GB670736A - Improvements in or relating to internal combustion turbine power plants - Google Patents
Improvements in or relating to internal combustion turbine power plantsInfo
- Publication number
- GB670736A GB670736A GB1798049A GB1798049A GB670736A GB 670736 A GB670736 A GB 670736A GB 1798049 A GB1798049 A GB 1798049A GB 1798049 A GB1798049 A GB 1798049A GB 670736 A GB670736 A GB 670736A
- Authority
- GB
- United Kingdom
- Prior art keywords
- assemblies
- compressor
- inlet
- passages
- turbine
- 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
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/12—Plants including a gas turbine driving a compressor or a ducted fan characterised by having more than one gas turbine
-
- 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
-
- 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)
- Supercharger (AREA)
Abstract
670,736. Jet propulsion plant. NAPIER & SON, Ltd., D. June 29, 1950 [July 7, 1949], No. 17980/49. Class 110(iii) [Also in Groups XXIV and XXXIII] A turbo-jet comprises three independently operable I.C. turbine assemblies B, C, D which are arranged with their axes on the apices of an isosceles triangle, preferably one having the base larger than the sides, and each assembly comprises a rotary air compressor which receives air direct from the atmosphere through an inlet passage, a turbine which is co-axial with the compressor and one or more combustion chambers therebetween. The assemblies may have a common nozzle, separate nozzles or a nozzle which is subdivided by partitions and one or more exhaust reheaters may be used therein. Each compressor has a separate inlet or, as shown, an inlet which is divided into two passages E<SP>1</SP>, E<SP>2</SP> which merge into three inlets. Auxiliaries positioned in the space bounded by the assemblies, are driven through a differential gearing (see Group XXIV). A cockpit is arranged in the space F bounded by the passages E<SP>1</SP>, E<SP>2</SP>. Specification 593,403 is referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1798049A GB670736A (en) | 1949-07-07 | 1949-07-07 | Improvements in or relating to internal combustion turbine power plants |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1798049A GB670736A (en) | 1949-07-07 | 1949-07-07 | Improvements in or relating to internal combustion turbine power plants |
Publications (1)
Publication Number | Publication Date |
---|---|
GB670736A true GB670736A (en) | 1952-04-23 |
Family
ID=10104564
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1798049A Expired GB670736A (en) | 1949-07-07 | 1949-07-07 | Improvements in or relating to internal combustion turbine power plants |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB670736A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1022912B (en) * | 1953-04-08 | 1958-01-16 | Schmidt Paul | Airplane with a tubular recoil drive that works periodically and with shock wave ignition |
DE1129380B (en) * | 1959-09-17 | 1962-05-10 | Hamburger Flugzeugbau G M B H | Propulsion unit with several jet engines |
EP0147351A1 (en) * | 1983-12-05 | 1985-07-03 | United Technologies Corporation | Bearing support structure |
JP2008106742A (en) * | 2006-10-13 | 2008-05-08 | Snecma | Turbojet engine auxiliary machine gear box drive shaft, and modular additional auxiliary machine |
-
1949
- 1949-07-07 GB GB1798049A patent/GB670736A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1022912B (en) * | 1953-04-08 | 1958-01-16 | Schmidt Paul | Airplane with a tubular recoil drive that works periodically and with shock wave ignition |
DE1129380B (en) * | 1959-09-17 | 1962-05-10 | Hamburger Flugzeugbau G M B H | Propulsion unit with several jet engines |
EP0147351A1 (en) * | 1983-12-05 | 1985-07-03 | United Technologies Corporation | Bearing support structure |
JP2008106742A (en) * | 2006-10-13 | 2008-05-08 | Snecma | Turbojet engine auxiliary machine gear box drive shaft, and modular additional auxiliary machine |
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