DE602005000097D1 - Flugzeugstartverfahren - Google Patents

Flugzeugstartverfahren

Info

Publication number
DE602005000097D1
DE602005000097D1 DE602005000097T DE602005000097T DE602005000097D1 DE 602005000097 D1 DE602005000097 D1 DE 602005000097D1 DE 602005000097 T DE602005000097 T DE 602005000097T DE 602005000097 T DE602005000097 T DE 602005000097T DE 602005000097 D1 DE602005000097 D1 DE 602005000097D1
Authority
DE
Germany
Prior art keywords
procedures
aircraft take
aircraft
function
speed
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.)
Active
Application number
DE602005000097T
Other languages
English (en)
Other versions
DE602005000097T2 (de
Inventor
Franck Delaplace
Gerard Mathieu
Nicolas Daniel
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 Operations SAS
Original Assignee
Airbus Operations 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 Operations SAS filed Critical Airbus Operations SAS
Publication of DE602005000097D1 publication Critical patent/DE602005000097D1/de
Application granted granted Critical
Publication of DE602005000097T2 publication Critical patent/DE602005000097T2/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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)
  • Automation & Control Theory (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Consolidation Of Soil By Introduction Of Solidifying Substances Into Soil (AREA)
  • Steering Controls (AREA)
  • Macromonomer-Based Addition Polymer (AREA)
  • Toys (AREA)
  • Traffic Control Systems (AREA)
  • Constituent Portions Of Griding Lathes, Driving, Sensing And Control (AREA)
DE602005000097T 2004-04-28 2005-03-29 Flugzeugstartverfahren Active DE602005000097T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0404494 2004-04-28
FR0404494A FR2869588B1 (fr) 2004-04-28 2004-04-28 Procede d'aide au decollage d'un aeronef.

Publications (2)

Publication Number Publication Date
DE602005000097D1 true DE602005000097D1 (de) 2006-10-12
DE602005000097T2 DE602005000097T2 (de) 2007-02-01

Family

ID=34942042

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602005000097T Active DE602005000097T2 (de) 2004-04-28 2005-03-29 Flugzeugstartverfahren

Country Status (7)

Country Link
US (1) US7281683B2 (de)
EP (1) EP1591854B1 (de)
AT (1) ATE338295T1 (de)
CA (1) CA2502145C (de)
DE (1) DE602005000097T2 (de)
ES (1) ES2270408T3 (de)
FR (1) FR2869588B1 (de)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2885706B1 (fr) * 2005-05-10 2007-06-15 Airbus France Sas Procede d'aide au decollage d'un aeronef.
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
FR2893909B1 (fr) * 2005-11-29 2007-12-21 Airbus France Sas Procede pour assurer la securite d'un aeronef volant horizontalement a faible vitesse.
DE102007012425A1 (de) * 2007-03-15 2008-09-18 Airbus Deutschland Gmbh Verfahren und Einrichtung zur Höhenflossentrimmung bei einem Flugzeug
FR2950165B1 (fr) * 2009-09-16 2012-08-17 Airbus Operations Sas Procede et systeme pour l'amelioration des performances d'un aeronef au decollage
US8793040B2 (en) * 2011-06-10 2014-07-29 Embraer S.A. Climb-optimized auto takeoff system
US9164505B1 (en) 2012-05-22 2015-10-20 The Boeing Company Automatic rejected takeoff system
US9821903B2 (en) * 2014-07-14 2017-11-21 The Boeing Company Closed loop control of aircraft control surfaces
US10464668B2 (en) 2015-09-02 2019-11-05 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles
US11001378B2 (en) 2016-08-08 2021-05-11 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles
AU2016338383A1 (en) 2015-09-02 2018-03-22 Jetoptera, Inc. Fluidic propulsive system
CN109070996A (zh) * 2016-04-25 2018-12-21 庞巴迪公司 具有电传动升降舵的飞行器俯仰控制系统
US11453483B2 (en) 2016-06-30 2022-09-27 Blended Wing Aircraft, Inc. Aircraft for commercial air travel and a method of manufacture
US10150558B2 (en) 2016-06-30 2018-12-11 DZYNE Technologies Incorporated Tilting landing gear systems and methods
US11226639B2 (en) 2016-09-23 2022-01-18 Yaborã Indústria Aeronáutica S.A. Enhanced take-off system
CA3068569A1 (en) 2017-06-27 2019-01-03 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles
CA2972498C (en) 2017-06-28 2024-01-23 Bombardier Inc. Takeoff pitch guidance system and method
US10816998B2 (en) * 2017-09-18 2020-10-27 The Boeing Company Airplane takeoff trims utilizing both stabilizers and elevators
WO2020142457A1 (en) * 2018-12-31 2020-07-09 DZYNE Technologies Incorporated Tilting landing gear systems and methods

