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CH510234A - Brennkammer, insbesondere für ein Gasturbinentriebwerk - Google Patents

Brennkammer, insbesondere für ein Gasturbinentriebwerk

Info

Publication number
CH510234A
CH510234A CH413070A CH413070A CH510234A CH 510234 A CH510234 A CH 510234A CH 413070 A CH413070 A CH 413070A CH 413070 A CH413070 A CH 413070A CH 510234 A CH510234 A CH 510234A
Authority
CH
Switzerland
Prior art keywords
combustion chamber
gas turbine
turbine engine
engine
combustion
Prior art date
Application number
CH413070A
Other languages
English (en)
Inventor
Goldberg Perry
Segalman Irwin
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 CH510234A publication Critical patent/CH510234A/de

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)
CH413070A 1969-04-02 1970-03-18 Brennkammer, insbesondere für ein Gasturbinentriebwerk CH510234A (de)

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
CH510234A true CH510234A (de) 1971-07-15

Family

ID=25210645

Family Applications (1)

Application Number Title Priority Date Filing Date
CH413070A CH510234A (de) 1969-04-02 1970-03-18 Brennkammer, insbesondere für ein Gasturbinentriebwerk

Country Status (7)

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

Also Published As

Publication number Publication date
BE748072A (fr) 1970-08-31
NL7004577A (de) 1970-10-06
FR2042278A5 (de) 1971-02-05
AU1230670A (en) 1971-09-16
IL33999A0 (en) 1970-07-19
DE2012950A1 (de) 1970-10-08

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Legal Events

Date Code Title Description
PL Patent ceased