DE3481290D1 - Kompositmaterialstruktur mit vollem feuerschutz. - Google Patents
Kompositmaterialstruktur mit vollem feuerschutz.Info
- Publication number
- DE3481290D1 DE3481290D1 DE8484901642T DE3481290T DE3481290D1 DE 3481290 D1 DE3481290 D1 DE 3481290D1 DE 8484901642 T DE8484901642 T DE 8484901642T DE 3481290 T DE3481290 T DE 3481290T DE 3481290 D1 DE3481290 D1 DE 3481290D1
- Authority
- DE
- Germany
- Prior art keywords
- composite material
- fire protection
- material structure
- full fire
- full
- 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
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
- B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form
- B32B3/10—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
- B32B3/12—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
-
- 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
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/12—Layered products comprising a layer of synthetic resin next to a fibrous or filamentary layer
-
- 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
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/28—Layered products comprising a layer of synthetic resin comprising synthetic resins not wholly covered by any one of the sub-groups B32B27/30 - B32B27/42
- B32B27/281—Layered products comprising a layer of synthetic resin comprising synthetic resins not wholly covered by any one of the sub-groups B32B27/30 - B32B27/42 comprising polyimides
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04B—GENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
- E04B1/00—Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
- E04B1/62—Insulation or other protection; Elements or use of specified material therefor
- E04B1/92—Protection against other undesired influences or dangers
- E04B1/94—Protection against other undesired influences or dangers against fire
- E04B1/941—Building elements specially adapted therefor
-
- 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
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/105—Ceramic fibres
-
- 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
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/106—Carbon fibres, e.g. graphite fibres
-
- 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
- B32B2305/00—Condition, form or state of the layers or laminate
- B32B2305/02—Cellular or porous
- B32B2305/024—Honeycomb
-
- 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
- B32B2307/30—Properties of the layers or laminate having particular thermal properties
- B32B2307/306—Resistant to heat
- B32B2307/3065—Flame resistant or retardant, fire resistant or retardant
-
- 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
- B32B2379/00—Other polymers having nitrogen, with or without oxygen or carbon only, in the main chain
- B32B2379/08—Polyimides
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S428/00—Stock material or miscellaneous articles
- Y10S428/902—High modulus filament or fiber
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S428/00—Stock material or miscellaneous articles
- Y10S428/92—Fire or heat protection feature
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24149—Honeycomb-like
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/30—Self-sustaining carbon mass or layer with impregnant or other layer
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/31504—Composite [nonstructural laminate]
- Y10T428/31551—Of polyamidoester [polyurethane, polyisocyanate, polycarbamate, etc.]
- Y10T428/31623—Next to polyamide or polyimide
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/31504—Composite [nonstructural laminate]
- Y10T428/31721—Of polyimide
