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US3814066A Expired / Lapsed US ⏱️ 0.0 years remaining

Air compressing internal combustion engine with direct injection

Assignee: MAN AG
•
Filing: 1971-07-28
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Granted: 1974-06-04
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Expires: 1991-07-28
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Abstract

Abstract An air compressing direct injection internal combustion engine in which either the reciprocatory piston or the pertaining cylinder head has a ball-shaped combustion chamber therein which is provided with a neck that is constricted with regard to the diameter of said combustion chamber and which is adapted so to receive the combustion air as to circulate the same in said combustion chamber, the ratio of the diameter of the said combustion chamber to the diameter of said neck being less than or at the maximum equalling 1.15 while the fuel injection nozzle is so directed toward the inside of said combustion chamber that the point of impact of the fuel jet upon the inside surface of said combustion chamber is located in that quarter of the combustion chamber which is remote from and opposite to said constriction.

Inventors

  • 👤 J Lohr

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-05 18:28
CPC Classifications
F; F02; F02B; F02B23/00; F02B23/02; F02B23/06; F02B23/0645; F02B23/066; F02B23/0675; F02B2275/00; F02B2275/14; F02B23/0618; F02B23/0621; F02B23/0624; F02B23/0648; F02B23/0651; F02B3/00; F02B3/06; Y; Y02; Y02T; Y02T10/00; Y02T10/10; Y02T10/12

Claims Analysis

Total Claims: 2
Claim 1
Independent Claim 248 words
An air compressing direct injection internal combustion engine having a reciprocatory piston forming a first element and having a pertaining cylinder head forming a second element, one of said elements being provided with a ball-shaped combustion chamber which has a neck that is constricted with regard to the diameter of said combustion chamber and which is adapted to receive the combustion air as to circulate the same in said combustion chamber, the ratio of the diameter of said combustion chamber to the diameter of said neck not exceeding 1.15, said engine also having a fuel injection nozzle associated with said combustion chamber and so directed toward the inside of said combustion chamber that the fuel jet injected by said fuel injection nozzle passes through a plane which is parallel to said neck and is spaced from the opposite end of said chamber onefourth of the distance from said end to said neck and to a point of impact upon the inside surface of said combustion chamber between said plane and said end to form a thin film of fuel on the wall of said chamber which is removed in vapor form through circulating combustion air, the ratio of the circumferential velocity of the air charge in said combustion chamber to the axial apeed of said air charge being not in excess of 4, said circumferential velocity with reference to said measuring diameter (0.7 cylinder diameter) and to maximum valve stroke substantially equalling the mean velocity of said piston.
Claim 2
Dependent Claim 248 words
An air compressing direct injection internal combustion engine having a reciprocatory piston forming a first element and having a pertaining cylinder head forming a second element, one of said elements being provided with a ball-shaped combustion chamber which has a neck that is constricted with regard to the diameter of said combustion chamber and which is adapted to receive the combustion air as to circulate the same in said combustion chamber, the ratio of the diameter of said combustion chamber to the diameter of said neck not exceeding 1.15, said engine also having a fuel injection nozzle associated with said combustion chamber and so directed toward the inside of said combustion chamber that the fuel jet injected by said fuel injection nozzle passes through a plane which is parallel to said neck and is spaced from the opposite end of said chamber onefourth of the distance from said end to said neck and to a point of impact upon the inside surface of said combustion chamber between said plane and said end to form a thin film of fuel on the wall of said chamber which is removed in vapor form through circulating combustion air, the ratio of the circumferential velocity of the air charge in said combustion chamber to the axial apeed of said air charge being not in excess of 4, said circumferential velocity with reference to said measuring diameter (0.7 cylinder diameter) and to maximum valve stroke substantially equalling the mean velocity of said piston.

References Cited (Backward Citations)

US2305801A Cited
US2767692A Cited
US2982270A Cited
US2921566A Cited
US2975773A Cited
US3085557A Cited
US2959160A Cited
US3424137A Cited
DE2004536A1 Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1977-06-03 1977-12-03 1978-06-04 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1981-06-03 1981-12-03 1982-06-04 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1985-06-03 1985-12-03 1986-06-04 $7700.00 Window Closed / Lapsed

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