ES8504593A1 - Procedimiento y dispositivo para el mando del frenado de una aeronave en el momento del aterrizaje. - Google Patents

Procedimiento y dispositivo para el mando del frenado de una aeronave en el momento del aterrizaje.

Info

Publication number
ES8504593A1
ES8504593A1 ES530357A ES530357A ES8504593A1 ES 8504593 A1 ES8504593 A1 ES 8504593A1 ES 530357 A ES530357 A ES 530357A ES 530357 A ES530357 A ES 530357A ES 8504593 A1 ES8504593 A1 ES 8504593A1
Authority
ES
Spain
Prior art keywords
nose
phase
landing gear
braking system
ground contact
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.)
Expired
Application number
ES530357A
Other languages
English (en)
Other versions
ES530357A0 (es
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.)
Messier Hispano SA
Safran Landing Systems SAS
Original Assignee
Messier Bugatti SA
Messier Hispano SA
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 Messier Bugatti SA, Messier Hispano SA filed Critical Messier Bugatti SA
Publication of ES8504593A1 publication Critical patent/ES8504593A1/es
Publication of ES530357A0 publication Critical patent/ES530357A0/es
Granted legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/42—Arrangement or adaptation of brakes
    • B64C25/426—Braking devices providing an automatic sequence of braking

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Regulating Braking Force (AREA)
  • Braking Systems And Boosters (AREA)

Abstract

PROCEDIMIENTO Y DISPOSITIVO PARA EL MANDO DEL FRENADO DE UNA AERONAVE EN EL MOMENTO DEL ATERRIZAJE.COMPRENDE: A) DETERMINAR EL VALOR DEL ANGULO DE INCLINACION BDB DE LA AERONAVE (1), A PARTIR DEL MOMENTO EN QUE TOMA CONTACTO CON LA PISTA, CON LOS ELEMENTOS DE RODADURA (6) DE LOS ATERRIZADORES PRINCIPALES (7); B) ELABORAR UNA SEN/AL REPRESENTATIVA DEL VALOR DEL ANGULO DE INCLINACION; Y C) GOBERNAR EL FRENADO DE LA AERONAVE EN FUNCION DE UN VALOR REPRESENTATIVO DE LA SEN/AL, PARA OBTENER UNA VARIACION DEL ANGULO DE INCLINACION ACEPTABLE. CONSTA DE DISPOSITIVOS (10) CONSTITUIDOS POR UNA CENTRAL DE INERCIA DE TIPO MECANICO O CON LASER; AMPLIFICADORES (13) Y RECEPTORES DE LAS SEN/ALES DE INFORMACION DE LA CENTRAL DE INERCIA; Y ELEMENTOS (16, 28, 18, 22) CON FRENOS DE DISCO (22) Y/O AEROFRENOS.
ES530357A 1983-03-08 1984-03-07 Procedimiento y dispositivo para el mando del frenado de una aeronave en el momento del aterrizaje. Granted ES530357A0 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8303750A FR2542277B1 (fr) 1983-03-08 1983-03-08 Procede et dispositif de commande du freinage d'un aeronef lors de l'atterrissage des qu'il a pris contact avec le sol d'une piste par ses trains d'atterrissage principaux et quand le train avant n'a pas encore pris contact avec le sol

Publications (2)

Publication Number Publication Date
ES8504593A1 true ES8504593A1 (es) 1985-04-16
ES530357A0 ES530357A0 (es) 1985-04-16

Family

ID=9286598

Family Applications (1)

Application Number Title Priority Date Filing Date
ES530357A Granted ES530357A0 (es) 1983-03-08 1984-03-07 Procedimiento y dispositivo para el mando del frenado de una aeronave en el momento del aterrizaje.

Country Status (6)

Country Link
US (1) US4580744A (es)
EP (1) EP0122162A1 (es)
BR (1) BR8400969A (es)
CA (1) CA1208744A (es)
ES (1) ES530357A0 (es)
FR (1) FR2542277B1 (es)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4923056A (en) * 1989-02-21 1990-05-08 Aircraft Braking Systems Corporation Method of increasing the service life of aircraft carbon disk brakes
US5968106A (en) * 1997-08-05 1999-10-19 The Boeing Company Aircraft stop-to-position autobrake control system
GB0129300D0 (en) * 2001-12-07 2002-01-23 Bae Systems Plc Method of landing an aircraft and apparatus therefor
FR2869014B1 (fr) * 2004-04-19 2006-07-07 Messier Bugatti Sa Procede de freinage d'un aeronef a plusieurs roues freinees
FR2877312B1 (fr) * 2004-11-02 2007-01-12 Airbus France Sas Procede et dispositif pour ameliorer l'efficacite de freinage d'un aeronef roulant sur le sol
FR2929242B1 (fr) * 2008-03-25 2010-06-11 Airbus France Procede de freinage ameliore pour un avion
FR2959483B1 (fr) * 2010-04-28 2012-06-01 Messier Bugatti Procede de gestion d'une liaison au sol d'un aeronef.

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2854098A (en) * 1955-12-08 1958-09-30 Lambert & Brake Corp Combined wheel and disc brake assembly and actuator means therefor
US4076331A (en) * 1973-09-06 1978-02-28 The Boeing Company Aircraft automatic braking system
US3881783A (en) * 1974-02-08 1975-05-06 Ron Benjamin Fixed slip hydraulic anti-lock braking system
US4326755A (en) * 1979-05-11 1982-04-27 Goodyear Aerospace Corporation Deceleration control circuit
DE3231162C2 (de) * 1982-08-21 1984-08-16 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Verfahren für das beschleunigte Herbeiführen des Bodenkontaktes von Flugzeugen

Also Published As

Publication number Publication date
FR2542277A1 (fr) 1984-09-14
BR8400969A (pt) 1984-10-16
FR2542277B1 (fr) 1985-06-28
CA1208744A (fr) 1986-07-29
EP0122162A1 (fr) 1984-10-17
ES530357A0 (es) 1985-04-16
US4580744A (en) 1986-04-08

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