GB736823A - Engine combustion chambers - Google Patents

Engine combustion chambers

Info

Publication number
GB736823A
GB736823A GB1463/53A GB146353A GB736823A GB 736823 A GB736823 A GB 736823A GB 1463/53 A GB1463/53 A GB 1463/53A GB 146353 A GB146353 A GB 146353A GB 736823 A GB736823 A GB 736823A
Authority
GB
United Kingdom
Prior art keywords
air
flame tube
nozzles
fuel
jan
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
GB1463/53A
Inventor
Squire Ronald Jackson
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 GB1463/53A priority Critical patent/GB736823A/en
Priority to US414741A priority patent/US2807139A/en
Priority to DEL18237A priority patent/DE961672C/en
Priority to FR1095756D priority patent/FR1095756A/en
Publication of GB736823A publication Critical patent/GB736823A/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
    • 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
    • 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
    • F23R3/045—Air inlet arrangements using pipes

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gas Burners (AREA)
  • Nozzles For Spraying Of Liquid Fuel (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)

Abstract

736,823. Generating combustion products under pressure. LUCAS (INDUSTRIES), Ltd., J. Jan. 18, 1954 [Jan. 19, 1953], No. 1463/53. Class 51 (1). In an annular air-jacketed type of combustion chamber for a jet propulsion engine or gas turbine engine, comprising an annular flame tube a, b mounted between inner and outer casing walls c, d, a number of equi-spaced fuel nozzles f being disposed in the inlet end wall of the flame tube, oppositely-inclined air nozzles k, n are provided in the inner and outer walls of the flame tube between the fuel nozzles, the air nozzles producing a swirling ring of air around each of the fuel jets. The end wall of the flame tube is formed of a number of segmental parts e. Each plate is formed with a frusto-conical dished recess and has air swirling vanes g disposed around the fuel injector f. Air inlets j, m are provided in the inner and outer walls of the flame tube and the air nozzles k, n project through the inlets.
GB1463/53A 1953-01-19 1953-01-19 Engine combustion chambers Expired GB736823A (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
GB1463/53A GB736823A (en) 1953-01-19 1953-01-19 Engine combustion chambers
US414741A US2807139A (en) 1953-01-19 1954-03-08 Air-jacketed combustion chambers for jet propulsion engines, gas turbines and the like
DEL18237A DE961672C (en) 1953-01-19 1954-03-11 Annular combustion chamber for jet engines, gas turbines or the like.
FR1095756D FR1095756A (en) 1953-01-19 1954-03-16 Engine combustion chamber

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1463/53A GB736823A (en) 1953-01-19 1953-01-19 Engine combustion chambers

Publications (1)

Publication Number Publication Date
GB736823A true GB736823A (en) 1955-09-14

Family

ID=9722419

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1463/53A Expired GB736823A (en) 1953-01-19 1953-01-19 Engine combustion chambers

Country Status (4)

Country Link
US (1) US2807139A (en)
DE (1) DE961672C (en)
FR (1) FR1095756A (en)
GB (1) GB736823A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0676590A1 (en) * 1994-04-08 1995-10-11 ROLLS-ROYCE plc Gas turbine engine combustion apparatus
GB2589885A (en) * 2019-12-11 2021-06-16 Rolls Royce Plc Combustor

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1199541B (en) * 1961-12-04 1965-08-26 Jan Jerie Dr Ing Propellant gas collector for the stator of gas turbines
US4301657A (en) * 1978-05-04 1981-11-24 Caterpillar Tractor Co. Gas turbine combustion chamber
DE4242650A1 (en) * 1992-12-17 1994-06-23 Asea Brown Boveri Gas turbine combustion chamber
FR2748088B1 (en) * 1996-04-24 1998-05-29 Snecma OPTIMIZATION OF THE MIXTURE OF BURNED GASES IN AN ANNULAR COMBUSTION CHAMBER
US20090090110A1 (en) * 2007-10-04 2009-04-09 Honeywell International, Inc. Faceted dome assemblies for gas turbine engine combustors
US8141365B2 (en) * 2009-02-27 2012-03-27 Honeywell International Inc. Plunged hole arrangement for annular rich-quench-lean gas turbine combustors
US8171740B2 (en) * 2009-02-27 2012-05-08 Honeywell International Inc. Annular rich-quench-lean gas turbine combustors with plunged holes

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB583211A (en) * 1940-01-24 1946-12-12 Anglo Saxon Petroleum Co Improved process and apparatus for the continuous generation of gases by reaction between air and liquid or pulverulent combustible material
GB578764A (en) * 1942-09-08 1946-07-11 Rover Co Ltd Improvements relating to combustion chambers for internal combustion turbines
GB595831A (en) * 1944-03-16 1947-12-18 Power Jets Ltd Improvements relating to combustion apparatus
BE468999A (en) * 1944-11-28
US2517015A (en) * 1945-05-16 1950-08-01 Bendix Aviat Corp Combustion chamber with shielded fuel nozzle
US2531810A (en) * 1946-06-05 1950-11-28 Kellogg M W Co Air inlet arrangement for combustion chamber flame tubes
US2488911A (en) * 1946-11-09 1949-11-22 Surface Combustion Corp Combustion apparatus for use with turbines
US2541171A (en) * 1947-01-25 1951-02-13 Kellogg M W Co Air inlet structure for combustion chambers
NL74196C (en) * 1947-08-11
US2607193A (en) * 1947-10-25 1952-08-19 Curtiss Wright Corp Annular combustion chamber with multiple notched fuel nozzles
US2671314A (en) * 1950-01-26 1954-03-09 Socony Vacuum Oil Co Inc Gas turbine and method of operation therefor
FR1025198A (en) * 1950-09-27 1953-04-13 Continuous combustion chamber and explosive waves
GB715909A (en) * 1952-02-01 1954-09-22 Rolls Royce Improvements in or relating to combustion equipment of gas-turbine engines
FR1052475A (en) * 1952-03-15 1954-01-25 Snecma Combustion chambers particularly suitable for gas turbines

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0676590A1 (en) * 1994-04-08 1995-10-11 ROLLS-ROYCE plc Gas turbine engine combustion apparatus
US5590530A (en) * 1994-04-08 1997-01-07 Rolls-Royce Plc Fuel and air mixing parts for a turbine combustion chamber
GB2589885A (en) * 2019-12-11 2021-06-16 Rolls Royce Plc Combustor

Also Published As

Publication number Publication date
US2807139A (en) 1957-09-24
FR1095756A (en) 1955-06-06
DE961672C (en) 1957-04-11

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