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US3644070A Expired / Lapsed US ⏱️ 0.0 years remaining

Cooling circuit for rotary piston internal combustion engines

Assignee: SOC D CONST ET D EXPLOIT DE MA
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Filing: 1969-09-30
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Granted: 1972-02-22
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Expires: 1989-09-30
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Abstract

Abstract The casing comprises a peripheral envelope having an inlet orifice, an exhaust orifice and spark plug wells. This envelope is cooled in its hot zone by a liquid circulating in a part of the cooling circuit. The successive cross sections of that part of the circuit are such that, at each cooled point of the envelope, the thermal exchanges take place in conditions of convection situated in the range 10* to 20* C. below the beginning of the nuclear ebullition conditions.

Inventors

  • 👤 Lucien Lermusiaux

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-07 18:11
CPC Classifications
F; F02; F02B; F02B55/00; F02B55/02; F02B55/04; F02B55/08; F02B55/10; F02B1/00; F02B1/02; F02B1/04; F02B53/00; F02B2053/005

Claims Analysis

Total Claims: 7
Claim 1
Independent Claim 253 words
A rotary piston internal combustion engine in which a peripheral envelope and lateral cheeks form a casing for the piston, said envelope having inner and outer surfaces and having at least one active part through which relatively high heat fluxes have to be removed, at least one passage for flow of a liquid coolant therethrough being arranged between Said inner and outer surfaces so as to traverse at least one said active part of the envelope, said passages having successive sections of predetermined cross-sectional areas in said active parts, said cross sections being predetermined from the heat flux characteristics of the coolant liquid, so that under normal operating conditions thermal exchange at any cooled point of the envelope takes place under conditions of convection and so that the temperature difference between the envelope and the liquid is smaller by a substantially constant value than the temperature difference corresponding to transition from said convection conditions to thermal exchange under substantially nuclear ebullition conditions, wherein said passage is arranged in the neighborhood of said inner surface, and comprised between two cylindrical surfaces, the first of which is substantially parallel to said inner surface, and the second of which surrounds the first at a distance depending on the cross section of the passage, said two cylindrical surfaces being connected together by ribs which are substantially parallel to the mean plane perpendicular to the generatrixes of said cylindrical surfaces, said ribs being disposed in staggered relation with respect to said plane, said cheeks limiting said passage laterally.
Claim 2
Dependent Claim 253 words
A rotary piston internal combustion engine in which a peripheral envelope and lateral cheeks form a casing for the piston, said envelope having inner and outer surfaces and having at least one active part through which relatively high heat fluxes have to be removed, at least one passage for flow of a liquid coolant therethrough being arranged between Said inner and outer surfaces so as to traverse at least one said active part of the envelope, said passages having successive sections of predetermined cross-sectional areas in said active parts, said cross sections being predetermined from the heat flux characteristics of the coolant liquid, so that under normal operating conditions thermal exchange at any cooled point of the envelope takes place under conditions of convection and so that the temperature difference between the envelope and the liquid is smaller by a substantially constant value than the temperature difference corresponding to transition from said convection conditions to thermal exchange under substantially nuclear ebullition conditions, wherein said passage is arranged in the neighborhood of said inner surface, and comprised between two cylindrical surfaces, the first of which is substantially parallel to said inner surface, and the second of which surrounds the first at a distance depending on the cross section of the passage, said two cylindrical surfaces being connected together by ribs which are substantially parallel to the mean plane perpendicular to the generatrixes of said cylindrical surfaces, said ribs being disposed in staggered relation with respect to said plane, said cheeks limiting said passage laterally.
Claim 3
Dependent Claim 19 words
A rotary piston engine according to claim 1, wherein the substantially constant value is between 10* and 20* C.
Claim 4
Dependent Claim 44 words
An envelope adapted to form part of a rotary piston engine according to claim 1, further comprising holes adapted for the passage of fastening means for fastening said cheeks to the envelope, these holes being situated radially outside said active part of the envelope.
Claim 5
Dependent Claim 39 words
A rotary piston engine according to claim 1, wherein said inner surface has a profile in the form of a trochoid having two lobes, the rotary piston having a transverse cross section in the form of a curvilinear triangle.
Claim 6
Dependent Claim 85 words
A rotary piston engine according to claim 4 comprising at least one spark plug, said envelope defining a well extending radially and housing said spark plug in the casing, wherein, in said active part, in the region of the spark plug well, the cross section of the passage for the coolant liquid is of increased area, said cylindrical surfaces being more separated radially in order to compensate for the loss in cross-sectional area of the passage due to the presence of said spark plug well.
Claim 7
Dependent Claim 60 words
A rotary piston engine according to claim 5 comprising two spark plugs, wherein a central rib connects the two cylindrical surfaces between the spark plug wells, and wherein, in order to compensate for the decreased strength of the envelope in the region of this central rib, the inner surface of the envelope is supported by a wall of increased thickness.

References Cited (Backward Citations)

US3007460A Cited
US3102516A Cited
US3323501A Cited
US3319612A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1975-02-21 1975-08-23 1976-02-22 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1979-02-21 1979-08-23 1980-02-22 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1983-02-21 1983-08-23 1984-02-22 $7700.00 Window Closed / Lapsed

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