LINER COOLANT FLOW PILOT FEATURE

The application relates to a liner coolant flow pilot feature. A coolant liner includes a first flow surface to direct coolant fluid toward the cylinder and a transition region coupled to the first flow surface. The transition region includes a convex portion having a first radius of curvature and a...

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Bibliographische Detailangaben
1. Verfasser:	ZHOU, Xiling
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES BLASTING COMBUSTION ENGINES CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	The application relates to a liner coolant flow pilot feature. A coolant liner includes a first flow surface to direct coolant fluid toward the cylinder and a transition region coupled to the first flow surface. The transition region includes a convex portion having a first radius of curvature and a concave portion having a second radius of curvature. The concave portion is coupled to the convex portion at an inflection point. A second flow surface is coupled to the transition region to direct coolant fluid around the cylinder.