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ES2055358T3 - Sistema para la elaboracion a bordo de un aeronave de una señal de alarma en caso de anomalia durante el despegue. - Google Patents

Sistema para la elaboracion a bordo de un aeronave de una señal de alarma en caso de anomalia durante el despegue.

Info

Publication number
ES2055358T3
ES2055358T3 ES90401063T ES90401063T ES2055358T3 ES 2055358 T3 ES2055358 T3 ES 2055358T3 ES 90401063 T ES90401063 T ES 90401063T ES 90401063 T ES90401063 T ES 90401063T ES 2055358 T3 ES2055358 T3 ES 2055358T3
Authority
ES
Spain
Prior art keywords
aircraft
real
dat
instant
elements
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 - Lifetime
Application number
ES90401063T
Other languages
English (en)
Inventor
Jean-Louis Bonafe
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 Group SAS
Original Assignee
Airbus Group SAS
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 Airbus Group SAS filed Critical Airbus Group SAS
Application granted granted Critical
Publication of ES2055358T3 publication Critical patent/ES2055358T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • G05D1/0083—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots to help an aircraft pilot in the rolling phase

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)
  • Emergency Alarm Devices (AREA)
  • Radar Systems Or Details Thereof (AREA)

Abstract

EL PRESENTE INVENTO SE REFIERE A UN SISTEMA PARA LA ELABORACION A BORDE DE UNA AERONAVE DE UNA SEÑAL DE ALARMA EN CASO DE ANOMALIA DURANTE EL DESPEGUE. SEGUN EL INVENTO, CONSTA DE: - UNOS ELEMENTOS (1,2) QUE PUEDEN SUMINISTRAR SEÑALES REPRESENTATIVAS DE LA ACELERACION TEORICA Y DE LA ACELERACION REAL, EN UN INSTANTE DADO, DE LA AERONAVE; - UNOS ELEMENTOS (7) PARA CALCULAR LA EXPRESION: D1 = D1T + (VAT (AL CUADRADO) - V11 2Y1T, EN LA CUAL: . Y1T ES LA ACELERACION REAL, EN EL INSTANTE T, DE LA AERONAVE, . V11T ES SU VELOCIDAD REAL, . VAT ES SU VELOCIDAD TEORICA, . D1T ES LA DISTANCIA REAL RECORRIDA, EN EL INSTANTE T, POR LA AERONAVE, Y . D1 ES LA DISTANCIA REAL PREVISTA RECORRIDA POR LA AERONAVE CUANDO V11T SEA IGUAL A VAT, ASI COMO LA RELACION: D1/DAT EN LA QUE DAT ES LA DISTANCIA TEORICA RECORRIDA, EN EL INSTANTE T, POR LA AERONAVE; - UNOS ELEMENTOS (11) PARA COMPARAR LA RELACION D1/DAT CON UN UMBRAL PREDETERMINADO S QUE GARANTIZA UNA DISTANCIA MINIMA DE SEGURIDAD PARA EL FRENADO Y LA DETENCION DE LA AERONAVE, Y SUMINISTRAR UNA SEÑAL DE INFORMACION A UNOS ELEMENTOS DE ALARMA (13) QUE PUEDEN EMITIR UNA SEÑAL DE ALARMA CUANDO DICHA RELACION D1/DAT ES SUPERIOR O IGUAL A DICHO UMBRAL.
ES90401063T 1989-06-20 1990-04-19 Sistema para la elaboracion a bordo de un aeronave de una señal de alarma en caso de anomalia durante el despegue. Expired - Lifetime ES2055358T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8908177A FR2650101B1 (fr) 1989-06-20 1989-06-20 Systeme pour l'elaboration a bord d'un aeronef d'un signal d'information pendant le decollage avec alerte ou alarme en cas d'anomalie

Publications (1)

Publication Number Publication Date
ES2055358T3 true ES2055358T3 (es) 1994-08-16

Family

ID=9382925

Family Applications (1)

Application Number Title Priority Date Filing Date
ES90401063T Expired - Lifetime ES2055358T3 (es) 1989-06-20 1990-04-19 Sistema para la elaboracion a bordo de un aeronave de una señal de alarma en caso de anomalia durante el despegue.

