CH258674A - Verbrennungs-Turbinenaggregat. - Google Patents
Verbrennungs-Turbinenaggregat.Info
- Publication number
- CH258674A CH258674A CH258674DA CH258674A CH 258674 A CH258674 A CH 258674A CH 258674D A CH258674D A CH 258674DA CH 258674 A CH258674 A CH 258674A
- Authority
- CH
- Switzerland
- Prior art keywords
- turbine unit
- combustion turbine
- combustion
- unit
- turbine
- Prior art date
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
-
- 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
-
- 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)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9203/46A GB610113A (en) | 1946-03-25 | 1946-03-25 | Improvements in or relating to gas-turbine engines |
Publications (1)
Publication Number | Publication Date |
---|---|
CH258674A true CH258674A (de) | 1948-12-15 |
Family
ID=9867397
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH258674D CH258674A (de) | 1946-03-25 | 1948-08-18 | Verbrennungs-Turbinenaggregat. |
Country Status (5)
Country | Link |
---|---|
US (1) | US2494821A (de) |
BE (1) | BE487120A (de) |
CH (1) | CH258674A (de) |
FR (1) | FR943932A (de) |
GB (1) | GB610113A (de) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1218800B (de) * | 1961-04-25 | 1966-06-08 | M A N Turbo Ges Mit Beschraenk | Gasturbine, insbesondere Kleingasturbine |
DE102010001059A1 (de) * | 2010-01-20 | 2011-07-21 | Rolls-Royce Deutschland Ltd & Co KG, 15827 | Zwischengehäuse für ein Gasturbinentriebwerk |
Families Citing this family (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2711074A (en) * | 1944-06-22 | 1955-06-21 | Gen Electric | Aft frame and rotor structure for combustion gas turbine |
BE487768A (de) * | 1947-03-14 | |||
US2789787A (en) * | 1949-10-22 | 1957-04-23 | Svenska Turbinfab Ab | Guide blade device for steam or gas turbines |
US2608057A (en) * | 1949-12-24 | 1952-08-26 | A V Roe Canada Ltd | Gas turbine nozzle box |
US2763462A (en) * | 1950-01-11 | 1956-09-18 | Gen Motors Corp | Turbine casing construction |
US2609176A (en) * | 1950-01-21 | 1952-09-02 | A V Roe Canada Ltd | Turbine nozzle guide vane construction |
US2654566A (en) * | 1950-02-11 | 1953-10-06 | A V Roe Canada Ltd | Turbine nozzle guide vane construction |
US2747367A (en) * | 1950-03-21 | 1956-05-29 | United Aircraft Corp | Gas turbine power plant supporting structure |
US2699040A (en) * | 1950-05-23 | 1955-01-11 | Gen Motors Corp | Detachable combustion chamber for gas turbines |
US2780174A (en) * | 1951-03-19 | 1957-02-05 | Solar Aircraft Co | Pump and power plant assembly |
US2702454A (en) * | 1951-06-07 | 1955-02-22 | United Aircraft Corp | Transition piece providing a connection between the combustion chambers and the turbine nozzle in gas turbine power plants |
US2848191A (en) * | 1951-11-03 | 1958-08-19 | A V Roe Canada Ltd | Nozzle box |
US2839894A (en) * | 1952-12-31 | 1958-06-24 | Gen Motors Corp | Supporting arrangement for a gas turbine combustion chamber |
US2825285A (en) * | 1953-12-28 | 1958-03-04 | Belton A Copp | Centrifugal pump with discharge manifold |
NL230456A (de) * | 1957-08-22 | |||
US4573315A (en) * | 1984-05-15 | 1986-03-04 | A/S Kongsberg Vapenfabrikk | Low pressure loss, convectively gas-cooled inlet manifold for high temperature radial turbine |
US6116013A (en) * | 1998-01-02 | 2000-09-12 | Siemens Westinghouse Power Corporation | Bolted gas turbine combustor transition coupling |
GB0618991D0 (en) * | 2006-09-27 | 2006-11-08 | Rolls Royce Plc | A component for a gas turbine engine |
US9021783B2 (en) * | 2012-10-12 | 2015-05-05 | United Technologies Corporation | Pulse detonation engine having a scroll ejector attenuator |
US9470422B2 (en) | 2013-10-22 | 2016-10-18 | Siemens Energy, Inc. | Gas turbine structural mounting arrangement between combustion gas duct annular chamber and turbine vane carrier |
US9810434B2 (en) * | 2016-01-21 | 2017-11-07 | Siemens Energy, Inc. | Transition duct system with arcuate ceramic liner for delivering hot-temperature gases in a combustion turbine engine |
US10465642B2 (en) | 2017-03-27 | 2019-11-05 | Kohler Co. | Carburetor drain |
CN113154456B (zh) * | 2021-04-15 | 2022-06-21 | 中国航发湖南动力机械研究所 | 回流燃烧室机匣头部结构及其制造方法和发动机燃烧室 |
CN115288804B (zh) * | 2022-10-10 | 2023-03-24 | 中国航发四川燃气涡轮研究院 | 一种鸟类骨架仿生式承力结构及其设计方法 |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2432359A (en) * | 1947-12-09 | Internal-combustion turbine power | ||
GB588082A (en) * | 1941-08-25 | 1947-05-14 | Power Jets Ltd | Improvements relating to engines |
GB579331A (en) * | 1943-07-13 | 1946-07-31 | Francis Robert Bell | Improvements in combustion chambers for power-gas-generators, internal-combustion turbines and the like |
-
0
- BE BE487120D patent/BE487120A/xx unknown
-
1946
- 1946-03-25 GB GB9203/46A patent/GB610113A/en not_active Expired
-
1947
- 1947-03-11 US US733912A patent/US2494821A/en not_active Expired - Lifetime
- 1947-03-24 FR FR943932D patent/FR943932A/fr not_active Expired
-
1948
- 1948-08-18 CH CH258674D patent/CH258674A/de unknown
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1218800B (de) * | 1961-04-25 | 1966-06-08 | M A N Turbo Ges Mit Beschraenk | Gasturbine, insbesondere Kleingasturbine |
DE102010001059A1 (de) * | 2010-01-20 | 2011-07-21 | Rolls-Royce Deutschland Ltd & Co KG, 15827 | Zwischengehäuse für ein Gasturbinentriebwerk |
US8857193B2 (en) | 2010-01-20 | 2014-10-14 | Rolls-Royce Deutschland Ltd & Co Kg | Intermediate casing for a gas-turbine engine |
Also Published As
Publication number | Publication date |
---|---|
FR943932A (fr) | 1949-03-22 |
US2494821A (en) | 1950-01-17 |
BE487120A (de) | |
GB610113A (en) | 1948-10-12 |
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