GB722190A - Gas turbine plant - Google Patents
Gas turbine plantInfo
- Publication number
- GB722190A GB722190A GB3027651A GB3027651A GB722190A GB 722190 A GB722190 A GB 722190A GB 3027651 A GB3027651 A GB 3027651A GB 3027651 A GB3027651 A GB 3027651A GB 722190 A GB722190 A GB 722190A
- Authority
- GB
- United Kingdom
- Prior art keywords
- rotor
- opening
- combustion chamber
- heat exchanger
- air
- 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
- 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
- F02C3/02—Gas-turbine plants characterised by the use of combustion products as the working fluid using exhaust-gas pressure in a pressure exchanger to compress combustion-air
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)
Abstract
722,190. Gas-turbine plant. INCONEX HANDELSGES. FUR INDUSTRIELLE PRODUKTE - KONSTRUKTIONEN - EXPORT. Dec. 28, 1951, No. 30276/51. Class 110 (3). [Also in Group XXVIII] A gas-turbine plant in which air is compressed, passed through a rotating pressure exchanger into a combustion chamber or heat exchanger, then again through the rotating pressure exchanger to drive a turbine has guide vanes between the combustion chamber or heat exchanger and the rotor of the pressure exchanger to lead the hot gases passing tangentially into the periphery of the rotor and other guide vanes between the rotor and combustion chamber or heat exchanger to guide the fresh air out of the rotor. Air compressed in the compressor 2 passes through an opening 12 into chambers 14 formed between the radial blades 15 of a pressure exchanger rotor 3. This air expels the residual gases in the rotor through the opening 22 to the exhaust 22a. The rotor chambers 14 after rotation reach the opening 17 and hot gases from the combustion chamber or heat exchanger 16 flow tangentially into the rotor chambers and compress the fresh air. After further rotation of the rotor the opening 18 is reached and the fresh compressed air enters the combustion chamber or heat exchanger 16. After passing the opening 18, the rotor contains preponderantly hot gas which passes through the opening 13 and the guiding device 6 to the turbine 7. Guide vanes 19 are provided to lead the hot gas tangentially on to the periphery of the rotor 3 and guide vanes 20 to lead the hot air out of the rotor. Specification 559,839 is referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3027651A GB722190A (en) | 1951-12-28 | 1951-12-28 | Gas turbine plant |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3027651A GB722190A (en) | 1951-12-28 | 1951-12-28 | Gas turbine plant |
Publications (1)
Publication Number | Publication Date |
---|---|
GB722190A true GB722190A (en) | 1955-01-19 |
Family
ID=10305073
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3027651A Expired GB722190A (en) | 1951-12-28 | 1951-12-28 | Gas turbine plant |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB722190A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2415467A (en) * | 2004-06-14 | 2005-12-28 | Mark Adrian Bourne | Gas turbine engine |
-
1951
- 1951-12-28 GB GB3027651A patent/GB722190A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2415467A (en) * | 2004-06-14 | 2005-12-28 | Mark Adrian Bourne | Gas turbine engine |
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