FR2902689B1 - Panneau raidi a raidisseurs composites a sensibilite aux chocs diminuee - Google Patents
Panneau raidi a raidisseurs composites a sensibilite aux chocs diminueeInfo
- Publication number
- FR2902689B1 FR2902689B1 FR0652584A FR0652584A FR2902689B1 FR 2902689 B1 FR2902689 B1 FR 2902689B1 FR 0652584 A FR0652584 A FR 0652584A FR 0652584 A FR0652584 A FR 0652584A FR 2902689 B1 FR2902689 B1 FR 2902689B1
- Authority
- FR
- France
- Prior art keywords
- core
- structural part
- skin
- coating
- placing
- 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 2
- 230000035945 sensitivity Effects 0.000 title 1
- 230000035939 shock Effects 0.000 title 1
- 239000011248 coating agent Substances 0.000 abstract 5
- 238000000576 coating method Methods 0.000 abstract 5
- 239000003351 stiffener Substances 0.000 abstract 4
- 238000000034 method Methods 0.000 abstract 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
- B64C1/12—Construction or attachment of skin panels
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/68—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
- B29C70/86—Incorporated in coherent impregnated reinforcing layers, e.g. by winding
- B29C70/865—Incorporated in coherent impregnated reinforcing layers, e.g. by winding completely encapsulated
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/88—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced
- B29C70/887—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced locally reinforced, e.g. by fillers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
- B29D99/00—Subject matter not provided for in other groups of this subclass
- B29D99/001—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings
- B29D99/0014—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings provided with ridges or ribs, e.g. joined ribs
-
- 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
- B64C1/064—Stringers; Longerons
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/26—Construction, shape, or attachment of separate skins, e.g. panels
-
- 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
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2007/00—Flat articles, e.g. films or sheets
- B29L2007/002—Panels; Plates; Sheets
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Laminated Bodies (AREA)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0652584A FR2902689B1 (fr) | 2006-06-22 | 2006-06-22 | Panneau raidi a raidisseurs composites a sensibilite aux chocs diminuee |
US11/766,177 US7814729B2 (en) | 2006-06-22 | 2007-06-21 | Stiff panel having composite stiffeners with reduced shock sensitivity |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0652584A FR2902689B1 (fr) | 2006-06-22 | 2006-06-22 | Panneau raidi a raidisseurs composites a sensibilite aux chocs diminuee |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2902689A1 FR2902689A1 (fr) | 2007-12-28 |
FR2902689B1 true FR2902689B1 (fr) | 2008-08-22 |
Family
ID=37682654
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0652584A Expired - Fee Related FR2902689B1 (fr) | 2006-06-22 | 2006-06-22 | Panneau raidi a raidisseurs composites a sensibilite aux chocs diminuee |
Country Status (2)
Country | Link |
---|---|
US (1) | US7814729B2 (fr) |
FR (1) | FR2902689B1 (fr) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8551382B2 (en) † | 2008-05-28 | 2013-10-08 | The Boeing Company | Modified blade stiffener and fabrication method therefor |
ES2382765B1 (es) * | 2009-06-29 | 2013-05-03 | Airbus Operations, S.L. | Diseño de cuadernas de aeronave |
US9340319B2 (en) | 2011-11-09 | 2016-05-17 | Norduyn Inc. | Cargo pallet and method of manufacture thereof |
FR2986989B1 (fr) * | 2012-02-17 | 2014-02-28 | Airbus Operations Sas | Procede et dispositif de protection de raidisseurs, ainsi que panneau composite correspondant |
EP2700574B1 (fr) | 2012-08-22 | 2016-08-17 | Airbus Operations GmbH | Réduction de charge passive pour caisson central à fibres renforcées d'un avion ayant une structure de coque rigide |
ES2566168T3 (es) * | 2012-12-28 | 2016-04-11 | Airbus Operations, S.L. | Estructura aeronáutica con elementos de refuerzo integrados |
US9719489B2 (en) | 2013-05-22 | 2017-08-01 | General Electric Company | Wind turbine rotor blade assembly having reinforcement assembly |
FI127614B (en) * | 2017-04-07 | 2018-10-15 | Patria Aerostructures Oy | COMPOSITE ELEMENT AND METHOD FOR MANUFACTURING IT |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1385217A (en) * | 1920-04-13 | 1921-07-19 | Henry M Lutz | Glazing-clip |
GB794166A (en) * | 1956-08-29 | 1958-04-30 | Robert Herrington Nichol | Improvements in or relating to the reinforcement of fibre glass boat hulls, or otherbodies of a like flexible nature, made from a plastic material |
FR1251327A (fr) * | 1959-12-07 | 1961-01-20 | Procédé de renforcement de structures en matières plastiques et structures obtenues à l'aide de ce procédé | |
US3207057A (en) * | 1962-09-07 | 1965-09-21 | Donn Prod Inc | Panel supporting grid |
US3995081A (en) * | 1974-10-07 | 1976-11-30 | General Dynamics Corporation | Composite structural beams and method |
US4554718A (en) * | 1984-06-04 | 1985-11-26 | Armstrong World Industries, Inc. | Method of reinforcing a ceiling runner |
US5306068A (en) * | 1991-08-30 | 1994-04-26 | Toray Industries Inc. | Automobile door |
US5325647A (en) * | 1992-08-21 | 1994-07-05 | Armstrong World Industries, Inc. | Composite ceiling grid |
AUPN323895A0 (en) * | 1995-05-29 | 1995-06-22 | Hatziathanasiou, Terry | Multi-width canopy |
GB9709776D0 (en) * | 1997-05-15 | 1997-07-09 | Ultraframe Plc | Structural members |
US6443513B1 (en) * | 1998-07-02 | 2002-09-03 | Concept Analysis Corporation | Cup bumper absorber |
ES2185443B1 (es) * | 2000-03-07 | 2004-09-01 | Airbus España S.L. | Procedimiento de fabricacion de piezas precuradas en material compuesto con rigidizadores aplicados en estado fresco. |
US6553734B1 (en) * | 2000-08-24 | 2003-04-29 | Lockheed Martin Corporation | Composite structural panel with undulated body |
FR2824801B1 (fr) * | 2001-05-15 | 2003-09-12 | Sofitec Sa | Panneau d'etancheite et d'isolation acoustique, en particulier pour porte de vehicule automobile |
EP1552081B1 (fr) * | 2002-09-03 | 2008-04-02 | Corus Bausysteme GmbH | Element de retenue de forme allongee |
US6883858B2 (en) * | 2002-09-10 | 2005-04-26 | L & L Products, Inc. | Structural reinforcement member and method of use therefor |
-
2006
- 2006-06-22 FR FR0652584A patent/FR2902689B1/fr not_active Expired - Fee Related
-
2007
- 2007-06-21 US US11/766,177 patent/US7814729B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
US20080010942A1 (en) | 2008-01-17 |
US7814729B2 (en) | 2010-10-19 |
FR2902689A1 (fr) | 2007-12-28 |
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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: 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 |
|
ST | Notification of lapse |
Effective date: 20220205 |