GB612532A - Improvements in or relating to combustion chambers for internal combustion turbines - Google Patents

Improvements in or relating to combustion chambers for internal combustion turbines

Info

Publication number
GB612532A
GB612532A GB10805/46A GB1080546A GB612532A GB 612532 A GB612532 A GB 612532A GB 10805/46 A GB10805/46 A GB 10805/46A GB 1080546 A GB1080546 A GB 1080546A GB 612532 A GB612532 A GB 612532A
Authority
GB
United Kingdom
Prior art keywords
flame tube
outer casing
inlet
casing
axial
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
GB10805/46A
Other languages
English (en)
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
Priority to GB10805/46A priority Critical patent/GB612532A/en
Priority to US733911A priority patent/US2615300A/en
Priority to FR944168D priority patent/FR944168A/fr
Priority to CH261728D priority patent/CH261728A/de
Publication of GB612532A publication Critical patent/GB612532A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
    • 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
    • F23R3/60—Support structures; Attaching or mounting means

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
GB10805/46A 1946-04-08 1946-04-08 Improvements in or relating to combustion chambers for internal combustion turbines Expired GB612532A (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
GB10805/46A GB612532A (en) 1946-04-08 1946-04-08 Improvements in or relating to combustion chambers for internal combustion turbines
US733911A US2615300A (en) 1946-04-08 1947-03-11 Combustion chamber for gas turbines and having flame tube mounting means allowing radial and axial expansion
FR944168D FR944168A (fr) 1946-04-08 1947-03-29 Perfectionnements aux chambres de combustion pour turbines à combustion interne
CH261728D CH261728A (de) 1946-04-08 1947-04-02 Brennkammer für Brennkraftturbinen.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB10805/46A GB612532A (en) 1946-04-08 1946-04-08 Improvements in or relating to combustion chambers for internal combustion turbines

Publications (1)

Publication Number Publication Date
GB612532A true GB612532A (en) 1948-11-15

Family

ID=29726706

Family Applications (1)

Application Number Title Priority Date Filing Date
GB10805/46A Expired GB612532A (en) 1946-04-08 1946-04-08 Improvements in or relating to combustion chambers for internal combustion turbines

Country Status (4)

Country Link
US (1) US2615300A (fr)
CH (1) CH261728A (fr)
FR (1) FR944168A (fr)
GB (1) GB612532A (fr)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1011066A (fr) * 1948-11-30 1952-06-18 Chambre de combustion
BE507040A (fr) * 1950-11-17
US2800767A (en) * 1952-12-31 1957-07-30 United Aircraft Corp Combustion section construction
US2839894A (en) * 1952-12-31 1958-06-24 Gen Motors Corp Supporting arrangement for a gas turbine combustion chamber
US2851854A (en) * 1955-01-21 1958-09-16 United Aircraft Corp Afterburner liner
DE1060667B (de) * 1955-10-15 1959-07-02 Stroemungsmasch Anst Verbrennungseinrichtung fuer Gasturbinen
US2852914A (en) * 1955-12-30 1958-09-23 United Aircraft Corp Combustion chamber support means
DE1047536B (de) * 1956-07-07 1958-12-24 Daimler Benz Ag Brennkammer fuer Gasturbinen
US3048015A (en) * 1959-07-08 1962-08-07 Gen Motors Corp Combustion chamber support and igniter
US3084907A (en) * 1960-10-31 1963-04-09 Gen Electric Gas turbine scroll mount
US5224825A (en) * 1991-12-26 1993-07-06 General Electric Company Locator pin retention device for floating joint
DE4223733C2 (de) * 1992-07-18 1995-05-18 Gutehoffnungshuette Man Verbindung von Mischrohr und Flammrohr einer Gasturbine
GB2293232B (en) * 1994-09-15 1998-05-20 Rolls Royce Plc A combustion chamber assembly
US6116013A (en) * 1998-01-02 2000-09-12 Siemens Westinghouse Power Corporation Bolted gas turbine combustor transition coupling
US7024863B2 (en) * 2003-07-08 2006-04-11 Pratt & Whitney Canada Corp. Combustor attachment with rotational joint
ITMI20031673A1 (it) * 2003-08-28 2005-02-28 Nuovo Pignone Spa Sistema di fissaggio di un tubo di fiamma o "liner".
US20080006641A1 (en) * 2005-02-22 2008-01-10 Pratt & Whitney Canada Corp. Positioning arrangement for components of a pressure vessel and method
US8141370B2 (en) * 2006-08-08 2012-03-27 General Electric Company Methods and apparatus for radially compliant component mounting
US20090067917A1 (en) * 2007-09-07 2009-03-12 The Boeing Company Bipod Flexure Ring
US8726675B2 (en) * 2007-09-07 2014-05-20 The Boeing Company Scalloped flexure ring
US9416969B2 (en) * 2013-03-14 2016-08-16 Siemens Aktiengesellschaft Gas turbine transition inlet ring adapter

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2432359A (en) * 1947-12-09 Internal-combustion turbine power
US2195025A (en) * 1935-07-17 1940-03-26 Couzinet Rene Alexandre Arthur Gas turbine
US2183313A (en) * 1938-07-07 1939-12-12 Robert H Goddard Combustion chamber for aircraft
US2268464A (en) * 1939-09-29 1941-12-30 Bbc Brown Boveri & Cie Combustion chamber
US2225775A (en) * 1940-01-26 1940-12-24 David L Garrett Apparatus for deparaffining oil wells
US2500925A (en) * 1943-03-13 1950-03-21 Claude A Bonvillian Apparatus for the combustion of fuel
GB588086A (en) * 1943-04-01 1947-05-14 Power Jets Ltd Improvements relating to combustion apparatus
US2420135A (en) * 1944-06-07 1947-05-06 Elliott Co Support for expansible members
US2458497A (en) * 1945-05-05 1949-01-11 Babcock & Wilcox Co Combustion chamber

Also Published As

Publication number Publication date
CH261728A (de) 1949-05-31
FR944168A (fr) 1949-03-29
US2615300A (en) 1952-10-28

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