JPS52156213A - Combustor receiving structure - Google Patents
Combustor receiving structureInfo
- Publication number
- JPS52156213A JPS52156213A JP2936877A JP2936877A JPS52156213A JP S52156213 A JPS52156213 A JP S52156213A JP 2936877 A JP2936877 A JP 2936877A JP 2936877 A JP2936877 A JP 2936877A JP S52156213 A JPS52156213 A JP S52156213A
- Authority
- JP
- Japan
- Prior art keywords
- receiving structure
- combustor receiving
- combustor
- receiving
- 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.)
- Pending
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
- F23R3/60—Support structures; Attaching or mounting means
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US69828376A | 1976-06-21 | 1976-06-21 |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS52156213A true JPS52156213A (en) | 1977-12-26 |
Family
ID=24804624
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2936877A Pending JPS52156213A (en) | 1976-06-21 | 1977-03-18 | Combustor receiving structure |
Country Status (4)
Country | Link |
---|---|
JP (1) | JPS52156213A (en) |
DE (1) | DE2711564A1 (en) |
FR (1) | FR2356000A1 (en) |
GB (1) | GB1578474A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5619340U (en) * | 1979-07-25 | 1981-02-20 | ||
JP2005300145A (en) * | 2004-04-15 | 2005-10-27 | Snecma Moteurs | Annular combustion chamber for turbomachine having improved inner fixing flange |
JP2008038897A (en) * | 2006-08-08 | 2008-02-21 | General Electric Co <Ge> | Method and apparatus for radially compliant component mounting |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2117102B (en) * | 1982-03-20 | 1985-07-03 | Rolls Royce | Improvements in or relating to mounting arrangements for combustion equipment |
DE19745683A1 (en) * | 1997-10-16 | 1999-04-22 | Bmw Rolls Royce Gmbh | Suspension of an annular gas turbine combustion chamber |
FR2825782A1 (en) * | 2001-06-06 | 2002-12-13 | Snecma Moteurs | Turbine with metal casing has composition combustion chamber fitted with sliding coupling to allow for differences in expansion coefficients |
US6672833B2 (en) * | 2001-12-18 | 2004-01-06 | General Electric Company | Gas turbine engine frame flowpath liner support |
US6931855B2 (en) | 2003-05-12 | 2005-08-23 | Siemens Westinghouse Power Corporation | Attachment system for coupling combustor liners to a carrier of a turbine combustor |
EP1741877A1 (en) * | 2005-07-04 | 2007-01-10 | Siemens Aktiengesellschaft | Heat shield and stator vane for a gas turbine |
FR2890156A1 (en) * | 2005-08-31 | 2007-03-02 | Snecma | Turbomachine e.g. aircraft turbojet, combustion chamber, has internal and external flanges with orifices of triangular shape, where successive triangular orifices are arranged in staggered and head-to-tail configuration |
FR2892181B1 (en) * | 2005-10-18 | 2008-02-01 | Snecma Sa | FIXING A COMBUSTION CHAMBER WITHIN ITS CARTER |
FR2944090B1 (en) * | 2009-04-07 | 2015-04-03 | Snecma | TURBOMACHINE WITH ANNULAR COMBUSTION CHAMBER |
EP3078914A1 (en) * | 2015-04-09 | 2016-10-12 | Siemens Aktiengesellschaft | Annular combustor for a gas turbine engine |
RU2715634C2 (en) * | 2016-11-21 | 2020-03-02 | Дженерал Электрик Текнолоджи Гмбх | Device and method for forced cooling of gas turbine plant components |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2447482A (en) * | 1945-04-25 | 1948-08-24 | Westinghouse Electric Corp | Turbine apparatus |
GB620270A (en) * | 1945-11-20 | 1949-03-22 | Westinghouse Electric Int Co | Improvements in or relating to turbine apparatus |
FR941475A (en) * | 1946-02-12 | 1949-01-12 | Lucas Ltd Joseph | Combustion chamber for engines |
GB698539A (en) * | 1951-08-23 | 1953-10-14 | Svenska Turbinfab Ab | Expansible connecting element |
US2795108A (en) * | 1953-10-07 | 1957-06-11 | Westinghouse Electric Corp | Combustion apparatus |
FR1368570A (en) * | 1962-09-11 | 1964-07-31 | Lucas Industries Ltd | Support of the downstream end of the combustion chamber of a gas turbo-engine |
GB1488481A (en) * | 1973-10-05 | 1977-10-12 | Rolls Royce | Gas turbine engines |
US3905192A (en) * | 1974-08-29 | 1975-09-16 | United Aircraft Corp | Combustor having staged premixing tubes |
-
1977
- 1977-03-07 GB GB955377A patent/GB1578474A/en not_active Expired
- 1977-03-17 DE DE19772711564 patent/DE2711564A1/en not_active Withdrawn
- 1977-03-18 JP JP2936877A patent/JPS52156213A/en active Pending
- 1977-03-21 FR FR7708378A patent/FR2356000A1/en active Pending
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5619340U (en) * | 1979-07-25 | 1981-02-20 | ||
JP2005300145A (en) * | 2004-04-15 | 2005-10-27 | Snecma Moteurs | Annular combustion chamber for turbomachine having improved inner fixing flange |
JP2008038897A (en) * | 2006-08-08 | 2008-02-21 | General Electric Co <Ge> | Method and apparatus for radially compliant component mounting |
US8141370B2 (en) | 2006-08-08 | 2012-03-27 | General Electric Company | Methods and apparatus for radially compliant component mounting |
Also Published As
Publication number | Publication date |
---|---|
FR2356000A1 (en) | 1978-01-20 |
DE2711564A1 (en) | 1977-12-29 |
GB1578474A (en) | 1980-11-05 |
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