FR2907421B1 - Element de panneau deformable et panneau le comprenant - Google Patents

Element de panneau deformable et panneau le comprenant

Info

Publication number
FR2907421B1
FR2907421B1 FR0654381A FR0654381A FR2907421B1 FR 2907421 B1 FR2907421 B1 FR 2907421B1 FR 0654381 A FR0654381 A FR 0654381A FR 0654381 A FR0654381 A FR 0654381A FR 2907421 B1 FR2907421 B1 FR 2907421B1
Authority
FR
France
Prior art keywords
panel
same
deformable
panel element
deformable panel
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
FR0654381A
Other languages
English (en)
Other versions
FR2907421A1 (fr
Inventor
Herve Marche
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 FR0654381A priority Critical patent/FR2907421B1/fr
Publication of FR2907421A1 publication Critical patent/FR2907421A1/fr
Application granted granted Critical
Publication of FR2907421B1 publication Critical patent/FR2907421B1/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
    • B64C1/34—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like comprising inflatable structural components
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/30—Wings comprising inflatable structural components
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/44—Varying camber
    • B64C3/46—Varying camber by inflatable elements
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00—Power-plant nacelles, fairings, or cowlings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/10—Varying effective area of jet pipe or nozzle by distorting the jet pipe or nozzle
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/10—Two-dimensional
    • F05D2250/18—Two-dimensional patterned
    • F05D2250/183—Two-dimensional patterned zigzag
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/50—Intrinsic material properties or characteristics
    • F05D2300/501—Elasticity

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Superstructure Of Vehicle (AREA)
FR0654381A 2006-10-19 2006-10-19 Element de panneau deformable et panneau le comprenant Active FR2907421B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR0654381A FR2907421B1 (fr) 2006-10-19 2006-10-19 Element de panneau deformable et panneau le comprenant

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0654381A FR2907421B1 (fr) 2006-10-19 2006-10-19 Element de panneau deformable et panneau le comprenant

Publications (2)

Publication Number Publication Date
FR2907421A1 FR2907421A1 (fr) 2008-04-25
FR2907421B1 true FR2907421B1 (fr) 2009-06-05

Family

ID=37954040

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0654381A Active FR2907421B1 (fr) 2006-10-19 2006-10-19 Element de panneau deformable et panneau le comprenant

Country Status (1)

Country Link
FR (1) FR2907421B1 (fr)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0908354D0 (en) 2009-05-15 2009-06-24 Airbus Uk Ltd Blade seal
FR2976624B1 (fr) * 2011-06-15 2015-04-03 Snecma Turbomoteur a double flux pour aeronef, a section de sortie variable du flux secondaire
US9989009B2 (en) 2012-10-31 2018-06-05 The Boeing Company Methods and apparatus for sealing variable area fan nozzles of jet engines
GB201420644D0 (en) * 2014-11-20 2015-01-07 Technion Res & Dev Foundation Solid-liquid composite structures
WO2020148765A1 (fr) * 2019-01-15 2020-07-23 Technion Research And Development Foundation Limited Morphage de la peau d'un aéronef au moyen d'un réseau de pelage visqueux intégré

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2979287A (en) * 1959-09-02 1961-04-11 Goodyear Aircraft Corp Inflatable wing with variable camber
US3129908A (en) * 1961-08-25 1964-04-21 Richard G Harper Device for selectively altering lift characteristics of an airfoil
US3892358A (en) * 1971-03-17 1975-07-01 Gen Electric Nozzle seal
ATE444400T1 (de) * 2004-12-08 2009-10-15 Prospective Concepts Ag Druckkörper mit externer membranverstärkung

Also Published As

Publication number Publication date
FR2907421A1 (fr) 2008-04-25

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Legal Events

Date Code Title Description
CA Change of address

Effective date: 20110916

CD Change of name or company name

Owner name: AIRBUS HOLDING, FR

Effective date: 20110916

CJ Change in legal form

Effective date: 20110916

TP Transmission of property

Owner name: AIRBUS HOLDING, FR

Effective date: 20110913

PLFP Fee payment

Year of fee payment: 10

PLFP Fee payment

Year of fee payment: 11

PLFP Fee payment

Year of fee payment: 12