GB507423A - Improvements in and relating to plant in which products of combustion are generated under pressure - Google Patents
Improvements in and relating to plant in which products of combustion are generated under pressureInfo
- Publication number
- GB507423A GB507423A GB3421937A GB3421937A GB507423A GB 507423 A GB507423 A GB 507423A GB 3421937 A GB3421937 A GB 3421937A GB 3421937 A GB3421937 A GB 3421937A GB 507423 A GB507423 A GB 507423A
- Authority
- GB
- United Kingdom
- Prior art keywords
- plant
- under pressure
- turbine
- combustion chamber
- 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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/26—Starting; Ignition
Abstract
507,423. Gas turbines. AKT.-GES. BROWN, BOVERI, &,CIE. Dec. 10, 1937, No. 34219. Convention date, Dec. 10, 1936. [Class 110 (iii)] [Also in Group XII] Relates to plant in which gases under pressure are burnt in a chamber 2 and passed to a heat-exchanger 3 and in which the residual heat is used to drive a turbine 4 coupled to an air-compressor 5 from which air under pressure is supplied to the combustion chamber 2. For starting up such a plant, a byepass 7 is provided equipped with a combustion chamber 8. With the parts 2, 3 shut by valves 11, a starter motor 6 can bring the turbine 4 into operation without the necessity of a preliminary heating of the parts 23. Subsequently, the valves 11 can be used to close the byepass and put the plant into normal condition. An electric generator 12 may take any excess of power developed by the turbine 4 and may also be used as a starting motor. The combustion chamber 8 consists of an open-ended cylinder 20, Fig. 2, spaced from the concentric pressure pipe 21, with regulatable fuel and air inlets 22, 23.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DEA81378D DE660359C (en) | 1936-12-11 | 1936-12-11 | Device for the commissioning of systems in which high pressures are used to increase performance, which are supplied by gas turbine-driven compressors |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB507423A true GB507423A (en) | 1939-06-12 |
Family
ID=6546757
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB3421937A Expired GB507423A (en) | 1936-12-11 | 1937-12-10 | Improvements in and relating to plant in which products of combustion are generated under pressure |
Country Status (4)
| Country | Link |
|---|---|
| BE (1) | BE425079A (en) |
| DE (1) | DE660359C (en) |
| FR (1) | FR830454A (en) |
| GB (1) | GB507423A (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE768007C (en) * | 1939-12-24 | 1955-05-05 | Messerschmitt Boelkow Blohm | Method for regulating the thrust generated by hot jet engines for propelling aircraft |
| DE853536C (en) * | 1942-08-04 | 1952-10-27 | Maschf Augsburg Nuernberg Ag | Gas turbine plant with parts made of ceramic materials |
-
1936
- 1936-12-11 DE DEA81378D patent/DE660359C/en not_active Expired
-
1937
- 1937-12-06 FR FR830454D patent/FR830454A/en not_active Expired
- 1937-12-08 BE BE425079D patent/BE425079A/xx unknown
- 1937-12-10 GB GB3421937A patent/GB507423A/en not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| DE660359C (en) | 1938-05-24 |
| BE425079A (en) | 1937-02-28 |
| FR830454A (en) | 1938-07-29 |
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