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T442/00—Fabric [woven, knitted, or nonwoven textile or cloth, etc.]
- Y10T442/30—Woven fabric [i.e., woven strand or strip material]
- Y10T442/3472—Woven fabric including an additional woven fabric layer
- Y10T442/3504—Woven fabric layers comprise chemically different strand material
- Y10T442/3512—Three or more fabric layers
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/US1984/000023 WO1985003032A1 (en) | 1984-01-09 | 1984-01-09 | Composite material structure with integral fire protection |
Publications (1)
Publication Number | Publication Date |
---|---|
DE3481290D1 true DE3481290D1 (de) | 1990-03-15 |
Family
ID=22181999
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE8484901642T Expired - Fee Related DE3481290D1 (de) | 1984-01-09 | 1984-01-09 | Kompositmaterialstruktur mit vollem feuerschutz. |
Country Status (4)
Country | Link |
---|---|
US (1) | US4767656A (de) |
EP (1) | EP0167533B1 (de) |
DE (1) | DE3481290D1 (de) |
WO (1) | WO1985003032A1 (de) |
Families Citing this family (96)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4801496A (en) * | 1986-06-24 | 1989-01-31 | The Boeing Company | Composite member with integrated thermal protection |
US4868050A (en) * | 1987-02-27 | 1989-09-19 | Ube Industries, Ltd. | Interleaf-containing, fiber-reinforced epoxy resin prepreg |
DE3872911T2 (de) * | 1987-03-31 | 1992-12-03 | Asahi Chemical Ind | Gewebe mit mehrschichtenaufbau und ein derartiges gewebe enthaltender verbundwerkstoff. |
US4844960A (en) * | 1987-04-14 | 1989-07-04 | B & B Progressive Materials And Technologies, Inc. | Time determinate fire protection blanket |
DE3713466A1 (de) * | 1987-04-22 | 1988-11-10 | Messerschmitt Boelkow Blohm | Transportflugzeug |
US5251917A (en) * | 1987-06-22 | 1993-10-12 | The Boeing Company | Fire-resistant seal |
GB8728887D0 (en) * | 1987-12-10 | 1988-01-27 | Ici Plc | Fibre reinforced thermoplastic composite structures |
US4921745A (en) * | 1987-12-25 | 1990-05-01 | Ube Industries, Ltd. | Honeycomb structure of aromatic polyimide |
JPH01192536A (ja) * | 1988-01-27 | 1989-08-02 | Ube Ind Ltd | ポリイミド製ハニカムコア及びその製造法 |
US4915998A (en) * | 1988-08-24 | 1990-04-10 | International Fuel Cells Corporation | Thermal insulation blanket |
DE3829712A1 (de) * | 1988-09-01 | 1990-03-15 | Basf Ag | Temperaturbestaendige thermoplastische formmassen |
US5092948A (en) * | 1989-01-03 | 1992-03-03 | The Regents Of The Univ, Of California | Fiber reinforced laminated ceramic composites and method thereof |
US5219642A (en) * | 1989-06-09 | 1993-06-15 | Imperial Chemical Industries Plc | Fibre reinforced stuctural thermoplastic composite materials |
US5143790A (en) * | 1989-08-09 | 1992-09-01 | Westinghouse Electric Corp. | Integrally-damped steel composite laminated structure and method of attaching same |
DE4030626A1 (de) * | 1989-09-27 | 1991-05-29 | Klaus Rennebeck | Verfahren zur herstellung eines halbzeugs |
US5080306A (en) * | 1989-10-10 | 1992-01-14 | General Dynamics Corporation, Space Systems Division | Multi-layer stitched blanket insulation |
WO1992017331A1 (en) * | 1991-04-04 | 1992-10-15 | Lincoln James D | Unidirectional carbon/phenolic prepreg material and method of manufacture |
US5418050A (en) * | 1991-04-05 | 1995-05-23 | Ici Composites Inc. | Fire/heat barrier laminates |
GB9107766D0 (en) * | 1991-04-12 | 1991-06-05 | Short Brothers Plc | A structural component |
US5222769A (en) * | 1992-02-26 | 1993-06-29 | Kaempen Charles E | Double-wall composite pipe and coupling structure assembly |
WO1993019912A1 (en) * | 1992-04-02 | 1993-10-14 | Akro Fireguard Products, Inc. | Aircraft fuselage flame barrier |
US5338383A (en) * | 1992-05-06 | 1994-08-16 | Aerojet General Corporation | Tank insulation method with cryogenic exposure |
