GB620343A - Improvements in or relating to diffusion systems for operation in high velocity air streams - Google Patents

Improvements in or relating to diffusion systems for operation in high velocity air streams

Info

Publication number
GB620343A
GB620343A GB765/47A GB76547A GB620343A GB 620343 A GB620343 A GB 620343A GB 765/47 A GB765/47 A GB 765/47A GB 76547 A GB76547 A GB 76547A GB 620343 A GB620343 A GB 620343A
Authority
GB
United Kingdom
Prior art keywords
holes
flame tube
air
combustion chambers
stream
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
GB765/47A
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.)
Power Jets Research and Development Ltd
Original Assignee
Power Jets Research and Development 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 Power Jets Research and Development Ltd filed Critical Power Jets Research and Development Ltd
Priority claimed from US793375A external-priority patent/US2667033A/en
Publication of GB620343A publication Critical patent/GB620343A/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
    • 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
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F23R3/20—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means
    • 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)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)

Abstract

620,343. Gas-turbine combustion chambers. POWER JETS (RESEARCH & DEVELOPMENT), Ltd.; and ASHWOOD, P. F. Jan. 9, 1947, Nos. 765 and 766. [Class 51 (i)] The air stream to a combustion chamber is divided by a wall 8, the larger part passing through a diffuser passage 11 surrounding the upstream end of the flame tube 4 and the lesser part passing through perforations 16, 17, 18 in a conical member 5 into the inner region of the up-stream spray of fuel issuing from a nozzle 6, which is of the spill-controlled type. Part of the air passed through the diffuser 11 enters the flame tube 4 through holes 19 in the region of the reversal of flame direction, a further part enters the tube through holes 20 as secondary combustion air and the rest passes through holes 21 and serves as diluent air. The holes 21 may be continued into the flame tube by scoop-like parts which are open on the up-stream side. The flared end 13 of the flame tube is spaced from the duct 1. A circular arrangement of combustion chambers may be disposed in an annular ducting which provides a diffusing passage between it and the chambers and the upstream ends of the combustion chambers lie close to the compressor outlets. Specification 599,257 is referred to.
GB765/47A 1947-01-09 1947-01-09 Improvements in or relating to diffusion systems for operation in high velocity air streams Expired GB620343A (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
GB271829X 1947-01-09
US793375A US2667033A (en) 1947-01-09 1947-12-23 Combustion apparatus for operation in fast-moving air streams
US357999A US2826039A (en) 1947-01-09 1953-05-28 Gas inlet structure for combustion chambers

Publications (1)

Publication Number Publication Date
GB620343A true GB620343A (en) 1949-03-23

Family

ID=32329572

Family Applications (1)

Application Number Title Priority Date Filing Date
GB765/47A Expired GB620343A (en) 1947-01-09 1947-01-09 Improvements in or relating to diffusion systems for operation in high velocity air streams

Country Status (6)

Country Link
US (1) US2826039A (en)
BE (1) BE479471A (en)
CH (1) CH271829A (en)
FR (1) FR959791A (en)
GB (1) GB620343A (en)
NL (3) NL207253A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20160223196A1 (en) * 2015-02-02 2016-08-04 The Government Of The United States Of America, As Represented By The Secretary Of The Navy Crude Oil Spray Combustor

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1123868B (en) * 1958-08-26 1962-02-15 Schweizerische Lokomotiv Combustion chamber, especially for gas turbines
GB970189A (en) * 1963-01-31 1964-09-16 Rolls Royce Combustion equipment for a gas turbine engine
US4590769A (en) * 1981-01-12 1986-05-27 United Technologies Corporation High-performance burner construction
US5187937A (en) * 1988-06-22 1993-02-23 The Secretary Of State For Defence In Her Britannic Majesty's Government Of The United Kingdom Of Great Britain And Northern Ireland Gas turbine engine combustors
US5321947A (en) * 1992-11-10 1994-06-21 Solar Turbines Incorporated Lean premix combustion system having reduced combustion pressure oscillation
US5372008A (en) * 1992-11-10 1994-12-13 Solar Turbines Incorporated Lean premix combustor system
TWI567343B (en) * 2015-01-16 2017-01-21 國家中山科學研究院 Combustion supporting device
CN106287814B (en) * 2016-09-29 2019-04-19 南京航空航天大学 A kind of ground gas turbine can burner of axial admission

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB578764A (en) * 1942-09-08 1946-07-11 Rover Co Ltd Improvements relating to combustion chambers for internal combustion turbines
US2546432A (en) * 1944-03-20 1951-03-27 Power Jets Res & Dev Ltd Apparatus for deflecting a fuel jet towards a region of turbulence in a propulsive gaseous stream
BE489359A (en) * 1944-10-05
US2610467A (en) * 1946-04-03 1952-09-16 Westinghouse Electric Corp Combustion chamber having telescoping walls and corrugated spacers
US2448561A (en) * 1946-05-01 1948-09-07 Westinghouse Electric Corp Gas turbine apparatus
US2531810A (en) * 1946-06-05 1950-11-28 Kellogg M W Co Air inlet arrangement for combustion chamber flame tubes
US2541171A (en) * 1947-01-25 1951-02-13 Kellogg M W Co Air inlet structure for combustion chambers
BE482256A (en) * 1947-05-23

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20160223196A1 (en) * 2015-02-02 2016-08-04 The Government Of The United States Of America, As Represented By The Secretary Of The Navy Crude Oil Spray Combustor

Also Published As

Publication number Publication date
FR959791A (en) 1950-04-05
CH271829A (en) 1950-11-15
NL207253A (en)
NL90479C (en)
US2826039A (en) 1958-03-11
BE479471A (en)
NL82911C (en)

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