GB132049A - - Google Patents

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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
Application number
Publication of GB132049A publication Critical patent/GB132049A/en
Active legal-status Critical Current

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Classifications

    • 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.
GB132049D Active GB132049A (en)

Publications (1)

Publication Number Publication Date
GB132049A true GB132049A (en)

Family

ID=1725556

Family Applications (1)

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Country Status (1)

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GB (1) GB132049A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
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

Cited By (3)

* Cited by examiner, † Cited by third party
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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