FR1006338A - Improvements to gas turbines - Google Patents

Improvements to gas turbines

Info

Publication number
FR1006338A
FR1006338A FR1006338DA FR1006338A FR 1006338 A FR1006338 A FR 1006338A FR 1006338D A FR1006338D A FR 1006338DA FR 1006338 A FR1006338 A FR 1006338A
Authority
FR
France
Prior art keywords
gas turbines
turbines
gas
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
Other languages
French (fr)
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.)
Compagnie Electro Mecanique SA
Original Assignee
Compagnie Electro Mecanique SA
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 Compagnie Electro Mecanique SA filed Critical Compagnie Electro Mecanique SA
Application granted granted Critical
Publication of FR1006338A publication Critical patent/FR1006338A/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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/46—Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings
    • 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34—Feeding into different combustion zones

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR1006338D 1947-12-20 1947-12-20 Improvements to gas turbines Expired FR1006338A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1006338T 1947-12-20

Publications (1)

Publication Number Publication Date
FR1006338A true FR1006338A (en) 1952-04-22

Family

ID=9565669

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1006338D Expired FR1006338A (en) 1947-12-20 1947-12-20 Improvements to gas turbines

Country Status (3)

Country Link
DE (1) DE811055C (en)
FR (1) FR1006338A (en)
GB (1) GB656930A (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE943440C (en) * 1953-01-25 1956-05-17 Habil Fritz A F Schmidt Dr Ing Exhaust control from intermittently working combustion chambers for aircraft jet engines, pulso engines or gas turbines
BE529689A (en) * 1953-06-18
US3018624A (en) * 1954-03-02 1962-01-30 Bristol Siddeley Engines Ltd Flame tubes for use in combustion systems of gas turbine engines
DE1032033B (en) * 1956-07-12 1958-06-12 Plessey Co Ltd Ram air turbine as a power source for auxiliary equipment in a gas turbine aircraft
US3096080A (en) * 1959-10-30 1963-07-02 Willems Peter Apparatus for generating oscillations in fluid
US3174283A (en) * 1963-06-28 1965-03-23 Crocco Luigi Expendable barrier
US3371480A (en) * 1966-06-16 1968-03-05 United Aircraft Corp One and one-half stage split turbine construction

Also Published As

Publication number Publication date
DE811055C (en) 1951-08-16
GB656930A (en) 1951-09-05

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