FI20041310A - Ilma-aluksen kääntyvä paneeli ja komposiittirakenteinen tukikappale - Google Patents

Ilma-aluksen kääntyvä paneeli ja komposiittirakenteinen tukikappale Download PDF

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Publication number
FI20041310A
FI20041310A FI20041310A FI20041310A FI20041310A FI 20041310 A FI20041310 A FI 20041310A FI 20041310 A FI20041310 A FI 20041310A FI 20041310 A FI20041310 A FI 20041310A FI 20041310 A FI20041310 A FI 20041310A
Authority
FI
Finland
Prior art keywords
aircraft
panel
support body
composite construction
swivel panel
Prior art date
Application number
FI20041310A
Other languages
English (en)
Swedish (sv)
Other versions
FI20041310A0 (fi
FI118122B (fi
Inventor
Risto Kallinen
Jani Korpimaeki
Jussi Linjama
Antti Aho-Mantila
Pentti Ahtonen
Original Assignee
Patria Finavicomp Oy
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 Patria Finavicomp Oy filed Critical Patria Finavicomp Oy
Priority to FI20041310A priority Critical patent/FI118122B/fi
Publication of FI20041310A0 publication Critical patent/FI20041310A0/fi
Priority to AU2005220172A priority patent/AU2005220172B2/en
Priority to ES05109158T priority patent/ES2369914T3/es
Priority to EP05109158A priority patent/EP1645504B1/en
Priority to AT05109158T priority patent/ATE517027T1/de
Priority to CA002522949A priority patent/CA2522949C/en
Publication of FI20041310A publication Critical patent/FI20041310A/fi
Priority to US11/447,235 priority patent/US7631840B2/en
Application granted granted Critical
Publication of FI118122B publication Critical patent/FI118122B/fi

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/02—Mounting or supporting thereof
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/32—Air braking surfaces
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/32—Air braking surfaces
    • B64C9/323—Air braking surfaces associated with wings

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)
  • Forklifts And Lifting Vehicles (AREA)
  • Moulding By Coating Moulds (AREA)
FI20041310A 2004-10-08 2004-10-08 Ilma-aluksen kääntyvä paneeli ja komposiittirakenteinen tukikappale FI118122B (fi)

Priority Applications (7)

Application Number Priority Date Filing Date Title
FI20041310A FI118122B (fi) 2004-10-08 2004-10-08 Ilma-aluksen kääntyvä paneeli ja komposiittirakenteinen tukikappale
AU2005220172A AU2005220172B2 (en) 2004-10-08 2005-10-04 Pivoting panel for aircraft, and composite support piece
ES05109158T ES2369914T3 (es) 2004-10-08 2005-10-04 Superficie con control de avión y elemento de soporte compuesto.
EP05109158A EP1645504B1 (en) 2004-10-08 2005-10-04 Aircraft control surface and composite support element
AT05109158T ATE517027T1 (de) 2004-10-08 2005-10-04 Flugzeugsteuerfläche und trägerelement aus faserverbundwerkstoff
CA002522949A CA2522949C (en) 2004-10-08 2005-10-06 Pivoting panel for aircraft, and composite support piece
US11/447,235 US7631840B2 (en) 2004-10-08 2006-06-05 Pivoting panel for aircraft, and composite support piece

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FI20041310 2004-10-08
FI20041310A FI118122B (fi) 2004-10-08 2004-10-08 Ilma-aluksen kääntyvä paneeli ja komposiittirakenteinen tukikappale

Publications (3)

Publication Number Publication Date
FI20041310A0 FI20041310A0 (fi) 2004-10-08
FI20041310A true FI20041310A (fi) 2006-04-09
FI118122B FI118122B (fi) 2007-07-13

Family

ID=33306011

Family Applications (1)

Application Number Title Priority Date Filing Date
FI20041310A FI118122B (fi) 2004-10-08 2004-10-08 Ilma-aluksen kääntyvä paneeli ja komposiittirakenteinen tukikappale

