[go: up one dir, main page]

FR2966425B1 - Aeronef muni d'un empennage comprenant un moyen de lutte contre le flottement aeroelastique. - Google Patents

Aeronef muni d'un empennage comprenant un moyen de lutte contre le flottement aeroelastique.

Info

Publication number
FR2966425B1
FR2966425B1 FR1004204A FR1004204A FR2966425B1 FR 2966425 B1 FR2966425 B1 FR 2966425B1 FR 1004204 A FR1004204 A FR 1004204A FR 1004204 A FR1004204 A FR 1004204A FR 2966425 B1 FR2966425 B1 FR 2966425B1
Authority
FR
France
Prior art keywords
aerelastic
combating
employment
aircraft
floating
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
FR1004204A
Other languages
English (en)
Other versions
FR2966425A1 (fr
Inventor
Rodolphe Lhermenault
Thomas Meyer
Jean Azeau
Julien Guitton
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 FR1004204A priority Critical patent/FR2966425B1/fr
Priority to US13/274,544 priority patent/US8814083B2/en
Publication of FR2966425A1 publication Critical patent/FR2966425A1/fr
Application granted granted Critical
Publication of FR2966425B1 publication Critical patent/FR2966425B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/26—Attaching the wing or tail units or stabilising surfaces
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
    • B64C2027/8263—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft comprising in addition rudders, tails, fins, or the like
    • B64C2027/8281—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft comprising in addition rudders, tails, fins, or the like comprising horizontal tail planes

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)
FR1004204A 2010-10-26 2010-10-26 Aeronef muni d'un empennage comprenant un moyen de lutte contre le flottement aeroelastique. Active FR2966425B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1004204A FR2966425B1 (fr) 2010-10-26 2010-10-26 Aeronef muni d'un empennage comprenant un moyen de lutte contre le flottement aeroelastique.
US13/274,544 US8814083B2 (en) 2010-10-26 2011-10-17 Aircraft provided with a tail plane including means for combating flutter

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1004204A FR2966425B1 (fr) 2010-10-26 2010-10-26 Aeronef muni d'un empennage comprenant un moyen de lutte contre le flottement aeroelastique.

Publications (2)

Publication Number Publication Date
FR2966425A1 FR2966425A1 (fr) 2012-04-27
FR2966425B1 true FR2966425B1 (fr) 2013-08-16

Family

ID=44080221

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1004204A Active FR2966425B1 (fr) 2010-10-26 2010-10-26 Aeronef muni d'un empennage comprenant un moyen de lutte contre le flottement aeroelastique.

Country Status (2)

Country Link
US (1) US8814083B2 (fr)
FR (1) FR2966425B1 (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2995586B1 (fr) 2012-09-17 2014-08-22 Eurocopter France Moyen de stabilisation en tangage et aeronef a voilure tournante muni d'un tel moyen
USD817253S1 (en) * 2016-01-20 2018-05-08 Hansung Ils Co., Ltd. Helicopter
US10407154B2 (en) * 2017-04-18 2019-09-10 Bell Helicopter Textron Inc. Horizontal stabilizer mount for a rotorcraft

