GB585509A - Improvements in or relating to power plants - Google Patents
Improvements in or relating to power plantsInfo
- Publication number
- GB585509A GB585509A GB6873/44A GB687344A GB585509A GB 585509 A GB585509 A GB 585509A GB 6873/44 A GB6873/44 A GB 6873/44A GB 687344 A GB687344 A GB 687344A GB 585509 A GB585509 A GB 585509A
- Authority
- GB
- United Kingdom
- Prior art keywords
- cavity
- delivered
- issue
- gases
- nozzles
- 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
- F02C7/268—Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
- F02C7/27—Fluid drives
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
585,509. Gas turbines. WESTINGHOUSE ELECTRIC INTERNATIONAL CO. April 13, 1944, No. 6873. Convention date, Feb. 3, 1943. [Class 110 (iii)] A gas turbine plant, the exhaust of which is used for the jet-propulsion of aircraft, is started by means of a cartridge burning an explosive or by other source of compressed gas which is delivered by a pipe 37 to an annular cavity 36 surrounding the main turbine blades 17. The gases issue from the cavity through nozzles 35 and impact on the turbine blade. Alternatively, the gases may be delivered to an adjacent cavity 43 and issue through nozzles similar to those at 35 but between the stator blades 21. Specification 582,151 is referred to.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US585509XA | 1943-02-03 | 1943-02-03 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB585509A true GB585509A (en) | 1947-02-10 |
Family
ID=22017510
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB6873/44A Expired GB585509A (en) | 1943-02-03 | 1944-04-13 | Improvements in or relating to power plants |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB585509A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1009438B (en) * | 1955-11-23 | 1957-05-29 | Power Jets Res & Dev Ltd | Method and device for carrying out the method for operating a jet engine |
| DE1043721B (en) * | 1955-10-05 | 1958-11-13 | Power Jets Res & Dev Ltd | Jet engine |
| DE1062987B (en) * | 1956-01-05 | 1959-08-06 | Power Jets Res & Dev Ltd | Gas turbine jet engine |
| GB2235498A (en) * | 1989-07-13 | 1991-03-06 | Sundstrand Corp | Starting gas turbine engines, for example in missiles |
-
1944
- 1944-04-13 GB GB6873/44A patent/GB585509A/en not_active Expired
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1043721B (en) * | 1955-10-05 | 1958-11-13 | Power Jets Res & Dev Ltd | Jet engine |
| DE1009438B (en) * | 1955-11-23 | 1957-05-29 | Power Jets Res & Dev Ltd | Method and device for carrying out the method for operating a jet engine |
| DE1062987B (en) * | 1956-01-05 | 1959-08-06 | Power Jets Res & Dev Ltd | Gas turbine jet engine |
| GB2235498A (en) * | 1989-07-13 | 1991-03-06 | Sundstrand Corp | Starting gas turbine engines, for example in missiles |
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