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3138353A (en) * 1962-03-21 1964-06-23 Boeing Co Method and apparatus for preventing complete stalls of an aircraft at slow speeds
US3691356A (en) * 1970-12-10 1972-09-12 Sperry Rand Corp Speed command and throttle control system for aircraft
US3949958A (en) * 1973-12-07 1976-04-13 Lockheed Aircraft Corporation Pitch control system
US4043523A (en) * 1976-03-11 1977-08-23 Ball Brothers Research Corporation Apparatus for aircraft pitch trim
US4099687A (en) * 1976-07-22 1978-07-11 Roberts Lawrence T All-axis control of aircraft in deep stall
US4261533A (en) * 1978-06-26 1981-04-14 Dynamic Engineering, Inc. All-axis control of aircraft in ultra deep stall
US4908619A (en) * 1984-11-13 1990-03-13 The Boeing Company Aircraft stall warning system
FR2806791B1 (fr) * 2000-03-23 2002-05-31 Aerospatiale Matra Airbus Procede pour determiner une vitesse minimale de controle d'un aeronef
FR2817535B1 (fr) * 2000-12-06 2003-03-21 Eads Airbus Sa Systeme pour commander automatiquement des dispositifs hypersustentateurs d'un aeronef durant le decollage
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
FR2826469B1 (fr) * 2001-06-25 2003-10-24 Eads Airbus Sa Procede et dispositif pour commander au moins une surface aerodynamique de profondeur d'un avion lors d'un decollage

Also Published As

Publication number Publication date
ATE338295T1 (de) 2006-09-15
US7281683B2 (en) 2007-10-16
CA2502145C (fr) 2012-01-03
DE602005000097T2 (de) 2007-02-01
FR2869588A1 (fr) 2005-11-04
ES2270408T3 (es) 2007-04-01
US20050242235A1 (en) 2005-11-03
CA2502145A1 (fr) 2005-10-28
EP1591854B1 (de) 2006-08-30
FR2869588B1 (fr) 2006-07-14
EP1591854A1 (de) 2005-11-02

Similar Documents

Publication Publication Date Title
DE602005000097D1 (de) Flugzeugstartverfahren
JP2019172258A5 (de)
FR2885706B1 (fr) Procede d'aide au decollage d'un aeronef.
NZ761084A (en) Decoupled hand controls for aircraft with vertical takeoff and landing and forward flight capabilities
ES2485824T3 (es) Una peonza de juguete
EP2772817A3 (de) Formationsflugsteuerung
WO2008048206A3 (en) Cf bearing with steady pitching moment
EP2116811A3 (de) Flugführungs- und Navigationsanzeige für einen Helikopter
ATE430352T1 (de) Gleitanflugverfahren für maximale vorhersagbarkeit
GB201117340D0 (en) Flat support
BRPI0911484A2 (pt) asa de sustentação para uma aeronave
WO2007080314A3 (fr) Systeme de pilotage d'un aeronef
BR112012005693A2 (pt) aparelho com capacidade propulsora com capacidade de mudança de tamanho ativa
WO2011048064A3 (en) Aircraft horizontal stabiliser fitted with leading-edge strake
ES2156660A1 (es) Mandos de vuelo con compensacion automatica.
GB201020410D0 (en) An air intake system for an air vehicle
WO2010139680A3 (de) Verfahren zur herstellung wasserabsorbierender polymerpartikel
FR2933956B1 (fr) Dispositif pour ceinturer une nacelle d'aeronef
FR2870607B1 (fr) Procede et dispositif pour construire une trajectoire de vol a basse altitude destinee a etre suivie par un aeronef
DE602008003754D1 (de) Aufblasbarer delta-traktions-drachen
WO2006057575A3 (fr) Avion a fuselage porteur
ES1140161U (es) Dispositivo aéreo remoto para medición de variables ambientales en espacios cerrados
EP4078018A4 (de) Traverse mit integrierter verdrahtung
RU2016150540A (ru) Система лопастей несущего винта
WO2010115815A3 (de) Flügel eines flugzeugs oder eines raumfahrzeugs mit einem beweglichen strömungskörper

Legal Events

Date Code Title Description
8364 No opposition during term of opposition
R082 Change of representative

Ref document number: 1591854

Country of ref document: EP

Representative=s name: MEISSNER & MEISSNER, 14199 BERLIN, DE