US5340520A (en) * | 1992-06-10 | 1994-08-23 | Beech Aircraft Corp. | Non-woven mat surface ply for woven fabric |
LU88149A1 (de) * | 1992-07-15 | 1994-04-01 | Euro Composites | Leichtbauplattenstruktur fuer Bodenpaneele |
JPH06173772A (ja) | 1992-08-10 | 1994-06-21 | Boeing Co:The | 逆推進装置内壁およびそのサンドイッチ構造 |
ES2155470T3 (es) * | 1993-02-08 | 2001-05-16 | Thermal Science Inc | Sistema protector termico reforzado. |
US5514444A (en) * | 1994-06-17 | 1996-05-07 | Hexcel Corporation | Fiber reinforced polyimide honeycomb for high temperature applications |
US5624726A (en) * | 1995-01-09 | 1997-04-29 | Minnesota Mining And Manufacturing Company | Insulation blanket |
US5626951A (en) * | 1995-04-03 | 1997-05-06 | Rockwell International Corporation | Thermal insulation system and method of forming thereof |
US5522198A (en) * | 1995-04-20 | 1996-06-04 | Byer; Gary M. | Method of using a woven carbon fabric to protect houses, persons and other structures from flames and heat |
US5753271A (en) * | 1995-08-18 | 1998-05-19 | Northrop Grumman Corporation | Heat blanket buffer assembly |
US6036464A (en) * | 1995-08-18 | 2000-03-14 | Northrop Grumman Corporation | Heat blanket buffer assembly |
FR2745746A1 (fr) * | 1996-03-05 | 1997-09-12 | Sade Compagnie Generale De Tra | Materiau composite pour le chemisage de canalisations |
US5804306A (en) * | 1996-11-27 | 1998-09-08 | Northrop Grumman Corporation | Ceramic matrix composite/organic matrix composite hybrid fire shield |
US5958583A (en) * | 1996-12-20 | 1999-09-28 | The Boeing Company | Alumina-based protective coating for ceramic materials |
US6205728B1 (en) * | 1997-04-30 | 2001-03-27 | Frank Sutelan | Laminated composite building component |
US5928752A (en) * | 1997-06-30 | 1999-07-27 | The Boeing Company | Quick installation-removal thermal insulation blanket for space craft |
US6114003A (en) * | 1997-09-04 | 2000-09-05 | No Fire Technologies, Inc. | Insulation blanket having an inner metal core air cell and adjoining outer insulation layers |
FR2780135B1 (fr) * | 1998-06-18 | 2000-08-25 | Philec Sa | Protection thermique formant bouclier thermique |
US6592981B1 (en) | 1998-08-07 | 2003-07-15 | Lockheed Martin Corporation | Oxidation resistant insulating sandwich tiles |
US6558785B1 (en) | 1998-08-07 | 2003-05-06 | Lockheed Martin Corporation | Insulated reentry heat shield |
US6224020B1 (en) * | 1998-12-24 | 2001-05-01 | Alliant Techsystems, Inc. | Payload fairing with improved acoustic suppression |
US6264369B1 (en) * | 1999-01-29 | 2001-07-24 | General Electric Company | Variable vane seal and washer materials |
JP2000343476A (ja) * | 1999-06-09 | 2000-12-12 | Nippon Mitsubishi Oil Corp | 搬送用部材 |
AU1429901A (en) * | 1999-07-22 | 2001-02-13 | Lockheed Martin Corporation | Oxidation resistant insulating sandwich tiles |
US9586699B1 (en) | 1999-08-16 | 2017-03-07 | Smart Drilling And Completion, Inc. | Methods and apparatus for monitoring and fixing holes in composite aircraft |
US7732358B2 (en) * | 2000-09-20 | 2010-06-08 | Goodrich Corporation | Inorganic matrix compositions and composites incorporating the matrix composition |
US6966945B1 (en) * | 2000-09-20 | 2005-11-22 | Goodrich Corporation | Inorganic matrix compositions, composites and process of making the same |
US20080063875A1 (en) * | 2000-09-20 | 2008-03-13 | Robinson John W | High heat distortion resistant inorganic laminate |
US20050031843A1 (en) * | 2000-09-20 | 2005-02-10 | Robinson John W. | Multi-layer fire barrier systems |
US7094285B2 (en) * | 2000-09-20 | 2006-08-22 | Goodrich Corporation | Inorganic matrix compositions, composites incorporating the matrix, and process of making the same |
US6969422B2 (en) * | 2000-09-20 | 2005-11-29 | Goodrich Corporation | Inorganic matrix composition and composites incorporating the matrix composition |
