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US3872841A Expired / Lapsed US ⏱️ 0.0 years remaining

Construction arrangement of combustion chamber for use in direct fuel injection type diesel engines

Assignee: Isuzu Motors Ltd
•
Filing: 1973-08-24
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Granted: 1975-03-25
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Expires: 1993-08-24
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Abstract

Abstract Herein disclosed are the construction arrangements of a combustion chamber for use in a direct fuel injection type Diesel engine. The combustion chamber is defined by a cylinder liner, a cylinder liner head and a piston being slidable within said cylinder and having a cavity at its crown portion. Means effect swirling motion in the combustion chamber, and a fuel injection nozzle is so attached at a cylinder head that its tip portion is disposed at the upper portion of the combustion chamber at the center of the cavity and has four or eight orifices being open so as to timely inject a metered fuel jet into the combustion chamber. According to a primary feature of the present invention, said cavity has the inner peripheral wall surface comprised of four flat inner side wall surfaces, each being in a straight line having the same length in its horizontal cross-section and respective adjacent straight lines being perpendicular to each other, and four inner corner wall surfaces, each being arcuate in its horizontal cross-section and being interposed between respective adjacent inner side wall surfaces and being so formed that the ratio of the radius of the corner wall surface to that of a circle, which is inscribed with said inner side wall surfaces, is the range of from 0.40 to 0.75. According to a secondary feature, the fuel injection direction of each of said orifices is so defined that fuel is injected from each orifice to the inner peripheral wall surface of the cavity at an angle excepting the range of from 40* to 55* extended from a straight line as a datum line, which is drawn between the center of the inscribed circle and a reference point which is defined by extending two edge lines of adjacent inner side wall surfaces, in the reverse direction to that of said swirling motion.

Inventors

  • 👤 Motoyasu Kimbara
  • 👤 Yoshitaka Yoshida

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-24 19:56
CPC Classifications
F; F02; F02B; F02B23/00; F02B23/02; F02B23/06; F02B23/0645; F02B23/0669; F02B23/0618; F02B23/0624; F02B23/0648; F02B23/0651; F02B23/0678; F02B23/0681; F02B23/0696; F02B2275/00; F02B2275/14; F02B2275/40; F02B3/00; F02B3/06; Y; Y02; Y02T; Y02T10/00; Y02T10/10; Y02T10/12

Claims Analysis

Total Claims: 4
Claim 1
Independent Claim 270 words
In a combustion chamber for use in a Diesel engine of the direct fuel injection type which is defined by a cylinder liner, a cylinder head, a piston being slidable within said cylinder liner and having a cavity at its crown portion, and having means for effecting air swirling in said cavity, and a fuel injection nozzle so attached at a cylinder head that its tip portion is disposed at the upper portion of the combustion chamber at the center of said cavity and having a plurality of orifices so as to timely inject metered fuel jets into said cavity from said orifices radially against said cavity wall, the improvement wherein: said cavity has its inner peripheral wall surface formed by four inner side wall surfaces, each being in a straight line and of the same length in its horizontal cross-section with respective two straight lines adjacent to each other being perpendicular to each other, and four inner corner wall surfaces, each being in a substantially arc in its horizontal cross-section and being interposed between respective two inner side wall surfaces adjacent to each other and being so formed that the ratio of the radius of the arc to that of a circle, which is inscribed with said wall surfaces, is within the range of from 0.40 to 0.75, and wherein: the fuel injection direCtion of each of said orifices is so defined that fuel is injected from each orifice to said straight line peripheral wall surface of said cavity at a slant angle with respect to each side wall surface in the horizontal plane at the point of contact.
Claim 2
Dependent Claim 270 words
In a combustion chamber for use in a Diesel engine of the direct fuel injection type which is defined by a cylinder liner, a cylinder head, a piston being slidable within said cylinder liner and having a cavity at its crown portion, and having means for effecting air swirling in said cavity, and a fuel injection nozzle so attached at a cylinder head that its tip portion is disposed at the upper portion of the combustion chamber at the center of said cavity and having a plurality of orifices so as to timely inject metered fuel jets into said cavity from said orifices radially against said cavity wall, the improvement wherein: said cavity has its inner peripheral wall surface formed by four inner side wall surfaces, each being in a straight line and of the same length in its horizontal cross-section with respective two straight lines adjacent to each other being perpendicular to each other, and four inner corner wall surfaces, each being in a substantially arc in its horizontal cross-section and being interposed between respective two inner side wall surfaces adjacent to each other and being so formed that the ratio of the radius of the arc to that of a circle, which is inscribed with said wall surfaces, is within the range of from 0.40 to 0.75, and wherein: the fuel injection direCtion of each of said orifices is so defined that fuel is injected from each orifice to said straight line peripheral wall surface of said cavity at a slant angle with respect to each side wall surface in the horizontal plane at the point of contact.
Claim 3
Dependent Claim 79 words
The combustion chamber according to claim 1, wherein said slant angle of the fuel injection direction of each orifice is in the range excepting that of from 40* to 55* ; extending from a straight line as a datum line, which is drawn between the center of the inscribed circle and a reference point which is defined by extending two edge lines of said adjacent inner side wall surfaces, in the reverse direction to that of said swirling motion.
Claim 4
Dependent Claim 42 words
The combustion chamber according to claim 2, wherein said angle of the fuel injection direction of each orifice is in the range of from 5* to 25* extended from said datum line in the reverse direction to that of said swirling mortion.

References Cited (Backward Citations)

US2828724A Cited
US2855906A Cited
US3083700A Cited
US3302627A Cited
US3814068A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1978-03-24 1978-09-23 1979-03-25 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1982-03-24 1982-09-23 1983-03-25 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1986-03-24 1986-09-23 1987-03-25 $7700.00 Window Closed / Lapsed

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