IL133435A0 - Heat resistant composite structure - Google Patents

Heat resistant composite structure

Info

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
Application number
IL13343598A
Original Assignee
Northrop Grumman Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Northrop Grumman Corp filed Critical Northrop Grumman Corp
Publication of IL133435A0 publication Critical patent/IL133435A0/en

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/30Shaping 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
    • B29C70/34Shaping 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
    • B29C70/342Shaping 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D7/00Arrangements of military equipment, e.g. armaments, armament accessories, or military shielding, in aircraft; Adaptations of armament mountings for aircraft
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09KMATERIALS FOR MISCELLANEOUS APPLICATIONS, NOT PROVIDED FOR ELSEWHERE
    • C09K21/00Fireproofing materials
    • C09K21/14Macromolecular materials
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING 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
    • B29K2995/00Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
    • B29K2995/0012Properties of moulding materials, reinforcements, fillers, preformed parts or moulds having particular thermal properties
    • B29K2995/0016Non-flammable or resistant to heat
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054Fuselage structures substantially made from particular materials
    • B64C2001/0072Fuselage structures substantially made from particular materials from composite materials
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/40Weight 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)
IL13343598A 1997-06-12 1998-05-19 Heat resistant composite structure IL133435A0 (en)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

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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