GB321933A - Improvements in or relating to motor vehicles - Google Patents

Improvements in or relating to motor vehicles

Info

Publication number
GB321933A
GB321933A GB14773/28A GB1477328A GB321933A GB 321933 A GB321933 A GB 321933A GB 14773/28 A GB14773/28 A GB 14773/28A GB 1477328 A GB1477328 A GB 1477328A GB 321933 A GB321933 A GB 321933A
Authority
GB
United Kingdom
Prior art keywords
water
air
turbine
compressor
reservoir
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
GB14773/28A
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
Priority to GB14773/28A priority Critical patent/GB321933A/en
Publication of GB321933A publication Critical patent/GB321933A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60G—VEHICLE SUSPENSION ARRANGEMENTS
    • B60G11/00—Resilient suspensions characterised by arrangement, location or kind of springs
    • B60G11/26—Resilient suspensions characterised by arrangement, location or kind of springs having fluid springs only, e.g. hydropneumatic springs
    • B60G11/27—Resilient suspensions characterised by arrangement, location or kind of springs having fluid springs only, e.g. hydropneumatic springs wherein the fluid is a gas
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02G—HOT GAS OR COMBUSTION-PRODUCT POSITIVE-DISPLACEMENT ENGINE PLANTS; USE OF WASTE HEAT OF COMBUSTION ENGINES; NOT OTHERWISE PROVIDED FOR
    • F02G5/00—Profiting from waste heat of combustion engines, not otherwise provided for
    • F02G5/02—Profiting from waste heat of exhaust gases
    • F02G5/04—Profiting from waste heat of exhaust gases in combination with other waste heat from combustion engines
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Air-Conditioning For Vehicles (AREA)
  • Jet Pumps And Other Pumps (AREA)

Abstract

321,933. Monnot, J. F. May 19, 1928. Compressing and distributing air for uses other than propulsion.-The exhaust manifold 3 is connected through a valve 5 and water-jacketed chambers 4, 9 to a turbine 21 which drives an air-compressor 22 and water pump 23. Valved injection nozzles 6, 10, 18 introduce compressed air, compressed air and oil, and water, respectively into the chambers, from which a. mixture of steam and gas issues to drive the turbine. The compressor 20 supplies a reservoir 26 from which pipes pass to the nozzles 6, 10 and to appliances such as the horn, windscreen wiper, engine-starter, tyre inflator, &c. In practice boxlike parts of the frame longitudinals form the reservoir 26. The pump 23 maintains a circulation through a tank 41, radiator 38 and waterjackets 15.
GB14773/28A 1928-05-19 1928-05-19 Improvements in or relating to motor vehicles Expired GB321933A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB14773/28A GB321933A (en) 1928-05-19 1928-05-19 Improvements in or relating to motor vehicles

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB14773/28A GB321933A (en) 1928-05-19 1928-05-19 Improvements in or relating to motor vehicles

Publications (1)

Publication Number Publication Date
GB321933A true GB321933A (en) 1929-11-19

Family

ID=10047221

Family Applications (1)

Application Number Title Priority Date Filing Date
GB14773/28A Expired GB321933A (en) 1928-05-19 1928-05-19 Improvements in or relating to motor vehicles

Country Status (1)

Country Link
GB (1) GB321933A (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2421518A (en) * 1940-07-05 1947-06-03 United Aircraft Corp Jet propulsion
US2485655A (en) * 1944-07-21 1949-10-25 Edwin H Polk Exhaust turbine driven fan and supercharger
US2583651A (en) * 1945-08-14 1952-01-29 Jr Arthur Fredrick Horning Airplane power plant with direct cooling of exhaust valves
US2608058A (en) * 1946-06-10 1952-08-26 Leon J Geeraert Combustion chamber with sliding valve controlling fuel, air, and water admission
US2648189A (en) * 1948-04-06 1953-08-11 Goetaverken Ab Internal-combustion engine and pneumatic transmission drive
US2654991A (en) * 1950-09-09 1953-10-13 Nettel Frederick Control for engine turbosupercharger systems
US2713243A (en) * 1946-10-23 1955-07-19 Curtiss Wright Corp Rocket and turbine engine combination for aircraft
US3513929A (en) * 1967-08-25 1970-05-26 Exxon Research Engineering Co Low-polluting engine and drive system
US3849988A (en) * 1972-04-06 1974-11-26 France Etat Combustion chambers for internal combustion engines equipped with a turbo-compressor unit with reheating upstream of the turbine
US4896505A (en) * 1989-01-03 1990-01-30 Holleyman John E Pressurized-fluid-operated engine

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2421518A (en) * 1940-07-05 1947-06-03 United Aircraft Corp Jet propulsion
US2485655A (en) * 1944-07-21 1949-10-25 Edwin H Polk Exhaust turbine driven fan and supercharger
US2583651A (en) * 1945-08-14 1952-01-29 Jr Arthur Fredrick Horning Airplane power plant with direct cooling of exhaust valves
US2608058A (en) * 1946-06-10 1952-08-26 Leon J Geeraert Combustion chamber with sliding valve controlling fuel, air, and water admission
US2713243A (en) * 1946-10-23 1955-07-19 Curtiss Wright Corp Rocket and turbine engine combination for aircraft
US2648189A (en) * 1948-04-06 1953-08-11 Goetaverken Ab Internal-combustion engine and pneumatic transmission drive
US2654991A (en) * 1950-09-09 1953-10-13 Nettel Frederick Control for engine turbosupercharger systems
US3513929A (en) * 1967-08-25 1970-05-26 Exxon Research Engineering Co Low-polluting engine and drive system
US3849988A (en) * 1972-04-06 1974-11-26 France Etat Combustion chambers for internal combustion engines equipped with a turbo-compressor unit with reheating upstream of the turbine
US4896505A (en) * 1989-01-03 1990-01-30 Holleyman John E Pressurized-fluid-operated engine

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