GB128625A - Improvements in Means for Regulating Internal-combustion Engines. - Google Patents

Improvements in Means for Regulating Internal-combustion Engines.

Info

Publication number
GB128625A
GB128625A GB11673/17A GB1167317A GB128625A GB 128625 A GB128625 A GB 128625A GB 11673/17 A GB11673/17 A GB 11673/17A GB 1167317 A GB1167317 A GB 1167317A GB 128625 A GB128625 A GB 128625A
Authority
GB
United Kingdom
Prior art keywords
blower
air
turbine
leading
valve
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
Application number
GB11673/17A
Inventor
Auguste Rateau
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Publication of GB128625A publication Critical patent/GB128625A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/12—Control of the pumps
    • F02B37/18—Control of the pumps by bypassing exhaust from the inlet to the outlet of turbine or to the atmosphere
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B33/00—Engines characterised by provision of pumps for charging or scavenging
    • F02B33/44—Passages conducting the charge from the pump to the engine inlet, e.g. reservoirs
    • F02B33/446—Passages conducting the charge from the pump to the engine inlet, e.g. reservoirs having valves for admission of atmospheric air to engine, e.g. at starting
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B39/00—Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00
    • F02B39/005—Cooling of pump drives
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/10—Internal combustion engine [ICE] based vehicles
    • Y02T10/12—Improving ICE efficiencies

Abstract

128,625. Rateau, A. Dec. 7, 1916, [Convention date]. Regulating.-Engines for aircraft are charged with air under pressure by a blower B actuated by a turbine D driven by exhaust gases from an internal-combustion engine A. The air is delivered to a carburettor C, and in the event of the blower being out of action, or delivering less than an adequate charge, supplementary air is drawn in through an automatic valve 8. The blower may be put out of action wholly or in part, by bypassing the exhaust gases through a valve 9 leading to the atmosphere. The valve may be controlled by hand, or automatically by a flexible diaphragm 20 open on one side to the atmosphere and on the other side acted upon by air at normal atmospheric pressure. The pipes leading to the turbine and from the blower have cooling-fins 11, 15 respectively. To prevent overheating of the turbine, cooling-air is supplied through a pipe 6 leading from the discharge pipe 4 of the blower. In a gas-engine, the gas is supplied by a separate blower.
GB11673/17A 1916-12-07 1917-08-14 Improvements in Means for Regulating Internal-combustion Engines. Expired GB128625A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR128625X 1916-12-07

Publications (1)

Publication Number Publication Date
GB128625A true GB128625A (en) 1919-07-03

Family

ID=32339391

Family Applications (1)

Application Number Title Priority Date Filing Date
GB11673/17A Expired GB128625A (en) 1916-12-07 1917-08-14 Improvements in Means for Regulating Internal-combustion Engines.

Country Status (1)

Country Link
GB (1) GB128625A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE894483C (en) * 1942-07-25 1954-06-14 Karl Dr-Ing Leist Speed limitation in altitude operation for loaders with adjustable speed

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE894483C (en) * 1942-07-25 1954-06-14 Karl Dr-Ing Leist Speed limitation in altitude operation for loaders with adjustable speed

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