FR2538507B1 - PROCESS FOR THE MANUFACTURE OF AN ABLATION LAYER CROSSED BY A MAT - Google Patents

PROCESS FOR THE MANUFACTURE OF AN ABLATION LAYER CROSSED BY A MAT

Info

Publication number
FR2538507B1
FR2538507B1 FR8320374A FR8320374A FR2538507B1 FR 2538507 B1 FR2538507 B1 FR 2538507B1 FR 8320374 A FR8320374 A FR 8320374A FR 8320374 A FR8320374 A FR 8320374A FR 2538507 B1 FR2538507 B1 FR 2538507B1
Authority
FR
France
Prior art keywords
mat
manufacture
ablation layer
layer crossed
crossed
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
Application number
FR8320374A
Other languages
French (fr)
Other versions
FR2538507A1 (en
Inventor
Peter Goedtke
Heinz Huber
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of FR2538507A1 publication Critical patent/FR2538507A1/en
Application granted granted Critical
Publication of FR2538507B1 publication Critical patent/FR2538507B1/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/002—Wall structures
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
    • B23K35/22—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
    • B23K35/24—Selection of soldering or welding materials proper
    • B23K35/30—Selection of soldering or welding materials proper with the principal constituent melting at less than 1550 degrees C
    • B23K35/3033—Ni as the principal constituent
    • B23K35/304—Ni as the principal constituent with Cr as the next major constituent
    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/78—Other construction of jet pipes
    • F02K1/82—Jet pipe walls, e.g. liners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32—Constructional parts; Details not otherwise provided for
    • F02K9/34—Casings; Combustion chambers; Liners thereof
    • F02K9/346—Liners, e.g. inhibitors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/97—Rocket nozzles
    • F02K9/974—Nozzle- linings; Ablative coatings
FR8320374A 1982-12-22 1983-12-20 PROCESS FOR THE MANUFACTURE OF AN ABLATION LAYER CROSSED BY A MAT Expired FR2538507B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3247414A DE3247414C2 (en) 1982-12-22 1982-12-22 Process for the production of an ablation layer interspersed with a mat

Publications (2)

Publication Number Publication Date
FR2538507A1 FR2538507A1 (en) 1984-06-29
FR2538507B1 true FR2538507B1 (en) 1988-10-14

Family

ID=6181360

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8320374A Expired FR2538507B1 (en) 1982-12-22 1983-12-20 PROCESS FOR THE MANUFACTURE OF AN ABLATION LAYER CROSSED BY A MAT

Country Status (2)

Country Link
DE (1) DE3247414C2 (en)
FR (1) FR2538507B1 (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2569237B1 (en) * 1984-08-14 1987-01-09 Aerospatiale ABLATION AND VIBRATION RESISTANT THERMAL PROTECTION DEVICE AND MANUFACTURING METHOD
DE4132415C1 (en) * 1991-09-28 1993-03-04 Deutsche Aerospace Ag, 8000 Muenchen, De Ablate layer for combustion chamber walls of rocket propulsion appts. - comprises silicone resin with phenyl gp(s) as matrix, high melting filler and alkaline earth carbonate
FR2740068B1 (en) * 1995-10-20 1998-01-09 Aerospatiale PART OF REINFORCED LOW DENSITY THERMAL PROTECTION MATERIAL AND PROCESS FOR OBTAINING SAME
DE19750517A1 (en) 1997-11-14 1999-05-20 Asea Brown Boveri Heat shield
DE19805402C2 (en) * 1998-02-11 2002-09-19 Deutsch Zentr Luft & Raumfahrt Method for the integral connection of components by means of a seam formed from connection material
CN100547237C (en) * 2006-03-24 2009-10-07 陈世钟 Plasma recombination boosting turbine fan jet aerial engine
CN109161889B (en) * 2018-07-19 2020-05-22 西安交通大学 Anti-sintering dual-mode composite structure thermal barrier coating and preparation process thereof

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1051405A (en) * 1950-11-07 1954-01-15 Birmingham Small Arms Co Ltd Porous metal objects
FR1186710A (en) * 1957-11-25 1959-08-31 Acetylene Dissous Du Sud Est Metal plastic compound
DE1160696B (en) * 1959-08-08 1964-01-02 Rheinmetall Gmbh Solid propellant for rockets
US3187503A (en) * 1962-05-01 1965-06-08 Bell Aerospace Corp Rocket engine construction
US3311013A (en) * 1963-01-09 1967-03-28 Aerojet General Co Propellant liner
US3427185A (en) * 1964-02-19 1969-02-11 United Aircraft Corp Composite structural material incorporating metallic filaments in a matrix,and method of manufacture
US4001475A (en) * 1974-05-09 1977-01-04 The United States Of America As Represented By The Secretary Of The Air Force Ablative surface insulator
DE3120902C1 (en) * 1981-05-26 1983-01-27 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Ablation layer and method and device for its production

Also Published As

Publication number Publication date
DE3247414C2 (en) 1986-10-23
DE3247414A1 (en) 1984-06-28
FR2538507A1 (en) 1984-06-29

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Legal Events

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ST Notification of lapse