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GB762596A - A combustion chamber, particularly for a gas turbine engine - Google Patents

A combustion chamber, particularly for a gas turbine engine

Info

Publication number
GB762596A
GB762596A GB475254A GB475254A GB762596A GB 762596 A GB762596 A GB 762596A GB 475254 A GB475254 A GB 475254A GB 475254 A GB475254 A GB 475254A GB 762596 A GB762596 A GB 762596A
Authority
GB
United Kingdom
Prior art keywords
flame tube
combustion chamber
outer casing
spacing means
sections
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
GB475254A
Inventor
Sidney Allen
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.)
Armstrong Siddeley Motors Ltd
Original Assignee
Armstrong Siddeley Motors 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 Armstrong Siddeley Motors Ltd filed Critical Armstrong Siddeley Motors Ltd
Priority to GB475254A priority Critical patent/GB762596A/en
Publication of GB762596A publication Critical patent/GB762596A/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

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

762,596. Generating combustion products under pressure. ARMSTRONG SIDDELEY MOTORS, Ltd. Jan. 12, 1955 [Feb. 18, 1954], No. 4752/54. Class 51 (1). A combustion chamber for a gas turbine engine comprises an outer casing 10 and an inner flame tube 12, the wall of the flame tube comprising successive axially-extending sections 11 which overlap at their ends to allow cooling air to flow along the interior surfaces of the sections. The sections are spaced apart by spacing means 14 and the downstream end of each flame tube section is continued beyond the spacing means and then diverges at 16 towards the next section to such an extent that a cooling air flow of substantially constant velocity is produced. The combustion chamber in Fig. 1 comprises an annular outer casing and an annular flame tube, and the spacing means are corrugated metal strips. A second embodiment comprises a cylindrical outer casing and a tube type flame tube. Reference has been directed by the Comptroller to Specification 743,149.
GB475254A 1954-02-18 1954-02-18 A combustion chamber, particularly for a gas turbine engine Expired GB762596A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB475254A GB762596A (en) 1954-02-18 1954-02-18 A combustion chamber, particularly for a gas turbine engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB475254A GB762596A (en) 1954-02-18 1954-02-18 A combustion chamber, particularly for a gas turbine engine

Publications (1)

Publication Number Publication Date
GB762596A true GB762596A (en) 1956-11-28

Family

ID=9783111

Family Applications (1)

Application Number Title Priority Date Filing Date
GB475254A Expired GB762596A (en) 1954-02-18 1954-02-18 A combustion chamber, particularly for a gas turbine engine

Country Status (1)

Country Link
GB (1) GB762596A (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1078815B (en) * 1957-12-23 1960-03-31 Her Majesty The Queen In The R Tube holder for flame tube sections and thus produced flame tube for gas turbine engines
DE1155940B (en) * 1959-11-20 1963-10-17 Rolls Royce Combustion device for gas turbine engines
US3736747A (en) * 1971-07-09 1973-06-05 G Warren Combustor
US4184326A (en) * 1975-12-05 1980-01-22 United Technologies Corporation Louver construction for liner of gas turbine engine combustor
US4475344A (en) * 1982-02-16 1984-10-09 Westinghouse Electric Corp. Low smoke combustor for land based combustion turbines
WO1989006308A1 (en) * 1987-12-28 1989-07-13 Sundstrand Corporation Annular combustor with tangential cooling air injection
US5465572A (en) * 1991-03-11 1995-11-14 General Electric Company Multi-hole film cooled afterburner cumbustor liner
JP2007198727A (en) * 2006-01-25 2007-08-09 Rolls Royce Plc Wall elements for gas turbine engine combustors
US8024933B2 (en) 2006-01-25 2011-09-27 Rolls-Royce Plc Wall elements for gas turbine engine combustors
US8650882B2 (en) 2006-01-25 2014-02-18 Rolls-Royce Plc Wall elements for gas turbine engine combustors
CN106705075A (en) * 2016-12-12 2017-05-24 深圳智慧能源技术有限公司 Torch with forced-cooling air film

Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1078815B (en) * 1957-12-23 1960-03-31 Her Majesty The Queen In The R Tube holder for flame tube sections and thus produced flame tube for gas turbine engines
DE1155940B (en) * 1959-11-20 1963-10-17 Rolls Royce Combustion device for gas turbine engines
US3736747A (en) * 1971-07-09 1973-06-05 G Warren Combustor
US4184326A (en) * 1975-12-05 1980-01-22 United Technologies Corporation Louver construction for liner of gas turbine engine combustor
US4475344A (en) * 1982-02-16 1984-10-09 Westinghouse Electric Corp. Low smoke combustor for land based combustion turbines
WO1989006308A1 (en) * 1987-12-28 1989-07-13 Sundstrand Corporation Annular combustor with tangential cooling air injection
US4928479A (en) * 1987-12-28 1990-05-29 Sundstrand Corporation Annular combustor with tangential cooling air injection
USRE34962E (en) * 1987-12-28 1995-06-13 Sundstrand Corporation Annular combustor with tangential cooling air injection
US5465572A (en) * 1991-03-11 1995-11-14 General Electric Company Multi-hole film cooled afterburner cumbustor liner
US5483794A (en) * 1991-03-11 1996-01-16 General Electric Company Multi-hole film cooled afterburner combustor liner
JP2007198727A (en) * 2006-01-25 2007-08-09 Rolls Royce Plc Wall elements for gas turbine engine combustors
US7886541B2 (en) 2006-01-25 2011-02-15 Rolls-Royce Plc Wall elements for gas turbine engine combustors
US8024933B2 (en) 2006-01-25 2011-09-27 Rolls-Royce Plc Wall elements for gas turbine engine combustors
EP1813869A3 (en) * 2006-01-25 2013-08-14 Rolls-Royce plc Wall elements for gas turbine engine combustors
US8650882B2 (en) 2006-01-25 2014-02-18 Rolls-Royce Plc Wall elements for gas turbine engine combustors
CN106705075A (en) * 2016-12-12 2017-05-24 深圳智慧能源技术有限公司 Torch with forced-cooling air film
CN106705075B (en) * 2016-12-12 2023-12-12 深圳智慧能源技术有限公司 Forced air film cooling torch

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