ATE505399T1 - Strukturbaueinheit zum verdecken eines verlängerte spalts über den aerodynamischen fläche eines flugzeuges - Google Patents

Strukturbaueinheit zum verdecken eines verlängerte spalts über den aerodynamischen fläche eines flugzeuges

Info

Publication number
ATE505399T1
ATE505399T1 AT09165623T AT09165623T ATE505399T1 AT E505399 T1 ATE505399 T1 AT E505399T1 AT 09165623 T AT09165623 T AT 09165623T AT 09165623 T AT09165623 T AT 09165623T AT E505399 T1 ATE505399 T1 AT E505399T1
Authority
AT
Austria
Prior art keywords
covering
aircraft
aerodynamic surface
structural unit
sliding
Prior art date
Application number
AT09165623T
Other languages
English (en)
Inventor
Franco Candela
Giuseppe Migliozzi
Original Assignee
Alenia Aeronautica Spa
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 Alenia Aeronautica Spa filed Critical Alenia Aeronautica Spa
Application granted granted Critical
Publication of ATE505399T1 publication Critical patent/ATE505399T1/de

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C7/00—Structures or fairings not otherwise provided for

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)
  • Connection Of Plates (AREA)
  • Golf Clubs (AREA)
  • Shielding Devices Or Components To Electric Or Magnetic Fields (AREA)
  • Paper (AREA)
  • Holo Graphy (AREA)
  • Stereophonic System (AREA)
AT09165623T 2008-07-16 2009-07-16 Strukturbaueinheit zum verdecken eines verlängerte spalts über den aerodynamischen fläche eines flugzeuges ATE505399T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ITTO2008A000545A IT1390909B1 (it) 2008-07-16 2008-07-16 Elemento strutturale a rigidezza calcolata, con caratteristiche di assorbimento di spostamenti e copertura interstizi

Publications (1)

Publication Number Publication Date
ATE505399T1 true ATE505399T1 (de) 2011-04-15

Family

ID=40756424

Family Applications (1)

Application Number Title Priority Date Filing Date
AT09165623T ATE505399T1 (de) 2008-07-16 2009-07-16 Strukturbaueinheit zum verdecken eines verlängerte spalts über den aerodynamischen fläche eines flugzeuges

Country Status (6)

Country Link
US (1) US8342452B2 (de)
EP (1) EP2147857B1 (de)
AT (1) ATE505399T1 (de)
DE (1) DE602009001065D1 (de)
ES (1) ES2364544T3 (de)
IT (1) IT1390909B1 (de)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2960216B1 (fr) 2010-05-19 2013-02-15 Aircelle Sa Element d'aerodynamisme pour une nacelle d'aeronef
WO2012173542A1 (en) * 2011-06-16 2012-12-20 Saab Ab A double-curved cover for covering a gap between two structural portions of an aircraft
DE102011085269A1 (de) * 2011-10-27 2013-05-02 Airbus Operations Gmbh Abdeckplatte, Türabdeckung sowie Luft- oder Raumfahrzeug
DE102013110480A1 (de) * 2013-09-23 2015-03-26 Airbus Operations Gmbh Blende und Türanordnung für ein Transportmittel
GB2545431A (en) * 2015-12-15 2017-06-21 Airbus Operations Ltd Seal
US10017239B2 (en) 2015-12-18 2018-07-10 Northrop Grumman Systems Corporation Dynamic conformal aerodynamic seal (CAS) for aircraft control surfaces
US9809295B1 (en) 2016-06-07 2017-11-07 Northrop Grumman Systems Corporation Flight actuated door seal
GB2561874B (en) * 2017-04-26 2019-09-18 Airbus Operations Ltd Magnetic seals

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2915948A (en) * 1956-06-07 1959-12-08 Boeing Co Airflow deflector for tail gun turrets
US3184186A (en) * 1962-09-20 1965-05-18 Shin Mitsubishi Jukogyo Kk Spoiler
DE2216710A1 (de) * 1972-04-07 1973-10-18 Dornier Gmbh Abdeckschild zur stroemungsguenstigen verkleidung von oberflaechenoeffnungen in bauteilen, insbesondere von oeffnungen an teilen von fluggeraeten
US4120470A (en) * 1976-09-28 1978-10-17 The Boeing Company Efficient trailing edge system for an aircraft wing
US4705236A (en) * 1981-09-29 1987-11-10 The Boeing Company Aileron system for aircraft and method of operating the same
US4784355A (en) * 1986-11-10 1988-11-15 The United States Of America As Represented By The Secretary Of The Air Force Flap system for short takeoff and landing aircraft
FR2670177B1 (fr) * 1990-12-05 1993-01-22 Snecma Joint d'etancheite entre l'arriere du fuselage d'un avion et les volets exterieurs de son turboreacteur.
US5372336A (en) * 1993-04-05 1994-12-13 Grumman Aerospace Corporation Folding wing assembly
US5598990A (en) * 1994-12-15 1997-02-04 University Of Kansas Center For Research Inc. Supersonic vortex generator
FR2728535A1 (fr) * 1994-12-26 1996-06-28 Aerospatiale Aerofrein a fente variable pour voilure d'aeronef
GB2323576B (en) * 1997-03-26 2001-08-22 British Aerospace Fairing arrangements for aircraft
NL1007065C2 (nl) * 1997-09-18 1999-03-24 Inalfa Ind Bv Open-dakconstructie voor een voertuig.
FR2789144A1 (fr) * 1999-02-03 2000-08-04 Joint Francais Joint pour panneaux et aeronef comportant un tel joint
DE29912525U1 (de) * 1999-07-17 2000-07-06 Karmann Gmbh W Cabriolet-Fahrzeug
FR2840877B1 (fr) * 2002-06-13 2004-08-06 Airbus France Dispositif d'articulation d'un volet sur une surface aerodynamique d'aeronef
US6877695B2 (en) * 2002-12-13 2005-04-12 The Boeing Company Hinge cover integration into door seal edges
FR2859976B1 (fr) * 2003-09-22 2006-12-08 Airbus France Aile d'aeronef comportant au moins un volet deporteur et volet deporteur pour ladite aile
ES2277716B1 (es) * 2004-12-31 2008-05-16 Airbus España, S.L. Tapa reforzada para ranuras en un contorno aerodinamico.
EP1686056B1 (de) * 2004-12-31 2011-07-27 Airbus Operations S.L. Verstärkte Abdeckung für Öffnungen eines aerodynamischen Profils
ES2277715B1 (es) * 2004-12-31 2008-05-16 Airbus España, S.L. Tapa reforzada para escotaduras en un contorno aerodinamico.
US7708231B2 (en) * 2005-11-21 2010-05-04 The Boeing Company Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods
GB0525896D0 (en) * 2005-12-20 2006-02-01 Airbus Uk Ltd A joint for use in aircraft construction

Also Published As

Publication number Publication date
EP2147857B1 (de) 2011-04-13
IT1390909B1 (it) 2011-10-19
ITTO20080545A1 (it) 2010-01-17
EP2147857A1 (de) 2010-01-27
ES2364544T3 (es) 2011-09-06
US20100096504A1 (en) 2010-04-22
DE602009001065D1 (de) 2011-05-26
US8342452B2 (en) 2013-01-01

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Legal Events

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