GB132049A - - Google Patents
Info
- Publication number
- GB132049A GB132049A GB132049DA GB132049A GB 132049 A GB132049 A GB 132049A GB 132049D A GB132049D A GB 132049DA GB 132049 A GB132049 A GB 132049A
- Authority
- GB
- United Kingdom
- Prior art keywords
- air
- engine
- fixed
- exhaust gases
- blades
- 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.)
- Active
Links
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N13/00—Exhaust or silencing apparatus characterised by constructional features ; Exhaust or silencing apparatus, or parts thereof, having pertinent characteristics not provided for in, or of interest apart from, groups F01N1/00 - F01N5/00, F01N9/00, F01N11/00
- F01N13/06—Exhaust or silencing apparatus characterised by constructional features ; Exhaust or silencing apparatus, or parts thereof, having pertinent characteristics not provided for in, or of interest apart from, groups F01N1/00 - F01N5/00, F01N9/00, F01N11/00 specially adapted for star-arrangement of cylinders, e.g. exhaust manifolds
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01P—COOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
- F01P7/00—Controlling of coolant flow
- F01P7/02—Controlling of coolant flow the coolant being cooling-air
- F01P7/04—Controlling of coolant flow the coolant being cooling-air by varying pump speed, e.g. by changing pump-drive gear ratio
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Jet Pumps And Other Pumps (AREA)
Abstract
132,049. Lake, C. J. Sept. 9, 1918. motor power plant.-Relates to motor installations for aircraft &c. wherein the exhaust gases from an internal-combustion engine are delivered together with additional air to the blades of an auxiliary turbine. The exhaust gases from a radial-cylinder rotary engine 2 discharge through nozzles 14 located in air tubes 15 disposed so as to receive a swift current of air, which together with the gases is led to the fixed and moving blades 12, 13 of a turbine having screw spokes 13<a> mounted on the sleeve 6 of the engine, which is mounted within a casing 16. Cooling and scavenging are thereby facilitated. Any number of sets of fixed and moving blades may be used. The cylinders may be non-rotary, and the arrangement of the air tubes may be modified.
Publications (1)
Publication Number | Publication Date |
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GB132049A true GB132049A (en) |
Family
ID=1725556
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB132049D Active GB132049A (en) |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB132049A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE767078C (en) * | 1934-02-23 | 1951-10-29 | Karl Leist Dr Ing | Partly pressurized combustion or exhaust gas turbine |
DE767617C (en) * | 1938-04-19 | 1953-01-26 | Milo Ab | Aircraft propulsion with propeller drive by an internal combustion engine and a turbine driven by exhaust gases from the internal combustion engine |
DE767871C (en) * | 1937-07-02 | 1954-03-22 | Messerschmitt Boelkow Blohm | Device for the improved utilization of the energy of the exhaust gases in internal combustion engines for propulsion of aircraft |
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0
- GB GB132049D patent/GB132049A/en active Active
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE767078C (en) * | 1934-02-23 | 1951-10-29 | Karl Leist Dr Ing | Partly pressurized combustion or exhaust gas turbine |
DE767871C (en) * | 1937-07-02 | 1954-03-22 | Messerschmitt Boelkow Blohm | Device for the improved utilization of the energy of the exhaust gases in internal combustion engines for propulsion of aircraft |
DE767617C (en) * | 1938-04-19 | 1953-01-26 | Milo Ab | Aircraft propulsion with propeller drive by an internal combustion engine and a turbine driven by exhaust gases from the internal combustion engine |
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