IL133435A0 - Heat resistant composite structure - Google Patents
Heat resistant composite structureInfo
- Publication number
- IL133435A0 IL133435A0 IL13343598A IL13343598A IL133435A0 IL 133435 A0 IL133435 A0 IL 133435A0 IL 13343598 A IL13343598 A IL 13343598A IL 13343598 A IL13343598 A IL 13343598A IL 133435 A0 IL133435 A0 IL 133435A0
- Authority
- IL
- Israel
- Prior art keywords
- heat resistant
- composite structure
- resistant composite
- heat
- resistant
- Prior art date
Links
- 239000002131 composite material Substances 0.000 title 1
Classifications
-
- 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
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/34—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
- B29C70/342—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation using isostatic pressure
-
- 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
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
-
- 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
- B64D7/00—Arrangements of military equipment, e.g. armaments, armament accessories, or military shielding, in aircraft; Adaptations of armament mountings for aircraft
-
- C—CHEMISTRY; METALLURGY
- C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
- C09K—MATERIALS FOR MISCELLANEOUS APPLICATIONS, NOT PROVIDED FOR ELSEWHERE
- C09K21/00—Fireproofing materials
- C09K21/14—Macromolecular materials
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2995/00—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
- B29K2995/0012—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds having particular thermal properties
- B29K2995/0016—Non-flammable or resistant to heat
-
- 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
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Organic Chemistry (AREA)
- Aviation & Aerospace Engineering (AREA)
- Composite Materials (AREA)
- Mechanical Engineering (AREA)
- Laminated Bodies (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US87357097A | 1997-06-12 | 1997-06-12 | |
PCT/US1998/010211 WO1998056574A1 (en) | 1997-06-12 | 1998-05-19 | Heat resistant composite structure |
Publications (1)
Publication Number | Publication Date |
---|---|
IL133435A0 true IL133435A0 (en) | 2001-04-30 |
Family
ID=25361900
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IL13343598A IL133435A0 (en) | 1997-06-12 | 1998-05-19 | Heat resistant composite structure |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP0988144A1 (en) |
AU (1) | AU8656398A (en) |
IL (1) | IL133435A0 (en) |
WO (1) | WO1998056574A1 (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5084575A (en) * | 1987-07-31 | 1992-01-28 | American Home Products Corporation | Quinoline substituted naphthalenepropionic acid derivatives as anti-inflammatory/antiallergic agents |
US4960892A (en) * | 1988-06-10 | 1990-10-02 | American Home Products Corporation | Naphthalenepropionic acid derivatives as anti-inflammatory/anti-allergic agents |
GB2447848B (en) * | 2007-03-22 | 2011-06-15 | Richard Kenneth Mcainsh | Laminate material and method of making the same |
CN112265347A (en) * | 2020-09-18 | 2021-01-26 | 航天特种材料及工艺技术研究所 | Structural bearing-ablation heat-proof integrated composite material and preparation method thereof |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5122226A (en) * | 1987-08-12 | 1992-06-16 | United Technologies Corporation | Method of making hybrid composite structures of fiber reinforced glass and resin matrices |
US5558932A (en) * | 1994-09-22 | 1996-09-24 | Auto-Air Composites, Inc. | Integrated structural composite and ceramic flame barrier |
US5582784A (en) * | 1995-08-16 | 1996-12-10 | Northrop Grumman Corporation | Method of making ceramic matrix composite/ceramic foam panels |
US5804306A (en) * | 1996-11-27 | 1998-09-08 | Northrop Grumman Corporation | Ceramic matrix composite/organic matrix composite hybrid fire shield |
-
1998
- 1998-05-19 IL IL13343598A patent/IL133435A0/en unknown
- 1998-05-19 AU AU86563/98A patent/AU8656398A/en not_active Abandoned
- 1998-05-19 WO PCT/US1998/010211 patent/WO1998056574A1/en not_active Application Discontinuation
- 1998-05-19 EP EP98937933A patent/EP0988144A1/en not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
EP0988144A1 (en) | 2000-03-29 |
AU8656398A (en) | 1998-12-30 |
WO1998056574A1 (en) | 1998-12-17 |
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