GB563749A - Improvements in or relating to internal combustion engines operating on the two-stroke cycle - Google Patents

Improvements in or relating to internal combustion engines operating on the two-stroke cycle

Info

Publication number
GB563749A
GB563749A GB14753/42A GB1475342A GB563749A GB 563749 A GB563749 A GB 563749A GB 14753/42 A GB14753/42 A GB 14753/42A GB 1475342 A GB1475342 A GB 1475342A GB 563749 A GB563749 A GB 563749A
Authority
GB
United Kingdom
Prior art keywords
exhaust
engine
cylinder
manifolds
flow
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
GB14753/42A
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.)
Sulzer AG
Original Assignee
Sulzer AG
Sulzer Freres SA
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 Sulzer AG, Sulzer Freres SA filed Critical Sulzer AG
Publication of GB563749A publication Critical patent/GB563749A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/02Gas passages between engine outlet and pump drive, e.g. reservoirs
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving 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

563,749. Exhaust arrangements for internal-combustion engines. SULZER FRERES SOC. ANON. Oct. 21, 1942, No. 14753. Convention date, Nov. 21, 1941. [Class 7 (ii)] In a multi-cylinder two-stroke internal-combustion engine each cylinder 17 is formed with two opposed exhaust passages 20, 21 leading from it, either passage being closable by a cover 24, Fig. 3, according to the side of the engine from which the exhaust is to be taken. In an opposed piston engine the exhaust ports 13 are controlled by the piston 1. Manifolds 14, 15 are provided, one on each side of the engine, and in conveying the exhaust to an exhaust gas turbine 16 the cylinders are connected to the manifolds in such a way that there is minimum interference between the exhaust of different cylinders. The covers 24 which cover the exhaust passages not required are shaped, as shown at 26, to direct the gas flow. The ports 13 in the cylinder liners are adapted for one direction of exhaust flow and may be rotated, Fig. 3, according to which of the passages 20, 21 is in use. In a modification, Fig. 5, each manifold comprises separate ports 28, 29 and 30, 31 connected to various cylinders so as to provide minimum interference and the cover members extend into close proximity with an unported part of each cylinder liner to obtain a freer flow of exhaust. In another modification, Fig. 7, manifolds 33, 34 on opposite sides of the engine direct exhaust flow in opposite directions, two turbines being preferably employed. The turbine can transmit power to the central gear 11, Fig. 1, of the engine or it may drive a compressor which may also be coupled by gearing to the engine.
GB14753/42A 1941-11-21 1942-10-21 Improvements in or relating to internal combustion engines operating on the two-stroke cycle Expired GB563749A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH563749X 1941-11-21

Publications (1)

Publication Number Publication Date
GB563749A true GB563749A (en) 1944-08-29

Family

ID=4520471

Family Applications (1)

Application Number Title Priority Date Filing Date
GB14753/42A Expired GB563749A (en) 1941-11-21 1942-10-21 Improvements in or relating to internal combustion engines operating on the two-stroke cycle

Country Status (1)

Country Link
GB (1) GB563749A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0373639A1 (en) * 1988-12-14 1990-06-20 Klöckner-Humboldt-Deutz Aktiengesellschaft Exhaust gas conduit system for a supercharged combustion engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0373639A1 (en) * 1988-12-14 1990-06-20 Klöckner-Humboldt-Deutz Aktiengesellschaft Exhaust gas conduit system for a supercharged combustion engine

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