FR2869565B1 - Protection d'une structure composite aux impacts - Google Patents
Protection d'une structure composite aux impactsInfo
- Publication number
- FR2869565B1 FR2869565B1 FR0404533A FR0404533A FR2869565B1 FR 2869565 B1 FR2869565 B1 FR 2869565B1 FR 0404533 A FR0404533 A FR 0404533A FR 0404533 A FR0404533 A FR 0404533A FR 2869565 B1 FR2869565 B1 FR 2869565B1
- Authority
- FR
- France
- Prior art keywords
- protecting
- composite structure
- impacts
- core
- protective layer
- 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
- 239000002131 composite material Substances 0.000 title abstract 3
- 239000011241 protective layer Substances 0.000 abstract 2
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B25/00—Layered products comprising a layer of natural or synthetic rubber
- B32B25/04—Layered products comprising a layer of natural or synthetic rubber comprising rubber as the main or only constituent of a layer, which is next to another layer of the same or of a different material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B15/06—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of natural rubber or synthetic rubber
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F1/00—Springs
- F16F1/36—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers
- F16F1/373—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers characterised by having a particular shape
- F16F1/3737—Planar, e.g. in sheet form
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F7/00—Vibration-dampers; Shock-absorbers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F7/00—Vibration-dampers; Shock-absorbers
- F16F7/12—Vibration-dampers; Shock-absorbers using plastic deformation of members
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/56—Damping, energy absorption
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2605/00—Vehicles
- B32B2605/18—Aircraft
-
- 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
- B64C2001/0054—Fuselage structures substantially made from particular materials
- B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0404533A FR2869565B1 (fr) | 2004-04-28 | 2004-04-28 | Protection d'une structure composite aux impacts |
US11/116,443 US7565778B2 (en) | 2004-04-28 | 2005-04-28 | Composite protection for revealing damage to a core in a vehicle such as an aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0404533A FR2869565B1 (fr) | 2004-04-28 | 2004-04-28 | Protection d'une structure composite aux impacts |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2869565A1 FR2869565A1 (fr) | 2005-11-04 |
FR2869565B1 true FR2869565B1 (fr) | 2007-08-10 |
Family
ID=34946820
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0404533A Expired - Fee Related FR2869565B1 (fr) | 2004-04-28 | 2004-04-28 | Protection d'une structure composite aux impacts |
Country Status (2)
Country | Link |
---|---|
US (1) | US7565778B2 (fr) |
FR (1) | FR2869565B1 (fr) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP5255831B2 (ja) * | 2007-12-27 | 2013-08-07 | 株式会社デルタツーリング | 衝撃吸収構造体、シェル型フレーム部材及び座席構造 |
PL2138348T3 (pl) * | 2008-06-24 | 2013-09-30 | Fiat Ricerche | Korpus podtrzymujący fotela samochodowego |
FR2933331B1 (fr) * | 2008-07-04 | 2015-04-10 | Astrium Sas | Dispositif de protection de structures composites contre les impacts |
EP2504231B1 (fr) * | 2009-11-23 | 2017-03-15 | LORD Corporation | Palier élastomère stratifié à haute capacité d'aéronef à voilure tournante |
US9068621B1 (en) | 2010-11-23 | 2015-06-30 | Lord Corporation | Rotary wing aircraft bearing for rotary wing aircraft motions |
WO2011062639A2 (fr) * | 2009-11-23 | 2011-05-26 | Lord Corporation | Palier d'aéronef à ailes rotatives pour mouvements d'aéronef à ailes rotatives |
HU3823U (en) * | 2010-03-11 | 2010-08-30 | Gubas Gabi | Safety airplane seat |
FR2964941B1 (fr) | 2010-09-16 | 2013-03-08 | Eurocopter France | Pale a vulnerabilite minimisee |
US9091073B2 (en) * | 2012-12-10 | 2015-07-28 | Brad Wells | Method and apparatus for temporary surface protection |
CN106965728B (zh) * | 2017-04-01 | 2023-05-23 | 安道拓(重庆)汽车部件有限公司 | 一种轻量化汽车座椅 |
EP3575071A1 (fr) | 2018-05-30 | 2019-12-04 | Crompton Technology Group Limited | Composants composites |
US11827333B2 (en) * | 2019-04-30 | 2023-11-28 | Textron Innovations Inc. | Object impact protection for an aircraft |
US11149581B2 (en) * | 2019-11-22 | 2021-10-19 | Rolls-Royce Plc | Turbine engine component with overstress indicator |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2242002B (en) * | 1990-03-13 | 1994-01-19 | Hideyuki Tada | Laminated rubber support assembly |
CA2145794A1 (fr) * | 1995-01-05 | 1996-07-06 | James Alfred Ii Benzing | Methode et appareil pour couper un stratifie d'elastomere renforce d'un cable |
US5947918A (en) * | 1996-11-18 | 1999-09-07 | Gore Enterprise Holdings, Inc. | Impact energy absorbing composite materials |
AUPP361898A0 (en) * | 1998-05-20 | 1998-06-11 | Starlon Pty Ltd | Extrusion |
DE19909675B4 (de) * | 1999-03-05 | 2005-07-14 | Mtu Aero Engines Gmbh | Schichtstruktur und Verfahren zu ihrer Herstellung |
US6586066B1 (en) * | 2000-03-21 | 2003-07-01 | Awi Licensing Company | Preglued underlayment composite and associated flooring installation system |
US7081300B2 (en) * | 2001-01-22 | 2006-07-25 | Formica Corporation | Decorative laminate assembly and method of producing same |
ITTO20020213A1 (it) * | 2002-03-12 | 2003-09-12 | Agusta Spa | Metodo di formatura di una pala per un rotore di un elicottero. |
DE10228902B4 (de) * | 2002-06-27 | 2005-04-21 | Db Cargo Ag | Blattfeder mit mehreren Schichten aus unterschiedlichen hochpolymeren Werkstoffen |
DE10340561A1 (de) * | 2002-09-09 | 2004-03-18 | Eurocopter Deutschland Gmbh | Leichtbau-Verbundmaterial, Zwischenprodukt für ein derartiges Leichtbau-Verbundmaterial, Verfahren zur Herstellung und Bearbeitung des Leichtbau-Verbundmaterials, sowie Verwendung für das Leichtbau-Verbundmaterial |
US7161056B2 (en) * | 2005-01-28 | 2007-01-09 | Ossur Hf | Wound dressing and method for manufacturing the same |
-
2004
- 2004-04-28 FR FR0404533A patent/FR2869565B1/fr not_active Expired - Fee Related
-
2005
- 2005-04-28 US US11/116,443 patent/US7565778B2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
US7565778B2 (en) | 2009-07-28 |
FR2869565A1 (fr) | 2005-11-04 |
US20050248191A1 (en) | 2005-11-10 |
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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: 13 |
|
PLFP | Fee payment |
Year of fee payment: 14 |
|
PLFP | Fee payment |
Year of fee payment: 15 |
|
PLFP | Fee payment |
Year of fee payment: 16 |
|
PLFP | Fee payment |
Year of fee payment: 17 |
|
ST | Notification of lapse |
Effective date: 20211205 |