GB584169A - Improvements in or relating to power plants for aircraft - Google Patents
Improvements in or relating to power plants for aircraftInfo
- Publication number
- GB584169A GB584169A GB2489844A GB2489844A GB584169A GB 584169 A GB584169 A GB 584169A GB 2489844 A GB2489844 A GB 2489844A GB 2489844 A GB2489844 A GB 2489844A GB 584169 A GB584169 A GB 584169A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- jet
- engine
- clutch
- relating
- 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
- F02K—JET-PROPULSION PLANTS
- F02K5/00—Plants including an engine, other than a gas turbine, driving a compressor or a ducted fan
- F02K5/02—Plants including an engine, other than a gas turbine, driving a compressor or a ducted fan the engine being of the reciprocating-piston type
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Supercharger (AREA)
Abstract
584,169. Gas turbine plant. FAIREY AVIATION CO., Ltd., CHAPLIN, H. E., and GOTT, G. E. Dec. 12, 1944, No. 24898. [Class 110 (iii)] [Also in Group XXXIII] An aircraft power plant comprises an I.C. engine a' which drives a propeller c through a clutch d. This engine also drives an aircompressor f through a two speed gear-box or clutch o. The compressor supplies air to the combustion chamber of the jet m. This jet is augmented by the engine exhaust to the subsidiary jets t. The plant can be used at will to drive the aircraft by the propeller alone, by the jet alone, or both siinultaneously.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2489844A GB584169A (en) | 1944-12-12 | 1944-12-12 | Improvements in or relating to power plants for aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2489844A GB584169A (en) | 1944-12-12 | 1944-12-12 | Improvements in or relating to power plants for aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB584169A true GB584169A (en) | 1947-01-08 |
Family
ID=10219004
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB2489844A Expired GB584169A (en) | 1944-12-12 | 1944-12-12 | Improvements in or relating to power plants for aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB584169A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2591676A (en) * | 1948-12-17 | 1952-04-08 | Jr Harry H Clayton | Ejector cooling shroud for use on the exhaust systems of turbojet aircraft engines |
| US2593541A (en) * | 1947-04-03 | 1952-04-22 | Napier & Son Ltd | Cooling apparatus for use with aero or other engines |
| EP2488736A4 (en) * | 2009-10-18 | 2015-06-10 | Israel Hirshberg | Use of hot gases and devices |
-
1944
- 1944-12-12 GB GB2489844A patent/GB584169A/en not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2593541A (en) * | 1947-04-03 | 1952-04-22 | Napier & Son Ltd | Cooling apparatus for use with aero or other engines |
| US2591676A (en) * | 1948-12-17 | 1952-04-08 | Jr Harry H Clayton | Ejector cooling shroud for use on the exhaust systems of turbojet aircraft engines |
| EP2488736A4 (en) * | 2009-10-18 | 2015-06-10 | Israel Hirshberg | Use of hot gases and devices |
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