IL33999A0 - Wall structure for a gas turbine engine - Google Patents

Wall structure for a gas turbine engine

Info

Publication number
IL33999A0
IL33999A0 IL33999A IL3399970A IL33999A0 IL 33999 A0 IL33999 A0 IL 33999A0 IL 33999 A IL33999 A IL 33999A IL 3399970 A IL3399970 A IL 3399970A IL 33999 A0 IL33999 A0 IL 33999A0
Authority
IL
Israel
Prior art keywords
gas turbine
turbine engine
wall structure
wall
engine
Prior art date
Application number
IL33999A
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 IL33999A0 publication Critical patent/IL33999A0/en

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
    • 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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/06—Arrangement of apertures along the flame tube
    • F23R3/08—Arrangement of apertures along the flame tube between annular flame tube sections, e.g. flame tubes with telescopic sections
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
IL33999A 1969-04-02 1970-03-03 Wall structure for a gas turbine engine IL33999A0 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US81279369A 1969-04-02 1969-04-02

Publications (1)

Publication Number Publication Date
IL33999A0 true IL33999A0 (en) 1970-07-19

Family

ID=25210645

Family Applications (1)

Application Number Title Priority Date Filing Date
IL33999A IL33999A0 (en) 1969-04-02 1970-03-03 Wall structure for a gas turbine engine

Country Status (7)

Country Link
AU (1) AU1230670A (en)
BE (1) BE748072A (en)
CH (1) CH510234A (en)
DE (1) DE2012950A1 (en)
FR (1) FR2042278A5 (en)
IL (1) IL33999A0 (en)
NL (1) NL7004577A (en)

Also Published As

Publication number Publication date
DE2012950A1 (en) 1970-10-08
NL7004577A (en) 1970-10-06
BE748072A (en) 1970-08-31
FR2042278A5 (en) 1971-02-05
AU1230670A (en) 1971-09-16
CH510234A (en) 1971-07-15

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