GB653159A - Improvements in or relating to gas turbine power plants - Google Patents
Improvements in or relating to gas turbine power plantsInfo
- Publication number
- GB653159A GB653159A GB26280/48A GB2628048A GB653159A GB 653159 A GB653159 A GB 653159A GB 26280/48 A GB26280/48 A GB 26280/48A GB 2628048 A GB2628048 A GB 2628048A GB 653159 A GB653159 A GB 653159A
- Authority
- GB
- United Kingdom
- Prior art keywords
- gas turbine
- passage
- blades
- manifold
- fairway
- 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
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/047—Heating to prevent icing
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
653,159. Gas turbine plant. WESTING- HOUSE ELECTRIC INTERNATIONAL CO. Oct. 8, 1948, No. 26280. Convention date, Oct. 9, 1947. [Classes 110(i) and 110(iii)] The intake of an air compressor forming part of a gas turbine plant is prevented from icing by means of hot gas extracted from the turbine and passed through a pipe 30, an annular manifold 28, guide vanes 25 and an inner manifold 35 from which manifold gases are exhausted by a pipe 37 which leads to a point 38 in the leading end of the fairway 16. A shield 39 guides the gases rearwardly over the fairway 16. The blades 25 may be hollow or may be solid blades having a passage in the leading edge formed by attaching a U-shaped member or tubular member to it. In another form the passage is drilled through the solid blade and this passage is connected by slots to the surface of the blade. In a further form the hollow blades 25 are provided with vent openings in the trailing edge.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US653159XA | 1947-10-09 | 1947-10-09 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB653159A true GB653159A (en) | 1951-05-09 |
Family
ID=22061847
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB26280/48A Expired GB653159A (en) | 1947-10-09 | 1948-10-08 | Improvements in or relating to gas turbine power plants |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB653159A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2218473A (en) * | 1988-05-10 | 1989-11-15 | Mtu Muenchen Gmbh | Composite propeller blade |
-
1948
- 1948-10-08 GB GB26280/48A patent/GB653159A/en not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2218473A (en) * | 1988-05-10 | 1989-11-15 | Mtu Muenchen Gmbh | Composite propeller blade |
| US4944655A (en) * | 1988-05-10 | 1990-07-31 | Mtu Motoren- Und Turbinen-Union Munich Gmbh | Propeller blade of a fiber-reinforced plastic material |
| GB2218473B (en) * | 1988-05-10 | 1992-07-15 | Mtu Muenchen Gmbh | Propeller blade of fibre-reinforced plastics material |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| GB1144036A (en) | A vane for an aerial flow turbomachine | |
| GB586572A (en) | Improvements in internal combustion turbine plant for propulsion by jet action, at least in part | |
| GB659151A (en) | Improvements in or relating to gas turbine power plants | |
| GB666536A (en) | Stator blades for a gas turbine | |
| GB1097300A (en) | Improvements in gas turbine blades | |
| GB636290A (en) | Improvements in diffusers for centrifugal compressors | |
| GB653159A (en) | Improvements in or relating to gas turbine power plants | |
| GB609446A (en) | Improvements in or relating to the rotors of gas turbines or the like | |
| GB192405A (en) | Improvements relating to wind turbines | |
| GB719061A (en) | Blade arrangement for improving the performance of a gas turbine plant | |
| GB660178A (en) | Improvements in or relating to gas turbine power plants of the continuous combustiontype | |
| GB1193587A (en) | Nozzle Guide Vanes for Gas Turbine Engines. | |
| GB635609A (en) | Improvements in and relating to wind tunnels | |
| GB586556A (en) | Improvements in internal combustion turbine plant for propulsion | |
| GB793823A (en) | Helicopters | |
| GB638094A (en) | Improvements in or relating to gas-turbine-engine installations | |
| GB345888A (en) | An improved method of supporting the guide blades in turbines | |
| GB584873A (en) | Improvements in and relating to gas turbines | |
| GB612796A (en) | Improvements in aeroplanes | |
| GB585509A (en) | Improvements in or relating to power plants | |
| GB682627A (en) | Improvements in wind motors having hollow blades with a radial flow of air therethrough | |
| GB1519449A (en) | Gas turbine engine | |
| GB650257A (en) | Improvements in or relating to turbine apparatus | |
| GB794198A (en) | Improvements relating to helicopters | |
| GB636860A (en) | Improvements in or relating to stationary blading for turbines |