AU4793068A - Flame tubes for gas turbine engines - Google Patents

Flame tubes for gas turbine engines

Info

Publication number
AU4793068A
AU4793068A AU47930/68A AU4793068A AU4793068A AU 4793068 A AU4793068 A AU 4793068A AU 47930/68 A AU47930/68 A AU 47930/68A AU 4793068 A AU4793068 A AU 4793068A AU 4793068 A AU4793068 A AU 4793068A
Authority
AU
Australia
Prior art keywords
gas turbine
turbine engines
flame tubes
flame
tubes
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
AU47930/68A
Inventor
ALBAN HEATON ALWIN HARRISON and SQUIRE ROGAL JACKSON KENNETH GREENWOOD
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.)
ZF International UK Ltd
Original Assignee
Joseph Lucas Industries 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 Joseph Lucas Industries Ltd filed Critical Joseph Lucas Industries Ltd
Publication of AU4793068A publication Critical patent/AU4793068A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/26Controlling the air flow
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2250/00Geometry
    • F05B2250/40Movement of component
    • F05B2250/41Movement of component with one degree of freedom
    • F05B2250/411Movement of component with one degree of freedom in rotation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00Function
    • F05B2260/70Adjusting of angle of incidence or attack of rotating blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00001Arrangements using bellows, e.g. to adjust volumes or reduce thermal stresses

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Gas Burners (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
AU47930/68A 1967-11-10 1968-12-17 Flame tubes for gas turbine engines Expired AU4793068A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB2809268A GB1256066A (en) 1967-11-10 1967-11-10 Flame tubes for gas turbine engines
GB5129367 1967-11-10

Publications (1)

Publication Number Publication Date
AU4793068A true AU4793068A (en) 1970-06-18

Family

ID=26259181

Family Applications (1)

Application Number Title Priority Date Filing Date
AU47930/68A Expired AU4793068A (en) 1967-11-10 1968-12-17 Flame tubes for gas turbine engines

Country Status (3)

Country Link
AU (1) AU4793068A (en)
FR (1) FR2028599A5 (en)
GB (1) GB1256066A (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2133832B1 (en) * 1971-04-15 1975-10-24 United Aircraft Canada
JPS4873607A (en) * 1972-01-10 1973-10-04
FR2748553B1 (en) * 1996-05-09 1998-06-19 Snecma INJECTION SYSTEM WITH VARIABLE GEOMETRY ADOPTING AIR FLOW ACCORDING TO ENGINE RPM
US8966877B2 (en) * 2010-01-29 2015-03-03 United Technologies Corporation Gas turbine combustor with variable airflow
DE102014204482A1 (en) 2014-03-11 2015-09-17 Rolls-Royce Deutschland Ltd & Co Kg Combustion chamber of a gas turbine
CN114076324B (en) * 2022-01-19 2022-07-08 中国航发四川燃气涡轮研究院 Combustion chamber capable of automatically adjusting mixed air intake

Also Published As

Publication number Publication date
FR2028599A5 (en) 1970-10-09
DE1815695A1 (en) 1970-08-13
GB1256066A (en) 1971-12-08
DE1815695B2 (en) 1976-07-15

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