Country Status (5)

Country Link
US (1) US5124700A (es)
EP (1) EP0404606B1 (es)
DE (1) DE69008933T2 (es)
ES (1) ES2055358T3 (es)
FR (1) FR2650101B1 (es)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5372039A (en) * 1993-08-20 1994-12-13 Weatherwise, Inc. Apparatus and method for determining geostrophic wind velocity
FR2725063B1 (fr) * 1994-09-28 1997-01-10 Aerospatiale Systeme pour l'elaboration a bord d'un aeronef d'un signal d'information, alerte ou alarme en cas d'anomalie pendant le decollage
CA2202409C (en) 1997-04-11 1998-04-07 Carl W. Millard Howgozit airspeed indicator system
US6133857A (en) * 1997-04-14 2000-10-17 Millard; Wayne C. Aircraft takeoff velocity indicator system
GB2375748B (en) * 2001-05-24 2003-06-18 Univ Cranfield A method and system for monitoring the performance of an aircraft during the take-off manoeuvre
US7518341B2 (en) * 2004-12-23 2009-04-14 Dell Product L.P. Method for verifying smart battery failures by measuring input charging voltage and associated systems
FR2894046B1 (fr) * 2005-11-28 2008-02-15 Airbus France Sas Procede de detection d'une erreur d'entree d'un des parametres de decollage dans un systeme de management de vol
US20110118909A1 (en) * 2009-11-19 2011-05-19 Honeywell International Inc. Systems and methods of detecting low takeoff performance due to incorrect weight information
US10315777B2 (en) 2011-12-22 2019-06-11 Embraer S.A. Safe takeoff monitoring system
US10815000B2 (en) 2016-05-31 2020-10-27 Embraer S.A. Short rejected takeoff system and method
US10429856B2 (en) 2017-09-07 2019-10-01 Embraer S.A. Safe takeoff system
FR3145217A1 (fr) 2023-01-25 2024-07-26 Airbus Operations Systeme pour generer un signal d'anomalie au decollage a bord d’un d'aeronef

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3034096A (en) * 1956-10-01 1962-05-08 Sperry Rand Corp Take-off monitoring apparatus for aircraft
US3504335A (en) * 1967-08-14 1970-03-31 Massachusetts Inst Technology Aircraft take-off monitoring system
US4122522A (en) * 1974-05-20 1978-10-24 Smith Gerald R Aircraft ground monitoring system
GB1602477A (en) * 1978-05-31 1981-11-11 Compania De Transport Aerian T Take-off director system
US4251868A (en) * 1978-09-15 1981-02-17 Compania De Transport Aerian Tarom Take-off director system
EP0025614A1 (en) * 1979-07-23 1981-03-25 The Boeing Company Method and apparatus for continuously determining an interval of time during which an action must be taken
EP0156911A4 (en) * 1983-09-12 1987-02-19 Robert C Scott TRACK CRITICAL MARGIN WARNING SYSTEM.
US4638437A (en) * 1984-06-25 1987-01-20 The Boeing Company Aircraft performance margin indicator
US4773015A (en) * 1985-02-06 1988-09-20 Accutold Method and apparatus for onboard monitoring of aircraft takeoff

Also Published As

Publication number Publication date
FR2650101B1 (fr) 1991-12-20
DE69008933D1 (de) 1994-06-23
US5124700A (en) 1992-06-23
EP0404606A1 (fr) 1990-12-27
FR2650101A1 (fr) 1991-01-25
EP0404606B1 (fr) 1994-05-18
DE69008933T2 (de) 1994-09-29

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