FR2756256B1 - Indicateur de marge de puissance pour un aeronef a voilure tournante, notamment un helicoptere - Google Patents

Indicateur de marge de puissance pour un aeronef a voilure tournante, notamment un helicoptere

Info

Publication number
FR2756256B1
FR2756256B1 FR9614443A FR9614443A FR2756256B1 FR 2756256 B1 FR2756256 B1 FR 2756256B1 FR 9614443 A FR9614443 A FR 9614443A FR 9614443 A FR9614443 A FR 9614443A FR 2756256 B1 FR2756256 B1 FR 2756256B1
Authority
FR
France
Prior art keywords
helicopter
wing aircraft
power margin
margin indicator
turn wing
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 - Fee Related
Application number
FR9614443A
Other languages
English (en)
Other versions
FR2756256A1 (fr
Inventor
Olivier Bosqui
Raymond Jacques Gerard Berlioz
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 Helicopters SAS
Original Assignee
Eurocopter France 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 Eurocopter France SA filed Critical Eurocopter France SA
Priority to FR9614443A priority Critical patent/FR2756256B1/fr
Priority to US08/977,610 priority patent/US6195598B1/en
Publication of FR2756256A1 publication Critical patent/FR2756256A1/fr
Application granted granted Critical
Publication of FR2756256B1 publication Critical patent/FR2756256B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D43/00—Arrangements or adaptations of instruments
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01D—MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE; ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVERED IN A SINGLE OTHER SUBCLASS; TARIFF METERING APPARATUS; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR
    • G01D7/00—Indicating measured values
    • G01D7/02—Indicating value of two or more variables simultaneously
    • G01D7/04—Indicating value of two or more variables simultaneously using a separate indicating element for each variable

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Turbines (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
FR9614443A 1996-11-26 1996-11-26 Indicateur de marge de puissance pour un aeronef a voilure tournante, notamment un helicoptere Expired - Fee Related FR2756256B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR9614443A FR2756256B1 (fr) 1996-11-26 1996-11-26 Indicateur de marge de puissance pour un aeronef a voilure tournante, notamment un helicoptere
US08/977,610 US6195598B1 (en) 1996-11-26 1997-11-25 Power margin indicator for a rotary-wing aircraft, especially a helicopter

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9614443A FR2756256B1 (fr) 1996-11-26 1996-11-26 Indicateur de marge de puissance pour un aeronef a voilure tournante, notamment un helicoptere

Publications (2)

Publication Number Publication Date
FR2756256A1 FR2756256A1 (fr) 1998-05-29
FR2756256B1 true FR2756256B1 (fr) 1999-01-22

Family

ID=9498020

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9614443A Expired - Fee Related FR2756256B1 (fr) 1996-11-26 1996-11-26 Indicateur de marge de puissance pour un aeronef a voilure tournante, notamment un helicoptere

Country Status (2)

Country Link
US (1) US6195598B1 (fr)
FR (1) FR2756256B1 (fr)

