FR2929590B1 - Ensemble de surfaces aerodynamiques pour aeronef. - Google Patents

Ensemble de surfaces aerodynamiques pour aeronef.

Info

Publication number
FR2929590B1
FR2929590B1 FR0801822A FR0801822A FR2929590B1 FR 2929590 B1 FR2929590 B1 FR 2929590B1 FR 0801822 A FR0801822 A FR 0801822A FR 0801822 A FR0801822 A FR 0801822A FR 2929590 B1 FR2929590 B1 FR 2929590B1
Authority
FR
France
Prior art keywords
aircraft
aerodynamic surface
surface assembly
assembly
aerodynamic
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
FR0801822A
Other languages
English (en)
Other versions
FR2929590A1 (fr
Inventor
Bertrand Soucheleau
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
Priority to FR0801822A priority Critical patent/FR2929590B1/fr
Priority to US12/413,959 priority patent/US8128039B2/en
Publication of FR2929590A1 publication Critical patent/FR2929590A1/fr
Application granted granted Critical
Publication of FR2929590B1 publication Critical patent/FR2929590B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/30—Balancing hinged surfaces, e.g. dynamically
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/10—Adjustable control surfaces or members, e.g. rudders one surface adjusted by movement of another, e.g. servo tabs

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Pallets (AREA)
FR0801822A 2008-04-02 2008-04-02 Ensemble de surfaces aerodynamiques pour aeronef. Active FR2929590B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0801822A FR2929590B1 (fr) 2008-04-02 2008-04-02 Ensemble de surfaces aerodynamiques pour aeronef.
US12/413,959 US8128039B2 (en) 2008-04-02 2009-03-30 Aerodynamic surface assembly for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0801822A FR2929590B1 (fr) 2008-04-02 2008-04-02 Ensemble de surfaces aerodynamiques pour aeronef.

Publications (2)

Publication Number Publication Date
FR2929590A1 FR2929590A1 (fr) 2009-10-09
FR2929590B1 true FR2929590B1 (fr) 2011-01-14

Family

ID=39930688

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0801822A Active FR2929590B1 (fr) 2008-04-02 2008-04-02 Ensemble de surfaces aerodynamiques pour aeronef.

Country Status (2)

Country Link
US (1) US8128039B2 (fr)
FR (1) FR2929590B1 (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2955309B1 (fr) * 2010-01-18 2013-05-10 Airbus Operations Sas Systeme de commande de vol pour un aeronef
CN104554705A (zh) * 2014-11-19 2015-04-29 中国航空工业集团公司沈阳飞机设计研究所 一种降低通用飞机舵面铰链力矩的方法
CN104978489B (zh) * 2015-07-02 2016-11-16 北京航天自动控制研究所 一种适用于滑翔飞行器的最小铰链力矩下压弹道计算方法

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US551495A (en) * 1895-12-17 Centrifugal grain-separator
GB491538A (en) * 1937-03-06 1938-09-05 Westland Aircraft Ltd Improvements in or relating to aircraft
US2239475A (en) * 1937-07-24 1941-04-22 Fred E Weick Balancing aircraft control surfaces
US2281696A (en) * 1940-03-12 1942-05-05 Lockheed Aircraft Corp Balanced control surface
US2551495A (en) * 1944-06-14 1951-05-01 Bell Aircraft Corp Aircraft control surface balance means
US2603436A (en) * 1947-03-18 1952-07-15 North American Aviation Inc Balanced control surface
US2630988A (en) * 1950-02-21 1953-03-10 North American Aviation Inc Aerodynamic balance control
US3790106A (en) * 1973-01-24 1974-02-05 J Morris Flap system
US3910530A (en) * 1973-11-07 1975-10-07 Boeing Co Leading edge flap
US4285482A (en) * 1979-08-10 1981-08-25 The Boeing Company Wing leading edge high lift device
US4995575A (en) * 1988-09-26 1991-02-26 The Boeing Company Wing trailing edge flap mechanism
GB8915487D0 (en) * 1989-07-06 1989-08-23 Short Brothers Plc A flap assembly
US5538202A (en) * 1993-11-02 1996-07-23 Northrop Grumman Corporation Hydraulic actuation system for aircraft control surfaces
US5603436A (en) * 1995-01-12 1997-02-18 Nalge Company Squeeze bottle and leakproof closure device
ES2156660B1 (es) * 1998-01-14 2002-02-16 Saiz Manuel Munoz Mandos de vuelo con compensacion automatica.
US6257528B1 (en) * 1999-07-20 2001-07-10 The Boeing Company Vehicle control system and method employing control surface and geared tab
US7510150B2 (en) * 2005-09-28 2009-03-31 The Boeing Company Energy recovery apparatus and method
US7766282B2 (en) * 2007-12-11 2010-08-03 The Boeing Company Trailing edge device catchers and associated systems and methods

Also Published As

Publication number Publication date
FR2929590A1 (fr) 2009-10-09
US8128039B2 (en) 2012-03-06
US20090250558A1 (en) 2009-10-08

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Effective date: 20110916

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