Country Status (7)

Country Link
US (1) US7631840B2 (fi)
EP (1) EP1645504B1 (fi)
AT (1) ATE517027T1 (fi)
AU (1) AU2005220172B2 (fi)
CA (1) CA2522949C (fi)
ES (1) ES2369914T3 (fi)
FI (1) FI118122B (fi)

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FR2888816B1 (fr) * 2005-07-20 2007-08-31 Airbus France Sas Panneau auto-raidi monolithique
GB0803692D0 (en) * 2008-02-29 2008-04-09 Airbus Uk Ltd Fitting for pivotally connecting aerodynamic control element to aircraft structure
GB0807395D0 (en) * 2008-04-23 2008-05-28 Airbus Uk Ltd Flight surface seal
US20130011605A1 (en) * 2011-07-05 2013-01-10 Israel Aerospace Industries Ltd. Manufacture of articles formed of composite materials
JP5920979B2 (ja) * 2012-07-04 2016-05-24 日本飛行機株式会社 航空機用部材
ES2584557T3 (es) * 2012-08-16 2016-09-28 Airbus Operations S.L. Estructura interna altamente integrada de un cajón de torsión de una superficie sustentadora de una aeronave y método para su producción
US9938006B2 (en) * 2012-08-28 2018-04-10 Bell Helicopter Textron Inc. Actuation system for an active element in a rotor blade
US9180966B2 (en) 2012-08-28 2015-11-10 Bell Helicopter Textron Inc. Actuation system for an active element in a rotor blade
US9180965B2 (en) 2012-08-28 2015-11-10 Bell Helicopter Textron Inc. Actuation system for an active element in a rotor blade
EP2914488A4 (en) 2012-11-01 2016-06-29 Israel Aerospace Ind Ltd MANUFACTURE OF INTEGRATED STRUCTURES MADE FROM COMPOSITE MATERIALS
ES2623044T3 (es) * 2012-11-22 2017-07-10 Airbus Operations S.L. Método de fabricación de una estructura altamente integrada incluyendo costillas de borde de ataque y de salida para una superficie de elevación de una aeronave
US8983171B2 (en) 2012-12-26 2015-03-17 Israel Aerospace Industries Ltd. System and method for inspecting structures formed of composite materials during the fabrication thereof
GB201315341D0 (en) * 2013-08-29 2013-10-09 Airbus Operations Ltd An aircraft structure and method of manufacture
EP2886450B1 (en) * 2013-12-23 2019-09-18 Airbus Operations S.L. Aircraft control surface
US10570936B2 (en) * 2014-03-07 2020-02-25 Parker-Hannifin Corporation Symmetrically loaded dual hydraulic fly-by-wire actuator
DE102014106743B4 (de) * 2014-05-13 2023-12-21 Airbus Operations Gmbh Strömungskörper mit einem darin integrierten Lasteinleitungselement, Verfahren zum Herstellen eines Strömungskörpers und Flugzeug mit einem solchen Strömungskörper
AT516211A1 (de) * 2014-08-11 2016-03-15 Facc Ag Steuerflächenelement
AT517198B1 (de) * 2015-04-24 2021-12-15 Facc Ag Steuerflächenelement für ein Flugzeug
DE102017117314A1 (de) 2017-07-31 2019-01-31 Airbus Operations Gmbh Befestigungseinheit zum beweglichen Befestigen einer Luftfahrzeugkomponente an einer Tragstruktur eines Luftfahrzeugs
GB2583134B (en) * 2019-04-18 2021-11-24 Fokker Aerostructures Bv Hinge structure

