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 ELEMENTSInfo
- 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
Links
- 238000004519 manufacturing process Methods 0.000 title 1
- 238000000034 method Methods 0.000 title 1
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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Laminated Bodies (AREA)
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 (6)
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 |
CN112389676A (en) * | 2020-12-02 | 2021-02-23 | 江汉大学 | Many rotor unmanned aerial vehicle carry on platform and unmanned aerial vehicle |
Family Cites Families (8)
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 |
-
2006
- 2006-07-21 FR FR0606703A patent/FR2903961B1/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
FR2903961A1 (en) | 2008-01-25 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
CD | Change of name or company name |
Owner name: AIRBUS HELICOPTERS, FR Effective date: 20140602 |
|
PLFP | Fee payment |
Year of fee payment: 11 |
|
PLFP | Fee payment |
Year of fee payment: 12 |
|
PLFP | Fee payment |
Year of fee payment: 13 |
|
PLFP | Fee payment |
Year of fee payment: 15 |
|
PLFP | Fee payment |
Year of fee payment: 16 |
|
ST | Notification of lapse |
Effective date: 20230305 |