FR2903961B1 - STRUCTURAL COMPONENT OF THE ROTOR CELL, METHOD FOR MANUFACTURING THE SAME, ROTARY CELL AND GIRAVION COMPRISING SUCH STRUCTURAL ELEMENTS - Google Patents

STRUCTURAL COMPONENT OF THE ROTOR CELL, METHOD FOR MANUFACTURING THE SAME, ROTARY CELL AND GIRAVION COMPRISING SUCH STRUCTURAL ELEMENTS

Info

Publication number
FR2903961B1
FR2903961B1 FR0606703A FR0606703A FR2903961B1 FR 2903961 B1 FR2903961 B1 FR 2903961B1 FR 0606703 A FR0606703 A FR 0606703A FR 0606703 A FR0606703 A FR 0606703A FR 2903961 B1 FR2903961 B1 FR 2903961B1
Authority
FR
France
Prior art keywords
cell
giravion
manufacturing
same
structural
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.)
Expired - Fee Related
Application number
FR0606703A
Other languages
French (fr)
Other versions
FR2903961A1 (en
Inventor
Herve Payen
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 Helicopters SAS
Original Assignee
Eurocopter France SA
Eurocopter SA
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 Eurocopter France SA, Eurocopter SA filed Critical Eurocopter France SA
Priority to FR0606703A priority Critical patent/FR2903961B1/en
Publication of FR2903961A1 publication Critical patent/FR2903961A1/en
Application granted granted Critical
Publication of FR2903961B1 publication Critical patent/FR2903961B1/en
Expired - Fee Related 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
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/061—Frames
    • B64C1/062—Frames specially adapted to absorb crash loads
    • 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
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/068—Fuselage sections
FR0606703A 2006-07-21 2006-07-21 STRUCTURAL COMPONENT OF THE ROTOR CELL, METHOD FOR MANUFACTURING THE SAME, ROTARY CELL AND GIRAVION COMPRISING SUCH STRUCTURAL ELEMENTS Expired - Fee Related FR2903961B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR0606703A FR2903961B1 (en) 2006-07-21 2006-07-21 STRUCTURAL COMPONENT OF THE ROTOR CELL, METHOD FOR MANUFACTURING THE SAME, ROTARY CELL AND GIRAVION COMPRISING SUCH STRUCTURAL ELEMENTS

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0606703A FR2903961B1 (en) 2006-07-21 2006-07-21 STRUCTURAL COMPONENT OF THE ROTOR CELL, METHOD FOR MANUFACTURING THE SAME, ROTARY CELL AND GIRAVION COMPRISING SUCH STRUCTURAL ELEMENTS

Publications (2)

Publication Number Publication Date
FR2903961A1 FR2903961A1 (en) 2008-01-25
FR2903961B1 true FR2903961B1 (en) 2009-09-25

Family

ID=37770843

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0606703A Expired - Fee Related FR2903961B1 (en) 2006-07-21 2006-07-21 STRUCTURAL COMPONENT OF THE ROTOR CELL, METHOD FOR MANUFACTURING THE SAME, ROTARY CELL AND GIRAVION COMPRISING SUCH STRUCTURAL ELEMENTS

Country Status (1)

Country Link
FR (1) FR2903961B1 (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5297288B2 (en) * 2009-07-17 2013-09-25 三菱重工業株式会社 Shock absorbing structure
DE102010014638B4 (en) 2010-04-12 2019-08-01 Airbus Defence and Space GmbH Aircraft with an integrated energy absorbing deformation structure and aircraft with such a fuselage
FR2969729B1 (en) 2010-12-24 2013-02-08 Eads Europ Aeronautic Defence STRUCTURAL PIECE WITH CAPACITY OF ENERGY DISSIPATION
US10099765B2 (en) * 2012-08-08 2018-10-16 The Boeing Company Monolithic composite structures for vehicles
EP2905228B1 (en) * 2014-02-06 2018-01-03 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Fuselage Airframe and Tank

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3401189A1 (en) * 1983-01-25 1984-07-26 Westland PLC, Yeovil, Somerset COMPOSITE HELICOPTER FUSELAGE
US4593870A (en) * 1983-09-09 1986-06-10 Bell Helicopter Textron Inc. Energy absorbing composite aircraft structure
US4734146A (en) 1986-03-31 1988-03-29 Rockwell International Corporation Method of producing a composite sine wave beam
FR2632604B1 (en) 1988-06-08 1991-07-12 Aerospatiale FRAME OF COMPOSITE MATERIAL IN PARTICULAR FOR AIRCRAFT FUSELAGE, AND METHOD FOR MANUFACTURING SAME
US5069318A (en) 1989-12-26 1991-12-03 Mcdonnell Douglas Corporation Self-stabilized stepped crashworthy stiffeners
US6620484B1 (en) * 2000-06-06 2003-09-16 The Boeing Company Variable density stitched-composite structural elements for energy absorption
US6398883B1 (en) * 2000-06-07 2002-06-04 The Boeing Company Friction stir grain refinement of structural members
US20020178583A1 (en) 2001-03-14 2002-12-05 Holman Wrenn P. Modular monolithic bulkhead panel

Also Published As

Publication number Publication date
FR2903961A1 (en) 2008-01-25

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Effective date: 20140602

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