US6503596B1 (en) | 2000-11-30 | 2003-01-07 | Michael L. Fellman | Composite firewall structure |
US6481960B2 (en) | 2001-03-30 | 2002-11-19 | General Electric Co. | Variable gas turbine compressor vane structure with sintered-and-infiltrated bushing and washer bearings |
JP3732126B2 (ja) * | 2001-08-06 | 2006-01-05 | 川崎重工業株式会社 | 熱防御構造体 |
US9625361B1 (en) | 2001-08-19 | 2017-04-18 | Smart Drilling And Completion, Inc. | Methods and apparatus to prevent failures of fiber-reinforced composite materials under compressive stresses caused by fluids and gases invading microfractures in the materials |
US6815037B2 (en) * | 2001-09-19 | 2004-11-09 | Nippon Mitsubishi Oil Corporation | Carrier member made of a UV resistant fiber-reinforced composite material and process for producing thereof |
US6712318B2 (en) * | 2001-11-26 | 2004-03-30 | The Boeing Company | Impact resistant surface insulation tile for a space vehicle and associated protection method |
US6698149B1 (en) * | 2002-01-29 | 2004-03-02 | Paragon Building Systems, Inc. | Composite laminated building material, and methods of making and using same |
US6863980B2 (en) * | 2002-10-08 | 2005-03-08 | The Boeing Company | Monolithic composite firewall |
US6764754B1 (en) | 2003-07-15 | 2004-07-20 | The Boeing Company | Composite material with improved damping characteristics and method of making same |
DE102004001081B4 (de) * | 2004-01-05 | 2013-02-14 | Airbus Operations Gmbh | Isolationsaufbau zur Innenisolierung eines Fahrzeuges |
DE102004001080A1 (de) | 2004-01-05 | 2005-08-04 | Airbus Deutschland Gmbh | Anordnung zur Innenverkleidung einer Passagierkabine eines Flugzeuges |
US7284726B2 (en) * | 2004-02-17 | 2007-10-23 | Sikorsky Aircraft Corporation | Self extinguishing composite primary structure |
US20070267545A1 (en) * | 2005-04-18 | 2007-11-22 | Orr James R | Asset protection method and apparatus |
ITRE20060154A1 (it) * | 2006-12-19 | 2008-06-20 | Ufi Filters Spa | Materiale composito stratificato e relativo metodo di realizzazione |
US7919167B1 (en) | 2006-12-19 | 2011-04-05 | Lockheed Martin Corporation | Carbon-phenolic ablator monoliths and their methods of manufacture |
US9511571B2 (en) * | 2007-01-23 | 2016-12-06 | The Boeing Company | Composite laminate having a damping interlayer and method of making the same |
US8070895B2 (en) | 2007-02-12 | 2011-12-06 | United States Gypsum Company | Water resistant cementitious article and method for preparing same |
US7980057B2 (en) * | 2007-05-21 | 2011-07-19 | Raytheon Company | Integral composite rocket motor dome/nozzle structure |
US20090022579A1 (en) * | 2007-07-17 | 2009-01-22 | Schlichting Kevin W | Burn resistant organic matrix composite material |
ITRM20070501A1 (it) * | 2007-09-27 | 2009-03-28 | Nautical Service Srl | Pannello in materiali compositi resistente alla fiamma passante per applicazioni aero, navali e terrestri e suoi sistemi di bloccaggio. |
US7927686B2 (en) * | 2007-10-11 | 2011-04-19 | The Boeing Company | Composite heat shield |
US20090165926A1 (en) * | 2007-10-24 | 2009-07-02 | United Technologies Corporation | Method and assembly for bonding metal layers in a gas turbine engine using a polyimide adhesive |
US8128100B2 (en) * | 2007-12-05 | 2012-03-06 | United Technologies Corporation | Laminate air seal for a gas turbine engine |
DE102007062082A1 (de) * | 2007-12-21 | 2009-07-23 | Airbus Deutschland Gmbh | Kernverbundstruktur |
US8163379B2 (en) | 2007-12-21 | 2012-04-24 | Airbus Deutschland Gmbh | Sandwich structure |
DE102008016104A1 (de) * | 2008-03-28 | 2009-10-08 | Airbus Deutschland Gmbh | Durchbrandsicherer Flugzeugrumpf |
