IL33995A0 - Wall structure and method of manufacturing it - Google Patents

Wall structure and method of manufacturing it

Info

Publication number
IL33995A0
IL33995A0 IL33995A IL3399570A IL33995A0 IL 33995 A0 IL33995 A0 IL 33995A0 IL 33995 A IL33995 A IL 33995A IL 3399570 A IL3399570 A IL 3399570A IL 33995 A0 IL33995 A0 IL 33995A0
Authority
IL
Israel
Prior art keywords
manufacturing
wall structure
wall
Prior art date
Application number
IL33995A
Other languages
English (en)
Original Assignee
United Aircraft 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 United Aircraft Corp filed Critical United Aircraft Corp
Publication of IL33995A0 publication Critical patent/IL33995A0/xx

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/005Combined with pressure or heat exchangers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/08Cooling; Heating; Heat-insulation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/78Other construction of jet pipes
    • F02K1/82Jet pipe walls, e.g. liners
    • F02K1/822Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infrared radiation suppressors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/002Wall structures
    • 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
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
IL33995A 1969-04-02 1970-03-03 Wall structure and method of manufacturing it IL33995A0 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US81260769A 1969-04-02 1969-04-02

Publications (1)

Publication Number Publication Date
IL33995A0 true IL33995A0 (en) 1970-05-21

Family

ID=25210105

Family Applications (1)

Application Number Title Priority Date Filing Date
IL33995A IL33995A0 (en) 1969-04-02 1970-03-03 Wall structure and method of manufacturing it

Country Status (6)

Country Link
AU (1) AU1230370A (fr)
BE (1) BE748069A (fr)
DE (1) DE2012947A1 (fr)
FR (1) FR2038152A1 (fr)
IL (1) IL33995A0 (fr)
NL (1) NL7004576A (fr)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4033381A (en) * 1975-06-27 1977-07-05 General Connectors Corporation Hot air duct
DE3003347A1 (de) * 1979-12-20 1981-06-25 BBC AG Brown, Boveri & Cie., Baden, Aargau Gekuehlte wand
FR2478259A1 (fr) * 1980-03-17 1981-09-18 Snecma Element metallique allege etanche de construction mecanique
EP0273073A1 (fr) * 1986-12-30 1988-07-06 Stirling Engine Associates Echangeur thermique
US4934600A (en) * 1988-12-14 1990-06-19 General Electric Company Exhaust nozzle thermal distortion control device
US5724816A (en) * 1996-04-10 1998-03-10 General Electric Company Combustor for a gas turbine with cooling structure
US5933699A (en) * 1996-06-24 1999-08-03 General Electric Company Method of making double-walled turbine components from pre-consolidated assemblies
US11619387B2 (en) * 2015-07-28 2023-04-04 Rolls-Royce Corporation Liner for a combustor of a gas turbine engine with metallic corrugated member

Also Published As

Publication number Publication date
BE748069A (fr) 1970-08-31
DE2012947A1 (de) 1970-11-05
FR2038152A1 (en) 1971-01-08
NL7004576A (fr) 1970-10-06
AU1230370A (en) 1971-09-16

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