Invention Grant
US08210825B2 Heated engine nose cone using spiral channels 有权
加热发动机鼻锥使用螺旋通道

Heated engine nose cone using spiral channels
Abstract:
A nose cone of a turbomachine, such as an aircraft engine, is heated to prevent ice formation. The nose cone is configured as a conical shell positioned concentrically over an inner shell with a space therebetween. Spiral spacers in the space provide distributed passages through which heated lubricating oil flows. A system for separating entrained air from the lubricating oil as part of this mechanism is disclosed.
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