GB377168A - Improvements in internal combustion engines - Google Patents

Improvements in internal combustion engines

Info

Publication number
GB377168A
GB377168A GB1317/31A GB131731A GB377168A GB 377168 A GB377168 A GB 377168A GB 1317/31 A GB1317/31 A GB 1317/31A GB 131731 A GB131731 A GB 131731A GB 377168 A GB377168 A GB 377168A
Authority
GB
United Kingdom
Prior art keywords
turbine
engine
rotary
jan
combustion
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
GB1317/31A
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.)
GEORG DREHER
Original Assignee
GEORG DREHER
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 GEORG DREHER filed Critical GEORG DREHER
Publication of GB377168A publication Critical patent/GB377168A/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
    • F02B41/00—Engines characterised by special means for improving conversion of heat or pressure energy into mechanical power
    • F02B41/02—Engines with prolonged expansion
    • F02B41/10—Engines with prolonged expansion in exhaust turbines
    • 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
    • F02B37/02—Gas passages between engine outlet and pump drive, e.g. reservoirs
    • 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
    • F02B3/00—Engines characterised by air compression and subsequent fuel addition
    • F02B3/06—Engines characterised by air compression and subsequent fuel addition with compression ignition
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)

Abstract

377,168. Motor power plant. DREHER, G., 31, Lyckallee, Charlottenburg, Berlin. Jan. 14, 1931, No. 1317. Convention date, Jan. 14, 1930. Void [Published under Sect. 91 of the Acts]. [Class 110 (iii).] A jet wheel turbine 3 operates in the cylinder head of an internal - combustion engine 1 and is actuated by combustion gases during the working and exhaust strokes of the engine. The gases pass to the turbine through a rotary valve 6. The turbine shaft is parallel to the engine crank shaft and is mechanically coupled to it. For a multicylinder engine, a series of jet wheels 4 operate on one rotor. Rotary inlet valves 10 supply fuel to a combustion chamber 2, and the exhaustgases from the turbine leave through a port 8. In a modified arrangement the turbine is attached to two cylinders each lying at an angle to the plane of symmetry which passes through the turbine axis. A flywheel for the engine may be omitted due to the rotary effect of the turbine.
GB1317/31A 1930-01-14 1931-01-14 Improvements in internal combustion engines Expired GB377168A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE377168X 1930-01-14

Publications (1)

Publication Number Publication Date
GB377168A true GB377168A (en) 1932-07-21

Family

ID=6344376

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1317/31A Expired GB377168A (en) 1930-01-14 1931-01-14 Improvements in internal combustion engines

Country Status (1)

Country Link
GB (1) GB377168A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2013179054A2 (en) * 2012-05-31 2013-12-05 SMITH, Andrew N P An internal combustion engine and a method of operating an internal combustion engine

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2013179054A2 (en) * 2012-05-31 2013-12-05 SMITH, Andrew N P An internal combustion engine and a method of operating an internal combustion engine
WO2013179054A3 (en) * 2012-05-31 2014-03-06 SMITH, Andrew N P An internal combustion engine and a method of operating an internal combustion engine
GB2518097A (en) * 2012-05-31 2015-03-11 Khalil Abu Al-Rubb An internal combustion engine and a method of operating an internal combustion engine
US9714607B2 (en) 2012-05-31 2017-07-25 Khalil Abu Al-Rubb Internal combustion engine and a method of operating an internal combustion engine
GB2518097B (en) * 2012-05-31 2018-07-18 Khalil Abu Al Rubb An internal combustion engine and a method of operating an internal combustion engine

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