GB800661A - Improvements in or relating to air turbines - Google Patents
Improvements in or relating to air turbinesInfo
- Publication number
- GB800661A GB800661A GB1818855A GB1818855A GB800661A GB 800661 A GB800661 A GB 800661A GB 1818855 A GB1818855 A GB 1818855A GB 1818855 A GB1818855 A GB 1818855A GB 800661 A GB800661 A GB 800661A
- Authority
- GB
- United Kingdom
- Prior art keywords
- air
- turbine
- gas turbine
- twotier
- june
- 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
- F02C7/32—Arrangement, mounting, or driving, of auxiliaries
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
Abstract
800,661. Air turbines; gas turbine plant. PLESSEY CO., Ltd. June 22, 1956 [June 23, 1955], No. 18188/55. Class 110 (3). In an air turbine for use as an auxiliary source . of power in an aircraft having a gas turbine installation, the air turbine is provided with twotier inlet nozzle guide vanes f, g and with twotier rotor blades b, c and air under pressure tapped from the compressor of the gas turbine installation flows through the outer portions g, c of the turbine guide vanes and rotor blades while ram air flows through the inner portions f, b. The air under pressure is led through a duct l controlled by a valve m, while the ram air is led through a duct from an intake in the aircraft fuselage n controlled by a valve device p.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1818855A GB800661A (en) | 1955-06-23 | 1955-06-23 | Improvements in or relating to air turbines |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1818855A GB800661A (en) | 1955-06-23 | 1955-06-23 | Improvements in or relating to air turbines |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB800661A true GB800661A (en) | 1958-08-27 |
Family
ID=10108172
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1818855A Expired GB800661A (en) | 1955-06-23 | 1955-06-23 | Improvements in or relating to air turbines |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB800661A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2235018A (en) * | 1989-05-13 | 1991-02-20 | Messerschmitt Boelkow Blohm | Device for air cooling and the provision of mechanical power |
-
1955
- 1955-06-23 GB GB1818855A patent/GB800661A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2235018A (en) * | 1989-05-13 | 1991-02-20 | Messerschmitt Boelkow Blohm | Device for air cooling and the provision of mechanical power |
| GB2235018B (en) * | 1989-05-13 | 1993-11-24 | Messerschmitt Boelkow Blohm | Device for air cooling and provision of mechanical power |
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