GB685062A - Improvements relating to combustion chambers for jet engines, gas turbines or the like - Google Patents

Improvements relating to combustion chambers for jet engines, gas turbines or the like

Info

Publication number
GB685062A
GB685062A GB33486/49A GB3348649A GB685062A GB 685062 A GB685062 A GB 685062A GB 33486/49 A GB33486/49 A GB 33486/49A GB 3348649 A GB3348649 A GB 3348649A GB 685062 A GB685062 A GB 685062A
Authority
GB
United Kingdom
Prior art keywords
air
passages
closed
flame tube
adjacent
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
GB33486/49A
Inventor
John Stanley Clarke
Geoffrey John Hudson
Alfred Huyton
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 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 Ltd filed Critical Joseph Lucas Ltd
Priority to GB33486/49A priority Critical patent/GB685062A/en
Publication of GB685062A publication Critical patent/GB685062A/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
    • F23R3/02—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)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

685,062. Generating combustion products under pressure. LUCAS, Ltd., J. Dec. 27, 1950 [Dec. 31, 1949], No. 33486/49. Class 51 (i). In an air jacketed type of combustion chamber for use in jet propulsion engines or gas turbines, the flame tube is constructed from sheet metal sections a and has parts which are shaped to form between them an annular air passage or passages closed at one end, lateral air admission orifices being formed adjacent the closed end. In Fig. 1, the downstream end f of each flame tube section a is disposed within the adjacent section so as to form annular air passages g and lateral air admission orifices hare formed adjacent the closed upstream ends of the passages through which air enters from the surrounding air jacket. In Fig. 3, the air passages g are formed between separately-formed rings and the section of the flame tube, the lateral air admission orifices h being disposed adjacent the closed upstream ends of the air passages as before.
GB33486/49A 1949-12-31 1949-12-31 Improvements relating to combustion chambers for jet engines, gas turbines or the like Expired GB685062A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB33486/49A GB685062A (en) 1949-12-31 1949-12-31 Improvements relating to combustion chambers for jet engines, gas turbines or the like

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB33486/49A GB685062A (en) 1949-12-31 1949-12-31 Improvements relating to combustion chambers for jet engines, gas turbines or the like

Publications (1)

Publication Number Publication Date
GB685062A true GB685062A (en) 1952-12-31

Family

ID=10353592

Family Applications (1)

Application Number Title Priority Date Filing Date
GB33486/49A Expired GB685062A (en) 1949-12-31 1949-12-31 Improvements relating to combustion chambers for jet engines, gas turbines or the like

Country Status (1)

Country Link
GB (1) GB685062A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1131947B (en) * 1959-03-28 1962-06-20 Maschf Augsburg Nuernberg Ag Combustion process for gas turbine combustion chambers and equipment for carrying out the process
US3995422A (en) * 1975-05-21 1976-12-07 General Electric Company Combustor liner structure

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1131947B (en) * 1959-03-28 1962-06-20 Maschf Augsburg Nuernberg Ag Combustion process for gas turbine combustion chambers and equipment for carrying out the process
US3995422A (en) * 1975-05-21 1976-12-07 General Electric Company Combustor liner structure

Similar Documents

Publication Publication Date Title
GB584820A (en) Improvements relating to internal combustion prime movers
GB680371A (en) Reheater for jet propulsion engines
GB723015A (en) Improvements in or relating to gas turbine plant
GB588847A (en) Improvements in combustion chambers for internal combustion turbines
GB676473A (en) Improvements in or relating to combustion chambers
GB703002A (en) Improvements in or relating to gas turbines
GB1116930A (en) Improvements in cooled flameholder assembly
GB587083A (en) Improvements in combustion chambers for internal combustion turbines
GB757332A (en) Liquid fuel combustion chambers for jet-propulsion, engines, gas turbines, or other purposes
GB685062A (en) Improvements relating to combustion chambers for jet engines, gas turbines or the like
GB616481A (en) Improvements in or relating to ignition systems for gas turbines
GB699251A (en) Sheet metal combustion chambers, flame tubes and other like tubular bodies
GB662764A (en) Improvements relating to combustion chambers for jet-engines or gas turbines
GB891826A (en) Improvements relating to flame-supporting devices for combustion chambers
GB697027A (en) Combustion chambers for prime movers
GB741488A (en) Combustion chambers for jet-propulsion engines, gas turbines and other prime movers
GB694484A (en) Improvements relating to combustion equipment for gas turbine engines
GB761167A (en) Flame spreading device for combustion systems
GB700017A (en) Combustion chambers for prime movers
GB710589A (en) Combustion chambers for jet engines or gas turbines
GB743149A (en) Liquid fuel combustion chambers for prime movers
GB682778A (en) Improvements relating to combustion chambers for prime movers
GB700705A (en) Combustion chambers for jet propulsion engines, gas turbines or other prime movers
GB702752A (en) Improvements relating to combustion equipment of gas turbine engines
GB576545A (en) Improvements relating to combustion chambers for prime movers