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US3895889A Expired / Lapsed US ⏱️ 0.0 years remaining

Liquid cooling system for rotary internal combustion engine

Assignee: Rotary Power International Inc
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Filing: 1974-03-04
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Granted: 1975-07-22
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Expires: 1994-03-04
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Abstract

Abstract The improved liquid cooling system is for a rotary internal combustion engine having a substantially trochoidal shaped housing cavity in which a rotor planetates, the engine being so constructed and disposed that the area of highest heat flux extends vertically along one side of the engine and substantially parallel to the major axis of the housing cavity. The cooling system comprises coolant inlet means and coolant outlet means disposed in the housing respectively below and above the minor axis of the housing cavity and a plurality of parallel passages in the housing adjacent the area of highest heat flux and extending substantially parallel to the longitudinal axis of the mainshaft, which passages are interconnected end-to-end for providing serial flow of coolant through successive passages from the inlet means to the outlet means so that flow of coolant is promoted by convection.

Inventors

  • 👤 Jr Robert W Loyd
  • 👤 Charles Lombaerde

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-30 19:15
CPC Classifications
F; F01; F01C; F01C21/00; F01C21/06

Claims Analysis

Total Claims: 5
Claim 1
Independent Claim 331 words
In a rotary internal combustion engine in which a rotor is eccentrically mounted on a mainshaft so that the rotor planetates within a multi-lobed, substantially trochoidal shaped cavity formed within the housing of the engine and which engine is disposed in its normal operative position with the major and minor axes of the cavity respectively extending substantially vertically and parallel to a horizontal plane and wherein combustion occurs in the area adjacent one of the lobe junctures so that the area of highest heat flux extends substantially along one side of the housing parallel to the major axis of said cavity, a cooling system for the housing of said engine comprising: a. a plurality of first cooling passageways in the housing adjacent the area where the highest heat flux is produced and extending substantially parallel to the longitudinal axis of said mainshaft; b. header means forming chambers in the housing at the opposite ends of said housing to connect said first cooling passageways together end-to-end to provide for series flow of coolant through each of said plurality of first cooling passageways from one end of the housing to the other and upwardly adjacent said area of highest heat flux; c. inlet means in the housing at a point below the minor axis of the trochoidal cavity and adjacent the combustion exhaust gas discharge means to communicate said first cooling passageways to a source of coolant to supply the first cooling passageways with coolant; d. outlet means in the housing at a point above the minor axis to communicate with said first cooling passageways and receive heated coolant from the latter; e. second cooling passageways in the housing adjacent the area where the lowest heat flux is produced and extending substantially parallel to the longitudinal axis of the mainshaft and communicating with said outlet means; and f. by-pass means downstream from said inlet means for passing a portion of the coolant passing through said first cooling passageways into said second cooling passageways.
Claim 2
Dependent Claim 331 words
In a rotary internal combustion engine in which a rotor is eccentrically mounted on a mainshaft so that the rotor planetates within a multi-lobed, substantially trochoidal shaped cavity formed within the housing of the engine and which engine is disposed in its normal operative position with the major and minor axes of the cavity respectively extending substantially vertically and parallel to a horizontal plane and wherein combustion occurs in the area adjacent one of the lobe junctures so that the area of highest heat flux extends substantially along one side of the housing parallel to the major axis of said cavity, a cooling system for the housing of said engine comprising: a. a plurality of first cooling passageways in the housing adjacent the area where the highest heat flux is produced and extending substantially parallel to the longitudinal axis of said mainshaft; b. header means forming chambers in the housing at the opposite ends of said housing to connect said first cooling passageways together end-to-end to provide for series flow of coolant through each of said plurality of first cooling passageways from one end of the housing to the other and upwardly adjacent said area of highest heat flux; c. inlet means in the housing at a point below the minor axis of the trochoidal cavity and adjacent the combustion exhaust gas discharge means to communicate said first cooling passageways to a source of coolant to supply the first cooling passageways with coolant; d. outlet means in the housing at a point above the minor axis to communicate with said first cooling passageways and receive heated coolant from the latter; e. second cooling passageways in the housing adjacent the area where the lowest heat flux is produced and extending substantially parallel to the longitudinal axis of the mainshaft and communicating with said outlet means; and f. by-pass means downstream from said inlet means for passing a portion of the coolant passing through said first cooling passageways into said second cooling passageways.
Claim 3
Dependent Claim 26 words
The cooling system of claim 1 wherein said header means are opposite end walls, the end walls being constructed and arranged to define said header chambers.
Claim 4
Dependent Claim 17 words
The apparatus of claim 2 wherein said by-pass means is located in one of said end walls.
Claim 5
Dependent Claim 34 words
The apparatus of claim 2 wherein said by-pass means is a passageway having a flow area sized to pass only a small portion of the total quantity of coolant passing through said inlet means.

References Cited (Backward Citations)

US3007460A Cited
US3102516A Cited
US3286700A Cited
US3319611A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1978-07-21 1979-01-20 1979-07-22 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1982-07-21 1983-01-20 1983-07-22 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1986-07-21 1987-01-20 1987-07-22 $7700.00 Window Closed / Lapsed

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