GB733485A - Combustion chambers for prime movers - Google Patents

Combustion chambers for prime movers

Info

Publication number
GB733485A
GB733485A GB1240552A GB1240552A GB733485A GB 733485 A GB733485 A GB 733485A GB 1240552 A GB1240552 A GB 1240552A GB 1240552 A GB1240552 A GB 1240552A GB 733485 A GB733485 A GB 733485A
Authority
GB
United Kingdom
Prior art keywords
plates
overlapping
combustion chamber
rings
air passages
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
GB1240552A
Inventor
Squire Ronald Jackson
John Stanley Clarke
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
Lucas Industries Ltd
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 Lucas Industries Ltd, Joseph Lucas Industries Ltd filed Critical Lucas Industries Ltd
Priority to GB1240552A priority Critical patent/GB733485A/en
Publication of GB733485A publication Critical patent/GB733485A/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
    • F23R3/10—Air inlet arrangements for primary air
    • 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
    • F23R3/10—Air inlet arrangements for primary air
    • F23R3/12—Air inlet arrangements for primary air inducing a vortex
    • F23R3/14—Air inlet arrangements for primary air inducing a vortex by using swirl vanes

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)

Abstract

733,485. Generating combustion products under pressure. LUCAS (INDUSTRIES), Ltd., J. Aug. 10, 1953 [May 16, 1952], No. 12405/52. Class 51 (1). In a combustion chamber for a gas turbine or jet propulsion engine, the end wall of the flame tube comprises at least in part ari imbricated construction formed from overlapping plates spaced apart to form air passages between them. In the annular combustion chamber shown in Figs. 1 and 3, an annular arrangement of overlapping plates f provides air passages g between the plates. The rear edges of the plates fare attached, as by spot-welding, to the corrugated edges of adjacent rings h. The rings h overlap to provide air passages i; they may be replaced by rings of overlapping plates similar to the plates f. Figs. 5 and 6 show a cylindrical combustion chamber in which each overlapping plate f has a tongue j by which it is secured, as by spotwelding, to the adjacent part of the end wall of the flame tube. An air nozzle k may be arranged within the plates f.
GB1240552A 1952-05-16 1952-05-16 Combustion chambers for prime movers Expired GB733485A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1240552A GB733485A (en) 1952-05-16 1952-05-16 Combustion chambers for prime movers

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1240552A GB733485A (en) 1952-05-16 1952-05-16 Combustion chambers for prime movers

Publications (1)

Publication Number Publication Date
GB733485A true GB733485A (en) 1955-07-13

Family

ID=10003985

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1240552A Expired GB733485A (en) 1952-05-16 1952-05-16 Combustion chambers for prime movers

Country Status (1)

Country Link
GB (1) GB733485A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1097213B (en) * 1958-05-22 1961-01-12 Rolls Royce Incinerator for gas turbine engines
US10386071B2 (en) 2015-08-13 2019-08-20 Pratt & Whitney Canada Corp. Combustor shape cooling system

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1097213B (en) * 1958-05-22 1961-01-12 Rolls Royce Incinerator for gas turbine engines
US10386071B2 (en) 2015-08-13 2019-08-20 Pratt & Whitney Canada Corp. Combustor shape cooling system

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