GB484677A - Hot air and gas power plant - Google Patents
Hot air and gas power plantInfo
- Publication number
- GB484677A GB484677A GB30317/36A GB3031736A GB484677A GB 484677 A GB484677 A GB 484677A GB 30317/36 A GB30317/36 A GB 30317/36A GB 3031736 A GB3031736 A GB 3031736A GB 484677 A GB484677 A GB 484677A
- Authority
- GB
- United Kingdom
- Prior art keywords
- turbine
- exhaust
- heat exchanger
- turbines
- conveyed
- 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
- F01K—STEAM ENGINE PLANTS; STEAM ACCUMULATORS; ENGINE PLANTS NOT OTHERWISE PROVIDED FOR; ENGINES USING SPECIAL WORKING FLUIDS OR CYCLES
- F01K25/00—Plants or engines characterised by use of special working fluids, not otherwise provided for; Plants operating in closed cycles and not otherwise provided for
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
484,677. Gas turbines. KARRER, W. Nov. 6, 1936, No. 30317. Convention date, Nov. 15, 1935. [Class 110 (iii)] [Also in Group XXVII] In a hot air or gas power plant in which a gaseous operating medium is heated at constant volume by heat exchange and expanded in a power engine or turbine, the operating medium is mechanically compressed before admission to the constant-volume heating chamber and the resulting pressure increase is converted wholly or partly into work at a suitable point in the plant. In the plant shown diagrammatically in Fig. 1, the medium d is supplied intermittently by a compressor G to the constant-volume chamber B of a heat exchanger and thence to an intermittent-flow turbine E and a continuous-flow turbine F<1>. A part d<1> of the exhaust from the turbine E is conveyed to a combustion chamber A, in which it supports the combustion of fuel b, the hot products passing through the jacket of the heat exchanger and afterwards driving a turbine F<2>. In a modification, Fig. 2, a part d<1> of the exhaust from the turbine E is conveyed to the combustion chamber A and thence through a jacket on the heat exchanger to a mixing chamber H, while the remainder of the exhaust from the turbine is conveyed directly to the mixing chamber H. The gases are thence conveyed to the turbine F and exhausted through a second jacket on the heat exchanger. In another modification, the whole of the operating medium passes through both turbines and part of the exhaust is then used in the combustion chamber A. The two turbines may be mounted on a single shaft driving the compressor G and an electric generator ; or these turbines may drive separate generators supplying the same main, the second turbine also driving the compressor G.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH484677X | 1935-11-15 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB484677A true GB484677A (en) | 1938-05-06 |
Family
ID=4516410
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB30317/36A Expired GB484677A (en) | 1935-11-15 | 1936-11-06 | Hot air and gas power plant |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB484677A (en) |
-
1936
- 1936-11-06 GB GB30317/36A patent/GB484677A/en not_active Expired
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