Family Cites Families (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2113000A (en) * 1933-05-17 1938-04-05 Curtiss Wright Corp Antiflutter device
US2981504A (en) * 1959-03-13 1961-04-25 Gen Dynamics Corp Fuselage blade sealing using conical surfaces
US3448946A (en) * 1966-09-16 1969-06-10 Kawasaki Kokuki Kogyo Kk Compound helicopter
US4227665A (en) * 1978-05-11 1980-10-14 Textron, Inc. Fixed leading edge slat spoiler for a horizontal stabilizer
US4708305A (en) * 1987-01-30 1987-11-24 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Helicopter anti-torque system using fuselage strakes
US5209430A (en) * 1991-11-07 1993-05-11 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Helicopter low-speed yaw control
US5377934A (en) * 1993-01-25 1995-01-03 Hill; Jamie R. Helicopter conversion
FR2719553B1 (fr) * 1994-05-04 1996-07-26 Eurocopter France Dispositif anti-couple à rotor arrière et stator redresseur carénés pour hélicoptère.
US5641133A (en) * 1994-05-11 1997-06-24 Mcdonnell Douglas Helicopter Co. Rotorcraft fuselage modal frequency placement using resilient mounting connections
USD363054S (en) * 1994-08-30 1995-10-10 Bell Helicopter Textron Inc. Helicopter
USD375077S (en) * 1995-01-24 1996-10-29 Bell Helicopter Textron Inc. Helicopter
US6116389A (en) * 1995-08-07 2000-09-12 Quality Research, Development & Consulting, Inc. Apparatus and method for confinement and damping of vibration energy
JP3051357B2 (ja) * 1997-03-26 2000-06-12 株式会社コミュータヘリコプタ先進技術研究所 主ロータトルク補正装置
EP1300335B1 (fr) * 2001-10-05 2005-03-02 Airbus France Aéronef à carénage ventral
US6830218B2 (en) * 2002-12-31 2004-12-14 The Boeing Company Structural attach method for thin fairings
US6938856B2 (en) * 2003-10-21 2005-09-06 Hobbico, Inc. Empennage assembly and attachment mechanism for a model airplane
US7393488B2 (en) * 2005-05-25 2008-07-01 The Boeing Company Methods of joining structures and joints formed thereby
ATE423060T1 (de) 2006-03-16 2009-03-15 Eads Constr Aeronauticas Sa Elastisch vorgeformte verkleidung für flugzeuge und verfahren zur ihrer herstellung
ES2315108B1 (es) * 2006-06-30 2010-01-12 Aibus España, S.L. Sistema de fijacion de un borde de ataque a la estructura de un plano sustentador de un avion.
US7575194B2 (en) 2006-11-30 2009-08-18 The Boeing Company Apparatuses and methods for joining composite members and other structural members in aircraft wing boxes and other structures
FR2915173B1 (fr) 2007-04-17 2009-10-23 Airbus Sa Sa Dispositif de fixation d'un organe de sustentation au fuselage d'un avion.
US8210468B2 (en) * 2007-05-14 2012-07-03 Blr Aerospace, L.L.C. Aircraft stabilizer system and methods of using the same
DE102008015073B4 (de) * 2008-03-19 2014-02-13 Eurocopter Deutschland Gmbh Hubschrauber mit Mitteln zur aerodynamischen Unterstützung des Drehmomentausgleichs
ES2369451B1 (es) * 2008-12-29 2012-10-15 Airbus Operations, S.L. Sistema de carenas para estabilizador horizontal de aeronave y procedimiento de instalación de dicho sistema.
ES2386136B1 (es) * 2009-03-30 2013-07-25 Airbus Operations, S.L. Estructura para el acoplamiento de la carena de una aeronave

Also Published As

Publication number Publication date
US20120138739A1 (en) 2012-06-07
US8814083B2 (en) 2014-08-26
FR2966425A1 (fr) 2012-04-27

Similar Documents

Publication Publication Date Title
GB2510488B (en) Identifying peptides at the single molecule level
GB201206830D0 (en) .
GB201106766D0 (en) .
GB201118961D0 (en) .
GB201118592D0 (en) .
PL120467U1 (pl) Osłona przed przeciągiem dla wagi
GB201104448D0 (en) .
WO2011117271A3 (fr) Mélanges fongicides basés sur des azolopyrimidinylamines
FR2994941B1 (fr) Ensemble propulsif pour aeronef comprenant un carenage structural.
GB201104429D0 (en) .
GB201102141D0 (en) .
GB201115799D0 (en) .
GB201114750D0 (en) .
AP2011005575A0 (en) Emulsion explosives.
FR2966425B1 (fr) Aeronef muni d'un empennage comprenant un moyen de lutte contre le flottement aeroelastique.
Niinaga Yuwan (Amami Ryukyuan)
GB201122259D0 (en) .
GB201119853D0 (en) .
Williamson About the Author
GB201117584D0 (en) .
GB201003897D0 (en) F.I.B.C ramp loader
Hemingway Ten Poems
Devečerski C bojnih polja
Millares Ecocalypso
杜飞 et al. 三山岛金矿新立主混合井快速掘砌技术研究

Legal Events

Date Code Title Description
CD Change of name or company name

Owner name: AIRBUS HELICOPTERS, FR

Effective date: 20140602

PLFP Fee payment

Year of fee payment: 6

PLFP Fee payment

Year of fee payment: 7

PLFP Fee payment

Year of fee payment: 8

PLFP Fee payment

Year of fee payment: 9

PLFP Fee payment

Year of fee payment: 10

PLFP Fee payment

Year of fee payment: 11

PLFP Fee payment

Year of fee payment: 12

PLFP Fee payment

Year of fee payment: 13

PLFP Fee payment

Year of fee payment: 14

PLFP Fee payment

Year of fee payment: 15

PLFP Fee payment

Year of fee payment: 16