CA942513A - Double wall combustion chamber - Google Patents
Double wall combustion chamberInfo
- Publication number
- CA942513A CA942513A CA127,592A CA127592A CA942513A CA 942513 A CA942513 A CA 942513A CA 127592 A CA127592 A CA 127592A CA 942513 A CA942513 A CA 942513A
- Authority
- CA
- Canada
- Prior art keywords
- combustion chamber
- double wall
- wall combustion
- double
- 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
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)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10604171A | 1971-01-13 | 1971-01-13 |
Publications (1)
Publication Number | Publication Date |
---|---|
CA942513A true CA942513A (en) | 1974-02-26 |
Family
ID=22309157
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA127,592A Expired CA942513A (en) | 1971-01-13 | 1971-11-15 | Double wall combustion chamber |
Country Status (8)
Country | Link |
---|---|
US (1) | US3702058A (en) |
CA (1) | CA942513A (en) |
CH (1) | CH547996A (en) |
DE (1) | DE2161644A1 (en) |
FR (1) | FR2121779B1 (en) |
GB (1) | GB1312907A (en) |
IT (1) | IT946524B (en) |
NL (1) | NL7118118A (en) |
Families Citing this family (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4174608A (en) * | 1972-08-15 | 1979-11-20 | Stal-Laval Turbin Ab | Combustion chamber for a gas turbine |
FR2340453A1 (en) * | 1976-02-06 | 1977-09-02 | Snecma | COMBUSTION CHAMBER BODY, ESPECIALLY FOR TURBOREACTORS |
US4132066A (en) * | 1977-09-23 | 1979-01-02 | United Technologies Corporation | Combustor liner for gas turbine engine |
US4262487A (en) * | 1979-02-01 | 1981-04-21 | Westinghouse Electric Corp. | Double wall combustion chamber for a combustion turbine |
US4292810A (en) * | 1979-02-01 | 1981-10-06 | Westinghouse Electric Corp. | Gas turbine combustion chamber |
US4413477A (en) * | 1980-12-29 | 1983-11-08 | General Electric Company | Liner assembly for gas turbine combustor |
US4845940A (en) * | 1981-02-27 | 1989-07-11 | Westinghouse Electric Corp. | Low NOx rich-lean combustor especially useful in gas turbines |
US4413470A (en) * | 1981-03-05 | 1983-11-08 | Electric Power Research Institute, Inc. | Catalytic combustion system for a stationary combustion turbine having a transition duct mounted catalytic element |
US4407205A (en) * | 1982-04-30 | 1983-10-04 | Beaufrere Albert H | Regeneratively cooled coal combustor/gasifier with integral dry ash removal |
US4642993A (en) * | 1985-04-29 | 1987-02-17 | Avco Corporation | Combustor liner wall |
US4887432A (en) * | 1988-10-07 | 1989-12-19 | Westinghouse Electric Corp. | Gas turbine combustion chamber with air scoops |
JPH04123865A (en) * | 1990-09-13 | 1992-04-23 | Hitachi Ltd | Manufacture of combustor liner, depositing method and depositing device |
JP3415663B2 (en) * | 1992-12-28 | 2003-06-09 | アルストム | Equipment for cooling the cooling surface in an impact manner |
DE4244303A1 (en) * | 1992-12-28 | 1994-06-30 | Abb Research Ltd | Impact cooling system for cooling surface e.g. of combustion chamber wall |
US5327727A (en) * | 1993-04-05 | 1994-07-12 | General Electric Company | Micro-grooved heat transfer combustor wall |
US6018950A (en) * | 1997-06-13 | 2000-02-01 | Siemens Westinghouse Power Corporation | Combustion turbine modular cooling panel |
EP1284391A1 (en) * | 2001-08-14 | 2003-02-19 | Siemens Aktiengesellschaft | Combustion chamber for gas turbines |
EP1312865A1 (en) * | 2001-11-15 | 2003-05-21 | Siemens Aktiengesellschaft | Gas turbine annular combustion chamber |
US7377116B2 (en) * | 2005-04-28 | 2008-05-27 | Siemens Power Generation, Inc. | Gas turbine combustor barrier structures for spring clips |
US7594401B1 (en) * | 2008-04-10 | 2009-09-29 | General Electric Company | Combustor seal having multiple cooling fluid pathways |
US8549861B2 (en) * | 2009-01-07 | 2013-10-08 | General Electric Company | Method and apparatus to enhance transition duct cooling in a gas turbine engine |
US8667801B2 (en) | 2010-09-08 | 2014-03-11 | Siemens Energy, Inc. | Combustor liner assembly with enhanced cooling system |
EP2500648B1 (en) * | 2011-03-15 | 2013-09-04 | Siemens Aktiengesellschaft | Gas turbine combustion chamber |
US9366438B2 (en) * | 2013-02-14 | 2016-06-14 | Siemens Aktiengesellschaft | Flow sleeve inlet assembly in a gas turbine engine |
US20220018541A1 (en) * | 2020-07-16 | 2022-01-20 | Raytheon Technologies Corporation | Article and method for manufacturing an expanded combustor liner |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH229934A (en) * | 1942-10-06 | 1943-11-30 | Bbc Brown Boveri & Cie | Gas turbine plant. |
FR945486A (en) * | 1946-04-03 | 1949-05-05 | Westinghouse Electric Corp | Improvements to combustion devices for gas turbines |
US2610467A (en) * | 1946-04-03 | 1952-09-16 | Westinghouse Electric Corp | Combustion chamber having telescoping walls and corrugated spacers |
GB759489A (en) * | 1953-02-26 | 1956-10-17 | Rolls Royce | Improvements in or relating to gas-turbine engine combustion equipment |
US3169367A (en) * | 1963-07-18 | 1965-02-16 | Westinghouse Electric Corp | Combustion apparatus |
GB998755A (en) * | 1964-05-07 | 1965-07-21 | Rolls Royce | Improvements in or relating to combustion equipment |
US3545202A (en) * | 1969-04-02 | 1970-12-08 | United Aircraft Corp | Wall structure and combustion holes for a gas turbine engine |
US3572031A (en) * | 1969-07-11 | 1971-03-23 | United Aircraft Corp | Variable area cooling passages for gas turbine burners |
-
1971
- 1971-01-13 US US106041A patent/US3702058A/en not_active Expired - Lifetime
- 1971-11-15 CA CA127,592A patent/CA942513A/en not_active Expired
- 1971-11-22 GB GB5412571A patent/GB1312907A/en not_active Expired
- 1971-12-11 DE DE19712161644 patent/DE2161644A1/en active Pending
- 1971-12-20 CH CH1858971A patent/CH547996A/en not_active IP Right Cessation
- 1971-12-30 NL NL7118118A patent/NL7118118A/xx unknown
-
1972
- 1972-01-12 FR FR7200919A patent/FR2121779B1/fr not_active Expired
- 1972-01-13 IT IT19306/72A patent/IT946524B/en active
Also Published As
Publication number | Publication date |
---|---|
NL7118118A (en) | 1972-07-17 |
IT946524B (en) | 1973-05-21 |
GB1312907A (en) | 1973-04-11 |
DE2161644A1 (en) | 1972-07-20 |
US3702058A (en) | 1972-11-07 |
FR2121779A1 (en) | 1972-08-25 |
CH547996A (en) | 1974-04-11 |
FR2121779B1 (en) | 1974-11-08 |
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