US7874109B2 (en) * | 2008-07-30 | 2011-01-25 | Honeywell International Inc. | Fireproof panels and methods of fabricating the same |
US8222165B2 (en) * | 2008-10-27 | 2012-07-17 | Pratt & Whitney Canada Corp. | Composite fire shield |
US8425710B2 (en) * | 2009-03-13 | 2013-04-23 | The Boeing Company | Automated placement of vibration damping materials |
US8329308B2 (en) | 2009-03-31 | 2012-12-11 | United States Gypsum Company | Cementitious article and method for preparing the same |
US8146298B2 (en) * | 2009-04-28 | 2012-04-03 | Pelefiregard Llc | Fire-resistant structures, fire-resistant insulations and a method for fire-protection |
ITMI20112399A1 (it) | 2011-12-28 | 2013-06-29 | Silcart S P A | Pannello isolante da costruzione e relativo metodo di fabbricazione |
GB2505871A (en) * | 2012-07-20 | 2014-03-19 | Williams Grand Prix Eng | Flame or heat resistant material comprising ceramic and carbon layers |
US8733500B1 (en) | 2012-11-12 | 2014-05-27 | Hexcel Corporation | Acoustic structure with internal thermal regulators |
FR3014840B1 (fr) | 2013-12-17 | 2017-10-13 | Airbus Operations Sas | Ensemble pour aeronef comprenant un corps d'attache moteur equipe d'au moins une ferrure de support de manille penetrant dans le caisson du mat d'accrochage |
FR3014841B1 (fr) | 2013-12-17 | 2017-12-08 | Airbus Operations Sas | Ensemble pour aeronef comprenant un corps d'attache moteur en partie realise d'une seule piece avec une nervure interieure de rigidification d'un caisson de mat d'accrochage |
FR3015431B1 (fr) * | 2013-12-19 | 2017-12-15 | Airbus Operations Sas | Structure primaire de mat d'accrochage renforcee. |
FR3015433B1 (fr) | 2013-12-23 | 2016-02-12 | Airbus Operations Sas | Ensemble pour aeronef comprenant un mat d'accrochage integre a la nacelle et agence en partie arriere du fuselage |
US20170080264A1 (en) * | 2014-05-05 | 2017-03-23 | Alonso P. Rodriguez | Methods and compositions for enhanced reinforcement for refractory fire containment walls |
US20160211495A1 (en) * | 2015-01-20 | 2016-07-21 | Williams Grand Prix Engineering Limited | Fire guards and materials therefor |
EP3271243B1 (de) | 2015-03-16 | 2021-07-14 | Daher Aerospace | Verfahren und vorrichtung zum feuerfestmachen eines verbundstoffteils |
US10195819B1 (en) | 2016-02-02 | 2019-02-05 | Fred D Donnelly | Multilayer ceramic composite and method of production |
US10508810B2 (en) | 2017-09-19 | 2019-12-17 | Hexcel Corporation | Thermal panel with a corrugated ceramic composite sheet having unequal ridge widths |
CN114044124A (zh) * | 2021-11-25 | 2022-02-15 | 江西九由航空装备有限公司 | 航空发动机舱壁复合材料整流罩高性能专用隔热件 |
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US2551115A (en) * | 1950-01-06 | 1951-05-01 | Daniel And Florence Guggenheim | Hollow partition between premixing and combustion chambers for rockets |
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US4495764A (en) * | 1983-05-26 | 1985-01-29 | The United States Of America As Represented By The Secretary Of The Air Force | Integrated insulation wall assembly |
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US4579782A (en) * | 1985-05-31 | 1986-04-01 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Laminate comprising fibers embedded in cured amine terminated bis-imide |
-
1984
- 1984-01-09 EP EP84901642A patent/EP0167533B1/de not_active Expired - Lifetime
- 1984-01-09 US US06/573,976 patent/US4767656A/en not_active Expired - Fee Related
- 1984-01-09 WO PCT/US1984/000023 patent/WO1985003032A1/en active IP Right Grant
- 1984-01-09 DE DE8484901642T patent/DE3481290D1/de not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
US4767656A (en) | 1988-08-30 |
WO1985003032A1 (en) | 1985-07-18 |
EP0167533A1 (de) | 1986-01-15 |
EP0167533B1 (de) | 1990-02-07 |
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