GB468287A - Method for the working of thermal power plants and plant for carrying out this method - Google Patents
Method for the working of thermal power plants and plant for carrying out this methodInfo
- Publication number
- GB468287A GB468287A GB56/36A GB5636A GB468287A GB 468287 A GB468287 A GB 468287A GB 56/36 A GB56/36 A GB 56/36A GB 5636 A GB5636 A GB 5636A GB 468287 A GB468287 A GB 468287A
- Authority
- GB
- United Kingdom
- Prior art keywords
- turbine
- working
- air
- compressor
- container
- 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
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/16—Control of working fluid flow
- F02C9/24—Control of the pressure level in closed cycles
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
468,287. Hot air and gas power plant. AKT.-GES. FUR TECHNISCHE STUDIEN. Jan. 1, 1936, No. 56. Convention date, July 12, 1935. [Class 7 (i)] [Also in Group XXVI] In a power plant, the working-fluid, preferably air, is heated in a coil 2 placed within a combustion chamber 1, enters and exhausts from a turbine 3, which drives a generator 4 and a compressor 5, and is exhausted at 6 into a heat-exchanger 7 in which working-fluid compressed in the compressor 5 is heated before entering the coil 2. The air exhausted from the turbine into the exchanger 7 is at a practically constant pressure and is cooled to at least 150‹ C. A cooling system 13 ... 16, fed by a pump 12, is provided for the compressor 5, and a coil 25 may cool the pipe 11. Hot exhaust gases from the chamber 1 pass through a pipe 17 into a heat-exchanger 18 in which the air passing into the chamber 1 is heated. A blower 20 supplies the air. As a governing means, working medium may be added to or withdrawn from the working cycle by means of storage containers 24, 24<1>. The container 24 is supplied from the atmosphere by a compressor 23 and is connected to an inlet valve 10<1> of a regulator 10. An outlet valve 10<2> leads to the container 24<1>. According to the adjustment of the valves 10<1>, 10<2> , air flows from the container 24 into the enclosed cycle or out of it. A governor on the turbine or the generator may control the valves 10<1>, 10<2>. The working- fluid may be throttled before or after the turbine. In a modified plant, the turbine is in two sections, one driving a generator and the other the compressor. The working - fluid passes through the first turbine and is returned to a heating coil in the chamber 1, to be restored to about its original temperature, before being led to the second turbine. The turbine may run at different speeds. Other gases such as helium, hydrogen, or nitrogen may be used in place of air. The container 24 may store up compressed air for starting-up the turbine.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CH468287X | 1935-07-12 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB468287A true GB468287A (en) | 1937-07-01 |
Family
ID=4515932
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB56/36A Expired GB468287A (en) | 1935-07-12 | 1936-01-01 | Method for the working of thermal power plants and plant for carrying out this method |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB468287A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2421387A (en) * | 1943-04-02 | 1947-06-03 | Ljungstroms Angturbin Ab | Hot air turbine power plant with automatic air supply control |
| US2641905A (en) * | 1948-06-21 | 1953-06-16 | Tech Studien Ag | Closed circuit power plant having bypass means to regulate heat input to each turbine |
| US2658349A (en) * | 1949-01-21 | 1953-11-10 | Tech Studien Ag | Plant for the recovery of waste heat from combustible gases derived from chemical processes |
| US2956402A (en) * | 1955-06-27 | 1960-10-18 | Garrett Corp | Multistage high altitude engine with single combustion stage |
-
1936
- 1936-01-01 GB GB56/36A patent/GB468287A/en not_active Expired
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2421387A (en) * | 1943-04-02 | 1947-06-03 | Ljungstroms Angturbin Ab | Hot air turbine power plant with automatic air supply control |
| US2641905A (en) * | 1948-06-21 | 1953-06-16 | Tech Studien Ag | Closed circuit power plant having bypass means to regulate heat input to each turbine |
| US2658349A (en) * | 1949-01-21 | 1953-11-10 | Tech Studien Ag | Plant for the recovery of waste heat from combustible gases derived from chemical processes |
| US2956402A (en) * | 1955-06-27 | 1960-10-18 | Garrett Corp | Multistage high altitude engine with single combustion stage |
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