A1 FR 7814024 A FR7814024 A FR 7814024A FR 7814024 A FR7814024 A FR 7814024A FR 2425380 A1 FR2425380 A1 FR 2425380A1
Authority
FR
France
Prior art keywords
engine
surface blown
aircraft
flap
utilise
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
FR7814024A
Other languages
English (en)
Other versions
FR2425380B3 (fr
Inventor
Fred Wilson May
Robert Edward Spitzer
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.)
Boeing Co
Original Assignee
Boeing Co
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 Boeing Co filed Critical Boeing Co
Priority to FR7814024A priority Critical patent/FR2425380A1/fr
Publication of FR2425380A1 publication Critical patent/FR2425380A1/fr
Application granted granted Critical
Publication of FR2425380B3 publication Critical patent/FR2425380B3/fr
Granted legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
    • G05D1/0072—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements to counteract a motor failure

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Force Measurement Appropriate To Specific Purposes (AREA)

Abstract

PROCEDE DE RECONFIGURATION AUTOMATIQUE DES GOUVERNES D'UN AVION ADAC A PLUSIEURS MOTEURS LORSQUE L'UN DES MOTEURS FONCTIONNE MAL ET QUE L'AVION EXECUTE UNE MANOEUVRE DE DECOLLAGE OU D'ATTERRISSAGE COURT, LES MOTEURS ETANT MONTES SUR LES AILES DE L'AVION ET CHAQUE MOTEUR FOURNISSANT UN COURANT D'ECHAPPEMENT A UN VOLET DEPLOYABLE D'AUGMENTATION DE PORTANCE COMPORTANT UN MOYEN POUR OUVRIR UNE OU DES FENTES TRANSVERSALES 36 EN REPONSE A UN SIGNAL PREDETERMINE. LE PROCEDE CONSISTE A DETECTER CELUI DES MOTEURS 12 OU 14 QUI FONCTIONNE MAL, A DEPLOYER AUTOMATIQUEMENT LE VOLET D'AUGMENTATION DE PORTANCE 24 OU 26 DE LA MEME FACON QUE LES VOLETS A FENTES CLASSIQUES 28, 30, A FOURNIR LEDIT SIGNAL POUR OUVRIR LA OU LES FENTES TRANSVERSALES, ET A ESCAMOTER AUTOMATIQUEMENT TOUS LES VOLETS A FENTES DE L'AILE 16 DONT LE MOTEUR 12 FONCTIONNE DE FACON A CONTRECARRER LE MOMENT DE ROULIS PROVOQUE.
FR7814024A 1978-05-11 1978-05-11 Installation de commande automatique pour avion a decollage et atterrissage courts (adac) Granted FR2425380A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR7814024A FR2425380A1 (fr) 1978-05-11 1978-05-11 Installation de commande automatique pour avion a decollage et atterrissage courts (adac)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7814024A FR2425380A1 (fr) 1978-05-11 1978-05-11 Installation de commande automatique pour avion a decollage et atterrissage courts (adac)

Publications (2)

Publication Number Publication Date
FR2425380A1 true FR2425380A1 (fr) 1979-12-07
FR2425380B3 FR2425380B3 (fr) 1981-01-23

Family

ID=9208146

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7814024A Granted FR2425380A1 (fr) 1978-05-11 1978-05-11 Installation de commande automatique pour avion a decollage et atterrissage courts (adac)

Country Status (1)

Country Link
FR (1) FR2425380A1 (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2817535A1 (fr) 2000-12-06 2002-06-07 Eads Airbus Sa Systeme pour commander automatiquement des dispositifs hypersustentateurs d'un aeronef durant le decollage
EP1498794A1 (fr) * 2003-07-15 2005-01-19 Airbus France Système pour commander automatiquement des dispositif hypersustentateurs d'un aéronef, en particulier des becs de bord d'attaque d'aile

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2817535A1 (fr) 2000-12-06 2002-06-07 Eads Airbus Sa Systeme pour commander automatiquement des dispositifs hypersustentateurs d'un aeronef durant le decollage
EP1223491A1 (fr) * 2000-12-06 2002-07-17 Airbus France Système pour commander automatiquement des dispositifs hypersustentateurs d'un aéronef durant le décollage
US6643568B2 (en) 2000-12-06 2003-11-04 Airbus France System for automatically controlling lift-augmentation devices of an aircraft during take-off
EP1498794A1 (fr) * 2003-07-15 2005-01-19 Airbus France Système pour commander automatiquement des dispositif hypersustentateurs d'un aéronef, en particulier des becs de bord d'attaque d'aile
FR2857760A1 (fr) * 2003-07-15 2005-01-21 Airbus France Systeme pour commander automatiquement des dispositifs hypersustentateurs d'un aeronef, en particulier des becs de bord d'attaque d'aile.
US7366592B2 (en) 2003-07-15 2008-04-29 Airbus France System for automatically controlling lift-enhancing devices of an aircraft, in particular wing leading edge slats

Also Published As

Publication number Publication date
FR2425380B3 (fr) 1981-01-23

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