BE748069A - Structure de paroi et methode pour sa fabrication - Google Patents

Structure de paroi et methode pour sa fabrication

Info

Publication number
BE748069A
BE748069A BE748069DA BE748069A BE 748069 A BE748069 A BE 748069A BE 748069D A BE748069D A BE 748069DA BE 748069 A BE748069 A BE 748069A
Authority
BE
Belgium
Prior art keywords
manufacturing
wall structure
wall
Prior art date
Application number
Other languages
English (en)
Inventor
P Goldberg
I Segalman
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 BE748069A publication Critical patent/BE748069A/fr

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
    • F23R3/005—Combined with pressure or heat exchangers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/08—Cooling; Heating; Heat-insulation
    • 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
    • F02K1/822—Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infrared radiation suppressors
    • 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
    • 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
    • Y02T50/60—Efficient 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)
BE748069D 1969-04-02 1970-03-27 Structure de paroi et methode pour sa fabrication BE748069A (fr)

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
BE748069A true BE748069A (fr) 1970-08-31

Family

ID=25210105

Family Applications (1)

Application Number Title Priority Date Filing Date
BE748069D BE748069A (fr) 1969-04-02 1970-03-27 Structure de paroi et methode pour sa fabrication

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
NL7004576A (fr) 1970-10-06
AU1230370A (en) 1971-09-16
DE2012947A1 (de) 1970-11-05
FR2038152A1 (en) 1971-01-08
IL33995A0 (en) 1970-05-21

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