GB783448A - Improvements in or relating to elastic fluid mechanism such as compressors, turbines, or diffusers - Google Patents
Improvements in or relating to elastic fluid mechanism such as compressors, turbines, or diffusersInfo
- Publication number
- GB783448A GB783448A GB237155A GB237155A GB783448A GB 783448 A GB783448 A GB 783448A GB 237155 A GB237155 A GB 237155A GB 237155 A GB237155 A GB 237155A GB 783448 A GB783448 A GB 783448A
- Authority
- GB
- United Kingdom
- Prior art keywords
- chamber
- diffusers
- compressors
- turbines
- relating
- 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
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
- F01D1/02—Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines
- F01D1/04—Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines traversed by the working-fluid substantially axially
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
- F02C3/08—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising at least one radial stage
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)
Abstract
783,448. Generating combustion products under pressure. BIRMANN, R. Jan. 26, 1955, No. 2371/55. Class 51 (1). [Also in Group XXVI] In the gas turbine plant shown, compressed air delivered by a compressor 152 is preheated by the turbine exhaust as it passes through preheater tubes 162 from a chamber 160 to a chamber 164 and thence through further preheater tubes 166 to a chamber 168, from which it enters a combustion chamber 172 through openings 170. The combustion gases leave the combustion chamber through nozzle vanes 174.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB237155A GB783448A (en) | 1955-01-26 | 1955-01-26 | Improvements in or relating to elastic fluid mechanism such as compressors, turbines, or diffusers |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB237155A GB783448A (en) | 1955-01-26 | 1955-01-26 | Improvements in or relating to elastic fluid mechanism such as compressors, turbines, or diffusers |
Publications (1)
Publication Number | Publication Date |
---|---|
GB783448A true GB783448A (en) | 1957-09-25 |
Family
ID=9738365
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB237155A Expired GB783448A (en) | 1955-01-26 | 1955-01-26 | Improvements in or relating to elastic fluid mechanism such as compressors, turbines, or diffusers |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB783448A (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2947468A (en) * | 1957-02-21 | 1960-08-02 | E E Lonabaugh | Multi-stage centrifugal compressor |
GB2127905A (en) * | 1982-09-30 | 1984-04-18 | Gen Electric | Centrifugal compressor |
GB2224083A (en) * | 1988-10-19 | 1990-04-25 | Rolls Royce Plc | Radial or mixed flow bladed rotors |
EP0402693A1 (en) * | 1989-06-10 | 1990-12-19 | Mtu Motoren- Und Turbinen-Union MàNchen Gmbh | Gasturbine with mixed-flow compressor |
WO2014149099A1 (en) * | 2013-03-15 | 2014-09-25 | Rolls-Royce North American Technologies, Inc. | Centrifugal compressor with axial impeller exit |
US10527059B2 (en) | 2013-10-21 | 2020-01-07 | Williams International Co., L.L.C. | Turbomachine diffuser |
EP4015831A1 (en) * | 2020-12-18 | 2022-06-22 | Siemens Energy Global GmbH & Co. KG | Radial turbomachine, in particular compressor |
-
1955
- 1955-01-26 GB GB237155A patent/GB783448A/en not_active Expired
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2947468A (en) * | 1957-02-21 | 1960-08-02 | E E Lonabaugh | Multi-stage centrifugal compressor |
GB2127905A (en) * | 1982-09-30 | 1984-04-18 | Gen Electric | Centrifugal compressor |
US4502837A (en) * | 1982-09-30 | 1985-03-05 | General Electric Company | Multi stage centrifugal impeller |
GB2224083A (en) * | 1988-10-19 | 1990-04-25 | Rolls Royce Plc | Radial or mixed flow bladed rotors |
EP0402693A1 (en) * | 1989-06-10 | 1990-12-19 | Mtu Motoren- Und Turbinen-Union MàNchen Gmbh | Gasturbine with mixed-flow compressor |
WO2014149099A1 (en) * | 2013-03-15 | 2014-09-25 | Rolls-Royce North American Technologies, Inc. | Centrifugal compressor with axial impeller exit |
US10527059B2 (en) | 2013-10-21 | 2020-01-07 | Williams International Co., L.L.C. | Turbomachine diffuser |
EP4015831A1 (en) * | 2020-12-18 | 2022-06-22 | Siemens Energy Global GmbH & Co. KG | Radial turbomachine, in particular compressor |
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