ATE517027T1 - Flugzeugsteuerfläche und trägerelement aus faserverbundwerkstoff - Google Patents

Flugzeugsteuerfläche und trägerelement aus faserverbundwerkstoff

Info

Publication number
ATE517027T1
ATE517027T1 AT05109158T AT05109158T ATE517027T1 AT E517027 T1 ATE517027 T1 AT E517027T1 AT 05109158 T AT05109158 T AT 05109158T AT 05109158 T AT05109158 T AT 05109158T AT E517027 T1 ATE517027 T1 AT E517027T1
Authority
AT
Austria
Prior art keywords
composite material
support element
fiber composite
control surface
element made
Prior art date
Application number
AT05109158T
Other languages
English (en)
Inventor
Risto Kallinen
Jani Korpimaeki
Jussi Linjama
Antti Aho-Mantila
Pentti Ahtonen
Original Assignee
Patria Aerostructures 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 Aerostructures Oy filed Critical Patria Aerostructures Oy
Application granted granted Critical
Publication of ATE517027T1 publication Critical patent/ATE517027T1/de

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)
AT05109158T 2004-10-08 2005-10-04 Flugzeugsteuerfläche und trägerelement aus faserverbundwerkstoff ATE517027T1 (de)

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
ATE517027T1 true ATE517027T1 (de) 2011-08-15

Family

ID=33306011

Family Applications (1)

Application Number Title Priority Date Filing Date
AT05109158T ATE517027T1 (de) 2004-10-08 2005-10-04 Flugzeugsteuerfläche und trägerelement aus faserverbundwerkstoff

Country Status (7)

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

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
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
US9938006B2 (en) * 2012-08-28 2018-04-10 Bell Helicopter Textron Inc. Actuation system for an active element in a rotor blade
WO2014068572A2 (en) 2012-11-01 2014-05-08 Israel Aerospace Industries Ltd. Manufacture of integrated structures formed of 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
ES2755765T3 (es) * 2013-12-23 2020-04-23 Airbus Operations Sl Superficie de control de aeronave
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

Family Cites Families (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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.
US6314630B1 (en) * 1996-03-22 2001-11-13 The Boeing Company Determinant wing assembly
US5836550A (en) * 1996-11-27 1998-11-17 Boeing Company Mechanism for streamwise fowler deployment of the wing trailing or leading edge
AU2047999A (en) * 1997-11-07 1999-05-31 Bayer Aktiengesellschaft Method for producing fulvene metal complexes
JP2000043796A (ja) * 1998-07-30 2000-02-15 Japan Aircraft Development Corp 複合材の翼形構造およびその成形方法
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
BRPI0408101A (pt) * 2003-03-03 2006-05-23 Flexsys Inc asa complacente adaptável e sistema de rotor
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
EP1645504A2 (de) 2006-04-12
US7631840B2 (en) 2009-12-15
EP1645504B1 (de) 2011-07-20
AU2005220172A1 (en) 2006-04-27
ES2369914T3 (es) 2011-12-09
AU2005220172B2 (en) 2011-04-14
US20090072090A1 (en) 2009-03-19
FI118122B (fi) 2007-07-13
EP1645504A3 (de) 2009-03-11
CA2522949A1 (en) 2006-04-08
FI20041310A0 (fi) 2004-10-08
FI20041310A (fi) 2006-04-09
CA2522949C (en) 2010-01-12

Similar Documents

Publication Publication Date Title
ATE517027T1 (de) Flugzeugsteuerfläche und trägerelement aus faserverbundwerkstoff
FR2877916B1 (fr) Cadre de structure de fuselage d'aeronef
FR2892070B1 (fr) Siege d'avion a architecture de controle repartie
DE602007011896D1 (de) Ausfallsichere steuerflächentropfenverbindung
WO2008046566A8 (de) Wurmförmiger mechanismus
BRPI0513001A (pt) instalação de produção para a preparação e/ou montagem de mercadorias, uso de um guindaste, e, processo para preparação e/ou montagem de mercadorias
ATE528460T1 (de) Verkleidungsanordnung für einen balkon und befestigungsverfahren dafür
DK1584598T3 (da) Elevator med kabinestyringspanel
ATE483631T1 (de) Flugzeugbaugruppe und mit einer solchen baugruppe ausgestattetes flugzeug
WO2006102091A3 (en) Backpack frame system
BRPI0820293A2 (pt) Conjunto de suporte e estrutura de assento correspondente
WO2005073482A3 (en) Panels and systems of such panels for instance for suspended ceilings
ATE553271T1 (de) Fussbodenpaneel mit polyurethan- und dekorschicht
NO20080508L (no) Festekors og fremgangsmate for feste
GB0525375D0 (en) Mounting mat for a pollution control device
PL1681399T3 (pl) Zestaw konstrukcyjny skrzydła okiennego przystosowanego do znormalizowanej produkcji
PL2088256T3 (pl) Ościeżnica okna dachowego i sposób jej wytwarzania
FR2900671B1 (fr) Construction temporaire et procede d'assemblage associe
FR2884267B1 (fr) Revetement de sol modulaire a dalles encadrees a assemblage rapide des modules d'encadrement
ATE382280T1 (de) Trägervorrichtung und entsprechende sitzstruktur
TW200724427A (en) Saddle and its frame
FR2869604B1 (fr) Activation d'une surface de verre
ATE437336T1 (de) Lampenschirm
DK1921414T3 (da) Panser
EP1965001A8 (de) Bekleidungssystem für Bauwerke mit zweidimensional und/oder sphärisch geformten, zu bekleidenden Bereichen

Legal Events

Date Code Title Description
UEP Publication of translation of european patent specification

Ref document number: 1645504

Country of ref document: EP