FR2995281B1 - Procede et aeronef pour minimiser les risques de renversement de cet aeronef au sol - Google Patents

Procede et aeronef pour minimiser les risques de renversement de cet aeronef au sol

Info

Publication number
FR2995281B1
FR2995281B1 FR1202443A FR1202443A FR2995281B1 FR 2995281 B1 FR2995281 B1 FR 2995281B1 FR 1202443 A FR1202443 A FR 1202443A FR 1202443 A FR1202443 A FR 1202443A FR 2995281 B1 FR2995281 B1 FR 2995281B1
Authority
FR
France
Prior art keywords
aircraft
minimize
risk
reverse
ground
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
FR1202443A
Other languages
English (en)
Other versions
FR2995281A1 (fr
Inventor
Andre Michel Dequin
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 FR1202443A priority Critical patent/FR2995281B1/fr
Priority to US14/024,756 priority patent/US9796470B2/en
Priority to CN201310415721.4A priority patent/CN103661964B/zh
Publication of FR2995281A1 publication Critical patent/FR2995281A1/fr
Application granted granted Critical
Publication of FR2995281B1 publication Critical patent/FR2995281B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/54—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
    • B64C27/56—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement characterised by the control initiating means, e.g. manually actuated
    • B64C27/57—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement characterised by the control initiating means, e.g. manually actuated automatic or condition responsive, e.g. responsive to rotor speed, torque or thrust
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D43/00—Arrangements or adaptations of instruments
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
FR1202443A 2012-09-13 2012-09-13 Procede et aeronef pour minimiser les risques de renversement de cet aeronef au sol Active FR2995281B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1202443A FR2995281B1 (fr) 2012-09-13 2012-09-13 Procede et aeronef pour minimiser les risques de renversement de cet aeronef au sol
US14/024,756 US9796470B2 (en) 2012-09-13 2013-09-12 Method and an aircraft for minimizing the risks of the aircraft toppling on the ground
CN201310415721.4A CN103661964B (zh) 2012-09-13 2013-09-12 使飞机在地面上倾倒的风险达到最小的方法和飞机

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1202443A FR2995281B1 (fr) 2012-09-13 2012-09-13 Procede et aeronef pour minimiser les risques de renversement de cet aeronef au sol

Publications (2)

Publication Number Publication Date
FR2995281A1 FR2995281A1 (fr) 2014-03-14
FR2995281B1 true FR2995281B1 (fr) 2014-08-29

Family

ID=47172711

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1202443A Active FR2995281B1 (fr) 2012-09-13 2012-09-13 Procede et aeronef pour minimiser les risques de renversement de cet aeronef au sol

Country Status (3)

Country Link
US (1) US9796470B2 (fr)
CN (1) CN103661964B (fr)
FR (1) FR2995281B1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3042885B1 (fr) * 2015-10-23 2018-07-27 Airbus Helicopters Systeme de commande d'un rotor de giravion, giravion equipe d'un tel systeme et methide de commande associee
FR3044809B1 (fr) * 2015-12-03 2017-11-24 Airbus Operations Sas Procede et systeme d'aide a l'atterrissage d'un aeronef.

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2787763B1 (fr) * 1998-12-24 2001-02-23 Eurocopter France Dispositif d'aide au recentrage d'un organe de commande d'un aeronef
FR2809082B1 (fr) * 2000-05-17 2002-09-20 Eurocopter France Indicateur de marge de puissance pour un aeronef a voilure tournante, notamment un helicoptere
DE202007010854U1 (de) * 2007-08-05 2007-10-11 Lees, Thilo System zur Landestoßermittlung bei Luftfahrzeugen
JP4636062B2 (ja) * 2007-08-27 2011-02-23 トヨタ自動車株式会社 車両の挙動制御装置
FR2946315B1 (fr) * 2009-06-04 2011-05-20 Eurocopter France Procede et systeme de commande et de regulation motrice pour helicoptere hybride
US8810435B2 (en) * 2012-06-28 2014-08-19 Honeywell International Inc. Apparatus and method for displaying a helicopter approach to an airport landing pad
US20140012468A1 (en) * 2012-07-09 2014-01-09 Ford Global Technologies, Llc Real-Time Center-of-Gravity Height Estimation

Also Published As

Publication number Publication date
CN103661964A (zh) 2014-03-26
FR2995281A1 (fr) 2014-03-14
US20140070048A1 (en) 2014-03-13
CN103661964B (zh) 2016-04-06
US9796470B2 (en) 2017-10-24

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