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US2451131A (en) * 1940-09-06 1948-10-12 Vidal Corp Method of making reinforced structures
US2403568A (en) * 1943-03-06 1946-07-09 Budd Edward G Mfg Co Aircraft control surface structure and method of assembly of same
US3102559A (en) * 1959-12-24 1963-09-03 Raymond Dev Ind Inc Woven honeycomb cellular fabrics
US3140066A (en) * 1962-12-04 1964-07-07 North American Aviation Inc Multiple pivot mounting means
US3768760A (en) * 1970-10-30 1973-10-30 Hercules Inc Graphite fiber composite covering employing multi-directional
US3775238A (en) * 1971-06-24 1973-11-27 J Lyman Structural composite material
DE2336541C3 (de) 1973-07-18 1980-04-24 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Anordnung zum Einleiten von Kräften in ein flächiges Bauteil mit Sandwichstruktur
US4003533A (en) * 1973-10-01 1977-01-18 General Dynamics Corporation Combination airbrake and pitch control device
US4131252A (en) * 1976-06-15 1978-12-26 The Boeing Company Apparatus for compensating for airflow blockage in aircraft slotted flap assemblies
US4335671A (en) * 1980-07-17 1982-06-22 The Boeing Company Flap leading edge for hydrofoil vessels and the like
US4471927A (en) * 1981-09-29 1984-09-18 The Boeing Company Trailing edge flap assembly
US4470366A (en) * 1982-09-30 1984-09-11 The Boeing Company Continuous single flap hinge and seal device for flexible hydrofoils and the like
SE446847B (sv) 1984-02-14 1986-10-13 Harald Unden Laminerad konstruktionsdel
US5224670A (en) 1991-09-13 1993-07-06 Grumman Aerospace Corporation Composite focused load control surface
FR2687173B1 (fr) 1992-02-11 1995-09-08 Aerospatiale Procede pour la realisation d'une armature de fibres pour piece de matiere composite, et piece composite comportant une telle armature.
FR2718707B1 (fr) * 1994-04-18 1996-07-12 Aerospatiale Dispositif de protection d'une charnière de gouverne, notamment pour aéronef.
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US5836550A (en) * 1996-11-27 1998-11-17 Boeing Company Mechanism for streamwise fowler deployment of the wing trailing or leading edge
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US6173924B1 (en) * 1999-06-15 2001-01-16 Northrop Grumman Corporation Low density flexible edge transition
US6889937B2 (en) * 1999-11-18 2005-05-10 Rocky Mountain Composites, Inc. Single piece co-cure composite wing
US6419189B1 (en) * 2000-11-01 2002-07-16 The Boeing Company Hot ruddervator apparatus and method for an aerospacecraft
ATE284346T1 (de) 2001-01-26 2004-12-15 Fischer Adv Components Gmbh Einrichtung zum verbinden beweglicher teile mit strukturbauteilen von flugzeugen od. dgl.
AT409482B (de) 2001-01-26 2002-08-26 Fischer Adv Components Gmbh Einrichtung zum verbinden beweglicher teile mit strukturbauteilen von flugzeugen od. dgl.
US6945727B2 (en) * 2002-07-19 2005-09-20 The Boeing Company Apparatuses and methods for joining structural members, such as composite structural members
DK1603798T3 (da) * 2003-03-03 2011-02-14 Flexsys Inc Tilpasningsdygtigt og fleksibelt vinge- og rotorsystem
DE10328717B3 (de) * 2003-06-25 2004-12-02 Eads Deutschland Gmbh Betätigungseinrichtung für eine an der Hinterkante des Tragflügels eines Flugzeugs angeordnete Ruderklappe

Also Published As

Publication number Publication date
CA2522949C (en) 2010-01-12
FI20041310A0 (fi) 2004-10-08
ES2369914T3 (es) 2011-12-09
EP1645504B1 (en) 2011-07-20
AU2005220172B2 (en) 2011-04-14
AU2005220172A1 (en) 2006-04-27
US20090072090A1 (en) 2009-03-19
ATE517027T1 (de) 2011-08-15
EP1645504A3 (en) 2009-03-11
FI118122B (fi) 2007-07-13
EP1645504A2 (en) 2006-04-12
US7631840B2 (en) 2009-12-15
CA2522949A1 (en) 2006-04-08

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