FR1075260A - Perfectionnements apportés aux installations avec turbines à gaz - Google Patents

Perfectionnements apportés aux installations avec turbines à gaz

Info

Publication number
FR1075260A
FR1075260A FR1075260DA FR1075260A FR 1075260 A FR1075260 A FR 1075260A FR 1075260D A FR1075260D A FR 1075260DA FR 1075260 A FR1075260 A FR 1075260A
Authority
FR
France
Prior art keywords
installations
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
English (en)
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.)
Power Jets Research and Development Ltd
Original Assignee
Power Jets Research and Development Ltd
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 Power Jets Research and Development Ltd filed Critical Power Jets Research and Development Ltd
Application granted granted Critical
Publication of FR1075260A publication Critical patent/FR1075260A/fr
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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34—Feeding into different combustion zones
    • F23R3/346—Feeding into different combustion zones for staged combustion
    • 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
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow

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)
FR1075260D 1952-01-17 1953-01-09 Perfectionnements apportés aux installations avec turbines à gaz Expired FR1075260A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1414/52A GB723015A (en) 1952-01-17 1952-01-17 Improvements in or relating to gas turbine plant

Publications (1)

Publication Number Publication Date
FR1075260A true FR1075260A (fr) 1954-10-14

Family

ID=9721609

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1075260D Expired FR1075260A (fr) 1952-01-17 1953-01-09 Perfectionnements apportés aux installations avec turbines à gaz

Country Status (3)

Country Link
US (1) US2704440A (fr)
FR (1) FR1075260A (fr)
GB (1) GB723015A (fr)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB703002A (en) * 1951-02-14 1954-01-27 Rolls Royce Improvements in or relating to gas turbines
US3153319A (en) * 1952-07-25 1964-10-20 Young Alec David Jet noise suppression means
DE1029196B (de) * 1955-10-01 1958-04-30 Messerschmitt Boelkow Blohm Ringbrennkammer fuer Brennkraft-Turbinen, insbesondere Flugzeug-Brennkraft-Turbinen
US3011311A (en) * 1955-10-24 1961-12-05 Williams Res Corp Gas turbine
FR1141587A (fr) * 1956-01-23 1957-09-04 Snecma Perfectionnements aux dispositifs de combustion des machines à combustion interne à flux continu
US3182453A (en) * 1956-03-26 1965-05-11 Power Jets Res & Dev Ltd Combustion system
US2974488A (en) * 1956-11-27 1961-03-14 Snecma Combustion devices for continuous-flow internal combustion machines
US2974487A (en) * 1957-10-19 1961-03-14 Bristol Siddeley Engines Ltd Combustion system for a gas turbine engine
US3048376A (en) * 1958-04-09 1962-08-07 Curtiss Wright Corp Fluid mixing apparatus
US3289413A (en) * 1964-08-19 1966-12-06 Gen Electric Fluid mixing apparatus for turbofan engines
US3999378A (en) * 1974-01-02 1976-12-28 General Electric Company Bypass augmentation burner arrangement for a gas turbine engine
US4199936A (en) * 1975-12-24 1980-04-29 The Boeing Company Gas turbine engine combustion noise suppressor
US4733538A (en) * 1978-10-02 1988-03-29 General Electric Company Combustion selective temperature dilution
US4825640A (en) * 1987-06-22 1989-05-02 Sundstrand Corporation Combustor with enhanced turbine nozzle cooling
US8904799B2 (en) * 2009-05-25 2014-12-09 Majed Toqan Tangential combustor with vaneless turbine for use on gas turbine engines
US8707708B2 (en) * 2010-02-22 2014-04-29 United Technologies Corporation 3D non-axisymmetric combustor liner
US10634354B2 (en) 2011-08-11 2020-04-28 Beckett Gas, Inc. Combustor
WO2013023127A1 (fr) * 2011-08-11 2013-02-14 Beckett Gas, Inc. Brûleur
US20150159877A1 (en) * 2013-12-06 2015-06-11 General Electric Company Late lean injection manifold mixing system
US11067277B2 (en) * 2016-10-07 2021-07-20 General Electric Company Component assembly for a gas turbine engine

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2563744A (en) * 1942-03-06 1951-08-07 Lockheed Aircraft Corp Gas turbine power plant having internal cooling means
US2588532A (en) * 1943-05-12 1952-03-11 Allis Chalmers Mfg Co Jet propulsion unit
BE463919A (fr) * 1943-11-05
US2565308A (en) * 1945-01-17 1951-08-21 Research Corp Combustion chamber with conical air diffuser
US2625792A (en) * 1947-09-10 1953-01-20 Rolls Royce Flame tube having telescoping walls with fluted ends to admit air
US2603948A (en) * 1947-10-31 1952-07-22 Mims Lisso Stewart Multistage gas turbine blade cooling with air in high-pressure turbine stages

Also Published As

Publication number Publication date
US2704440A (en) 1955-03-22
GB723015A (en) 1955-02-02

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