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6332105B1 (en) * 1999-05-21 2001-12-18 Georgia Tech Research Corporation Neural network based automatic limit prediction and avoidance system and method
FR2809082B1 (fr) 2000-05-17 2002-09-20 Eurocopter France Indicateur de marge de puissance pour un aeronef a voilure tournante, notamment un helicoptere
US7212942B2 (en) * 2003-06-10 2007-05-01 Precision Innovations Llc Power available and limitation indicator for use with an aircraft engine
ITTO20040050A1 (it) 2004-02-03 2004-05-03 Agusta Spa Dispositivo indicatore di un margine di potenza residua di motori a turbina di velivoli
US7414544B2 (en) * 2005-01-28 2008-08-19 Bell Helicopter Textron, Inc. Power situation indicator
FR2932919B1 (fr) * 2008-06-24 2010-08-20 Eurocopter France Adaptation d'alertes de terrain selectives, en fonction la manoeuvrabilite instantanee d'un giravion
US7801695B2 (en) * 2008-12-23 2010-09-21 Honeywell International Inc. Operations support systems and methods with model-based torque estimates
US8321118B2 (en) * 2008-12-23 2012-11-27 Honeywell International Inc. Operations support systems and methods with power assurance
US8417410B2 (en) * 2008-12-23 2013-04-09 Honeywell International Inc. Operations support systems and methods with power management
US20100161196A1 (en) * 2008-12-23 2010-06-24 Honeywell International Inc. Operations support systems and methods with engine diagnostics
US9272778B2 (en) 2009-06-04 2016-03-01 Airbus Helicopters Device for assisting in piloting hybrid helicopter, hybrid helicopter provided with such device, and method implemented by such device
FR2946322B1 (fr) 2009-06-04 2011-06-17 Eurocopter France Dispositif d'aide au pilotage d'un helicoptere hybride, helicoptere hybride muni d'un tel dispositif et procede mis en oeuvre par ledit dispositif
FR2973340B1 (fr) 2011-03-30 2013-04-12 Eurocopter France Procede, dispositif d'aide au pilotage d'un aeronef, et aeronef
FR2989796B1 (fr) * 2012-04-20 2014-04-11 Eurocopter France Instrument de secours pour aeronef combinant des informations de vol, une information de marge de puissance et une assistance au pilotage
US8881297B2 (en) 2012-09-06 2014-11-04 Brooks Automation, Inc. Access arbitration module and system for semiconductor fabrication equipment and methods for using and operating the same
US9409655B1 (en) 2015-01-28 2016-08-09 Airbus Helicopters Flight instrument displaying a variable rotational speed of a main rotor of an aircraft
FR3033316B1 (fr) 2015-03-04 2018-04-06 Airbus Helicopters Procede et dispositif de determination et d'optimisation de parametres caracteristiques du fonctionnement d'un aeronef a voilure tournante
FR3037923B1 (fr) 2015-06-23 2018-05-04 Airbus Helicopters Procede de regulation d'une installation motrice trimoteur pour un aeronef a voilure tournante
US9950805B2 (en) * 2015-10-26 2018-04-24 The Boeing Company Aircraft engine fan speed display improvements for enhanced monitoring and thrust setting ability
FR3051772B1 (fr) 2016-05-30 2019-08-23 Airbus Helicopters Procede, dispositif d'aide au pilotage d'un aeronef, et aeronef
FR3053314B1 (fr) * 2016-07-01 2018-07-27 Airbus Helicopters Dispositif indicateur de marge de puissance pour giravion, giravion associe et procede correspondant
US10173787B1 (en) 2018-02-12 2019-01-08 Bell Helicopter Textron Inc. Rotor speed indication systems for rotorcraft
FR3081597B1 (fr) * 2018-05-24 2021-07-30 Airbus Helicopters Procede et dispositif de determination et d'affichage d'une distance de securite d'un giravion en prenant en compte la hauteur des vagues
FR3084057B1 (fr) 2018-07-17 2020-06-19 Airbus Helicopters Procede et dispositif de determination predictive de parametres caractaristiques du fonctionnement d'un aeronef a voilure tournante pour la realisation d'une manoeuvre predeterminee
FR3086274B1 (fr) 2018-09-26 2021-03-12 Airbus Helicopters Procede et dispositif d'aide au pilotage d'un giravion hydride muni d'un rotor de sustentation et d'au moins un rotor propulsif generant une poussee
FR3097527B1 (fr) * 2019-06-20 2021-06-18 Airbus Helicopters Procédé d’aide au pilotage d’un giravion hybride muni d’un rotor de sustentation et d’au moins un rotor propulsif à hélice générant une poussée
FR3124165A1 (fr) 2021-06-17 2022-12-23 Airbus Helicopters Procédé et dispositif d’aide au pilotage d’un giravion muni d’au moins une hélice
FR3134564A1 (fr) 2022-04-15 2023-10-20 Airbus Helicopters Procédé et système d'aide au pilotage d'un aéronef, aéronef équipé d’un tel système.

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4034605A (en) * 1975-09-26 1977-07-12 Pacer Systems Inc. Maneuver margin presenting
US4736331A (en) * 1982-05-26 1988-04-05 United Technologies Corporation Helicopter power available to hover indicator
US5050081A (en) * 1988-11-14 1991-09-17 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Method and system for monitoring and displaying engine performance parameters
FR2710026B1 (fr) 1993-09-17 1995-12-08 Aerospatiale Dispositif de surveillance du système propulsif d'un aéronef.
FR2731069B1 (fr) * 1995-02-23 1997-04-30 Pelletier Patrick Dispositif d'aide au pilotage
FR2749546B1 (fr) * 1996-06-07 1998-08-07 Eurocopter France Indicateur de pilotage pour aeronef
FR2755945B1 (fr) * 1996-11-19 1999-01-15 Eurocopter France Indicateur de pilotage pour aeronef

Also Published As

Publication number Publication date
US6195598B1 (en) 2001-02-27
FR2756256A1 (fr) 1998-05-29

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Legal Events

Date Code Title Description
CD Change of name or company name

Owner name: AIRBUS HELICOPTERS, FR

Effective date: 20150203

ST Notification of lapse

Effective date: 20160729