GB1037923A - Combustion chamber for a gas turbine - Google Patents

Combustion chamber for a gas turbine

Info

Publication number
GB1037923A
GB1037923A GB23689/64A GB2368964A GB1037923A GB 1037923 A GB1037923 A GB 1037923A GB 23689/64 A GB23689/64 A GB 23689/64A GB 2368964 A GB2368964 A GB 2368964A GB 1037923 A GB1037923 A GB 1037923A
Authority
GB
United Kingdom
Prior art keywords
flame tube
primary
gas turbine
holes
combustion chamber
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
GB23689/64A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of GB1037923A publication Critical patent/GB1037923A/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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/54—Reverse-flow combustion chambers

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

1,037,923. Gas turbine combustion chambers. G. BAYARD. June 8, 1964 [Dec. 9, 1963], No. 23689. Heading F1L. An annular gas turbine reverse flow combustion chamber flame tube comprises spaced walls 1, 2 joined at the upstream end of the flame tube by an annulus 5. Annular indentations 3, 4 in walls 1, 2 respectively form a reduced area section 11 dividing the flame tube into primary and secondary zones 9, 10. Primary air enters zone 9 from annular channel 15 through holes 26, 27 and secondary air enters zone 10 through holes 28. Fuel injectors 22 and igniters 24 mounted on support 13 project into primary zone 9. Partitions 29, 30 shroud the injectors and igniters. Holes 26 in the region of partitions 29, 30 are formed so as to slow down the primary airflow. Adjustable abutments 17, 18 support the flame tube within engine outer casing 12.
GB23689/64A 1963-12-09 1964-06-08 Combustion chamber for a gas turbine Expired GB1037923A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR4934A FR1388005A (en) 1963-12-09 1963-12-09 Gas turbine combustion chamber

Publications (1)

Publication Number Publication Date
GB1037923A true GB1037923A (en) 1966-08-03

Family

ID=8570510

Family Applications (1)

Application Number Title Priority Date Filing Date
GB23689/64A Expired GB1037923A (en) 1963-12-09 1964-06-08 Combustion chamber for a gas turbine

Country Status (3)

Country Link
US (1) US3287905A (en)
FR (1) FR1388005A (en)
GB (1) GB1037923A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2871418B1 (en) 2013-11-11 2015-10-21 Rolls-Royce Deutschland Ltd & Co KG Gas turbine combustion chamber and method for its manufacture

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3902314A (en) * 1973-11-29 1975-09-02 Avco Corp Gas turbine engine frame structure
US4018043A (en) * 1975-09-19 1977-04-19 Avco Corporation Gas turbine engines with toroidal combustors
GB1600130A (en) * 1977-05-21 1981-10-14 Rolls Royce Combustion systems
US4845941A (en) * 1986-11-07 1989-07-11 Paul Marius A Gas turbine engine operating process
US5058375A (en) * 1988-12-28 1991-10-22 Sundstrand Corporation Gas turbine annular combustor with radial dilution air injection
US5140808A (en) * 1989-03-17 1992-08-25 Sundstrand Corporation Gas turbine engine with fuel mainfold system
US5033263A (en) * 1989-03-17 1991-07-23 Sundstrand Corporation Compact gas turbine engine
US5048298A (en) * 1989-07-10 1991-09-17 Sundstrand Corporation Low cost fuel system for a gas turbine engine
US5109671A (en) * 1989-12-05 1992-05-05 Allied-Signal Inc. Combustion apparatus and method for a turbine engine
US5363644A (en) * 1989-12-21 1994-11-15 Sundstrand Corporation Annular combustor
US20070245710A1 (en) * 2006-04-21 2007-10-25 Honeywell International, Inc. Optimized configuration of a reverse flow combustion system for a gas turbine engine
US20120023964A1 (en) * 2010-07-27 2012-02-02 Carsten Ralf Mehring Liquid-fueled premixed reverse-flow annular combustor for a gas turbine engine
WO2024019723A1 (en) * 2022-07-21 2024-01-25 Raytheon Technologies Corporation Electrolysis energy recovery

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2296023A (en) * 1941-03-03 1942-09-15 Northrop Aircraft Inc Burner
US2633705A (en) * 1946-03-30 1953-04-07 John Hawkins And Associates Re Segmentally separable gas turbine power plant
GB721899A (en) * 1952-03-06 1955-01-12 Lucas Industries Ltd Liquid fuel combustion apparatus for jet-propulsion engines or gas turbines
BE535905A (en) * 1954-02-23
US3088278A (en) * 1957-05-01 1963-05-07 Avco Mfg Corp Gas turbine engine
GB863011A (en) * 1957-12-20 1961-03-15 Constuction De Moteurs D Aviat Burner device for continuous-flow internal combustion engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2871418B1 (en) 2013-11-11 2015-10-21 Rolls-Royce Deutschland Ltd & Co KG Gas turbine combustion chamber and method for its manufacture

Also Published As

Publication number Publication date
FR1388005A (en) 1965-02-05
US3287905A (en) 1966-11-29

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