GB586555A - Improvements in internal combustion gas turbine plant, supercharger plant, air conditioning plant and the like - Google Patents
Improvements in internal combustion gas turbine plant, supercharger plant, air conditioning plant and the likeInfo
- Publication number
- GB586555A GB586555A GB1619041A GB1619041A GB586555A GB 586555 A GB586555 A GB 586555A GB 1619041 A GB1619041 A GB 1619041A GB 1619041 A GB1619041 A GB 1619041A GB 586555 A GB586555 A GB 586555A
- Authority
- GB
- United Kingdom
- Prior art keywords
- plant
- compressor
- bladings
- air
- turbine
- 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
- F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
- F02C3/06—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
- F02C3/067—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages having counter-rotating rotors
Abstract
586,555. Gas turbines. BAUMANN, K., and METROPOLITAN-VICKERS ELECTRICAL CO., Ltd. Dec. 15,' 1941, No. 16190. [Class 110 (iii)] A gas turbine plant which may be used for jet propulsion of aircraft or supercharging an I.C. engine, or, in air-conditioning or refrigerating plant, comprises a contra-rotational air-compressor driven by contra-rotational turbine discs 36, 37 which are axially beyond the compressor. The discs 36, 37 have bladings 34, 35 which pass or further compress the air delivered from the compressor. The combustion chamber is of annular swan-neck form and delivers products of combustion to fixed bladings I which precede the turbine bladings II, III. The exhaust is received by fixed bladings IV. The air-compressor rotors are driven through tubular shafts or sleeves 15, 39 and there is a bearing 43 between the sleeves. In one modification the fixed blading ring IV is omitted and the outer compressor rotor is directly connected to the foundation ring of the blading III. Modifications of the driving sleeve and bearing arrangements are described. In another form an annular combustion chamber, or group of chambers, is interposed between the compressor and the turbine and three arrangements of driving sleeves and bearings are described. Specifications 544,909, 586,551, 586,552, 586,553 and 586,554 are referred to.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1619041A GB586555A (en) | 1941-12-15 | 1941-12-15 | Improvements in internal combustion gas turbine plant, supercharger plant, air conditioning plant and the like |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1619041A GB586555A (en) | 1941-12-15 | 1941-12-15 | Improvements in internal combustion gas turbine plant, supercharger plant, air conditioning plant and the like |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB586555A true GB586555A (en) | 1947-03-24 |
Family
ID=10072798
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1619041A Expired GB586555A (en) | 1941-12-15 | 1941-12-15 | Improvements in internal combustion gas turbine plant, supercharger plant, air conditioning plant and the like |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB586555A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2812898A (en) * | 1954-02-25 | 1957-11-12 | Ernest H Buell | Reverse action rotors for use in a jet propulsion system |
| DE1045037B (en) * | 1952-04-30 | 1958-11-27 | Alfred Buechi Dr Ing | Turbine driven centrifugal compressor or pump |
| US2990108A (en) * | 1957-03-04 | 1961-06-27 | Curtiss Wright Corp | Compressor with annular discharge diffuser |
-
1941
- 1941-12-15 GB GB1619041A patent/GB586555A/en not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1045037B (en) * | 1952-04-30 | 1958-11-27 | Alfred Buechi Dr Ing | Turbine driven centrifugal compressor or pump |
| US2812898A (en) * | 1954-02-25 | 1957-11-12 | Ernest H Buell | Reverse action rotors for use in a jet propulsion system |
| US2990108A (en) * | 1957-03-04 | 1961-06-27 | Curtiss Wright Corp | Compressor with annular discharge diffuser |
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