FR2809082B1 - 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
FR2809082B1
FR2809082B1 FR0006270A FR0006270A FR2809082B1 FR 2809082 B1 FR2809082 B1 FR 2809082B1 FR 0006270 A FR0006270 A FR 0006270A FR 0006270 A FR0006270 A FR 0006270A FR 2809082 B1 FR2809082 B1 FR 2809082B1
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
FR0006270A
Other languages
English (en)
Other versions
FR2809082A1 (fr
Inventor
Alain Permanne
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
Eurocopter 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, Eurocopter SA filed Critical Eurocopter France SA
Priority to FR0006270A priority Critical patent/FR2809082B1/fr
Priority to US09/814,956 priority patent/US6411869B2/en
Publication of FR2809082A1 publication Critical patent/FR2809082A1/fr
Application granted granted Critical
Publication of FR2809082B1 publication Critical patent/FR2809082B1/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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Turbines (AREA)
FR0006270A 2000-05-17 2000-05-17 Indicateur de marge de puissance pour un aeronef a voilure tournante, notamment un helicoptere Expired - Fee Related FR2809082B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0006270A FR2809082B1 (fr) 2000-05-17 2000-05-17 Indicateur de marge de puissance pour un aeronef a voilure tournante, notamment un helicoptere
US09/814,956 US6411869B2 (en) 2000-05-17 2001-03-23 Power margin indicator for a rotary wing aircraft, particularly a helicopter

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0006270A FR2809082B1 (fr) 2000-05-17 2000-05-17 Indicateur de marge de puissance pour un aeronef a voilure tournante, notamment un helicoptere

Publications (2)

Publication Number Publication Date
FR2809082A1 FR2809082A1 (fr) 2001-11-23
FR2809082B1 true FR2809082B1 (fr) 2002-09-20

Family

ID=8850306

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0006270A Expired - Fee Related FR2809082B1 (fr) 2000-05-17 2000-05-17 Indicateur de marge de puissance pour un aeronef a voilure tournante, notamment un helicoptere

Country Status (2)

Country Link
US (1) US6411869B2 (fr)
FR (1) FR2809082B1 (fr)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
US7031812B1 (en) * 2004-03-15 2006-04-18 Howell Instruments, Inc. System and method for monitoring aircraft engine health and determining engine power available, and applications thereof
FR2875916B1 (fr) * 2004-09-28 2015-06-26 Eurocopter France Procede et dispositif d'aide au pilotage d'un aeronef a voilure tournante au voisinage d'un point de pose ou de decollage
US7414544B2 (en) * 2005-01-28 2008-08-19 Bell Helicopter Textron, Inc. Power situation indicator
FR2888638B1 (fr) * 2005-07-18 2007-09-28 Airbus Sas Indicateur de pilotage pour un aeronef, destine a fournir un parametre de puissance d'au moins un turbopropulseur dudit 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
US20080140268A1 (en) * 2006-12-11 2008-06-12 Howell Instruments, Inc. Total engine smart indicator for an aircraft, and application thereof
FR2932919B1 (fr) 2008-06-24 2010-08-20 Eurocopter France Adaptation d'alertes de terrain selectives, en fonction la manoeuvrabilite instantanee d'un giravion
WO2010056241A1 (fr) * 2008-11-13 2010-05-20 Sikorsky Aircraft Corporation Système à sécurité intégrée adaptatif pour turbines à gaz commandées par régulation automatique à pleine autorité redondante
FR2943131B1 (fr) * 2009-03-12 2011-02-25 Eurocopter France Procede de determination et d'affichage d'indications de pilotage et indicateur de pilotage pour mettre en oeuvre ledit procede
FR2973340B1 (fr) * 2011-03-30 2013-04-12 Eurocopter France Procede, dispositif d'aide au pilotage d'un aeronef, et aeronef
FR2995281B1 (fr) * 2012-09-13 2014-08-29 Eurocopter France Procede et aeronef pour minimiser les risques de renversement de cet aeronef au sol
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
US9514628B2 (en) * 2015-03-26 2016-12-06 Bell Helicopter Textron Inc. Electrical load monitoring system
CN105447079B (zh) * 2015-11-04 2018-11-02 华中科技大学 一种基于函数依赖的数据清洗方法
FR3051772B1 (fr) 2016-05-30 2019-08-23 Airbus Helicopters Procede, dispositif d'aide au pilotage d'un aeronef, et aeronef
US10173787B1 (en) * 2018-02-12 2019-01-08 Bell Helicopter Textron Inc. Rotor speed indication systems for rotorcraft
US11247782B2 (en) * 2018-09-21 2022-02-15 Textron Innovations Inc. System and method for controlling rotorcraft
FR3116044B1 (fr) 2020-11-10 2022-12-30 Safran Helicopter Engines Procédé de détermination d’au moins une limite de puissance d’une chaine propulsive hybride pour véhicule de transport, en particulier, un aéronef
FR3134564B1 (fr) 2022-04-15 2024-07-19 Airbus Helicopters Procédé et système d'aide au pilotage d'un aéronef, aéronef équipé d’un tel système.
FR3138414A1 (fr) * 2022-07-29 2024-02-02 Safran Helicopter Engines Surveillance d’un systeme propulsif d’un aeronef

Family Cites Families (4)

* 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
FR2731069B1 (fr) * 1995-02-23 1997-04-30 Pelletier Patrick Dispositif d'aide au pilotage
FR2755945B1 (fr) * 1996-11-19 1999-01-15 Eurocopter France Indicateur de pilotage pour aeronef
FR2756256B1 (fr) * 1996-11-26 1999-01-22 Eurocopter France Indicateur de marge de puissance pour un aeronef a voilure tournante, notamment un helicoptere

Also Published As

Publication number Publication date
US6411869B2 (en) 2002-06-25
US20010044679A1 (en) 2001-11-22
FR2809082A1 (fr) 2001-11-23

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Legal Events

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CD Change of name or company name

Owner name: AIRBUS HELICOPTERS, FR

Effective date: 20140602

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Year of fee payment: 17

PLFP Fee payment

Year of fee payment: 18

PLFP Fee payment

Year of fee payment: 19

ST Notification of lapse

Effective date: 20200108