GB384340A - An improved method of and means for effecting combustion in internal combustion engin - Google Patents

An improved method of and means for effecting combustion in internal combustion engin

Info

Publication number
GB384340A
GB384340A GB16659/31A GB1665931A GB384340A GB 384340 A GB384340 A GB 384340A GB 16659/31 A GB16659/31 A GB 16659/31A GB 1665931 A GB1665931 A GB 1665931A GB 384340 A GB384340 A GB 384340A
Authority
GB
United Kingdom
Prior art keywords
plug
air
passage
chamber
fuel
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
GB16659/31A
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.)
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 GB16659/31A priority Critical patent/GB384340A/en
Publication of GB384340A publication Critical patent/GB384340A/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
    • F02B19/00Engines characterised by precombustion chambers
    • F02B19/08Engines characterised by precombustion chambers the chamber being of air-swirl type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B19/00Engines characterised by precombustion chambers
    • F02B2019/006Engines characterised by precombustion chambers with thermal insulation
    • 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)
  • Combustion Methods Of Internal-Combustion Engines (AREA)

Abstract

384,340. Oil engines. RICARDO, H. R., 21, Suffolk Street, Pall Mall, London. June 8, 1931, No. 16659. [Class 7 (iii).] In a compressionignition engine of the type in which substantially the whole of the air charge is forced into a spherical offset combustion chamber F during the compression stroke, the fuel is discharged by an injector H in a compact stream which passes through the centre of the chamber and impinges on an uncooled plug G, which forms the lower portion of the combustion chamber, at a spot adjacent to a tapering passage G<4> through which the air is forced tangentially into the chamber ; the circumferential portions of the rotating air charge are thus brought progressively into contact with the fuel spray as it impinges on the plug so that the air and fuel are thoroughly mixed immediately before the charge reaches the inner end of the passage G<4>, and the tendency for unconsumed air to be driven out of the chamber is reduced. No fuel is injected directly into the end of the passage. The passage may be of circular cross section throughout, or it may change to a crescent or kidney shape towards its inner end, the area of the latter end being preferably three-fifths that at the outer. Instead of the passage traversing the plug, it may be formed by a groove cut in the outer cylindrical surface of the plug, the direction of rotation of the charge thus being opposite to that obtaining in Fig. 1. The plug G is made of a heat-resisting metal of low heat conductivity ; it is fitted loosely in the mouth of a water-cooled pocket so that it is surrounded by a heat insulating air-space F<1>. A retaining ring G<2> may be optionally provided, the off-set of the plug ensuring sufficient overlap between the cylinder end and plug to retain the latter if the ring is omitted. In the modified construction shown in Fig. 3, the upper portion of the combustion chamber is provided with a liner K which is insulated from the watercooled pocket by an air gap ; the liner is supported by an integral boss K<1> which passes through a bore in the wall of the pocket and is secured by a ring K<2>. An electrically heated hot wire J is employed at starting. The injector socket passes through the water jacket chamber of the cylinder head to ensure adequate cooling. Specification 371,025 is referred to.
GB16659/31A 1931-06-08 1931-06-08 An improved method of and means for effecting combustion in internal combustion engin Expired GB384340A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB16659/31A GB384340A (en) 1931-06-08 1931-06-08 An improved method of and means for effecting combustion in internal combustion engin

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB16659/31A GB384340A (en) 1931-06-08 1931-06-08 An improved method of and means for effecting combustion in internal combustion engin

Publications (1)

Publication Number Publication Date
GB384340A true GB384340A (en) 1932-12-08

Family

ID=10081294

Family Applications (1)

Application Number Title Priority Date Filing Date
GB16659/31A Expired GB384340A (en) 1931-06-08 1931-06-08 An improved method of and means for effecting combustion in internal combustion engin

Country Status (1)

Country Link
GB (1) GB384340A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113969846A (en) * 2021-11-01 2022-01-25 安徽航瑞航空动力装备有限公司 Engine cylinder head and method of assembling the same

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113969846A (en) * 2021-11-01 2022-01-25 安徽航瑞航空动力装备有限公司 Engine cylinder head and method of assembling the same

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