Invention Grant
- Patent Title: Heated engine nose cone using spiral channels
- Patent Title (中): 加热发动机鼻锥使用螺旋通道
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Application No.: US11837787Application Date: 2007-08-13
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Publication No.: US08210825B2Publication Date: 2012-07-03
- Inventor: Joseph M. Jensen , James D. Bolla , Joseph T. Humphrey , Steve H. Nguyen
- Applicant: Joseph M. Jensen , James D. Bolla , Joseph T. Humphrey , Steve H. Nguyen
- Applicant Address: US NJ Morristown
- Assignee: Honeywell International Inc.
- Current Assignee: Honeywell International Inc.
- Current Assignee Address: US NJ Morristown
- Agent Robert Desmond, Esq.
- Main IPC: F02C7/047
- IPC: F02C7/047

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.
Public/Granted literature
- US20080279688A1 HEATED ENGINE NOSE CONE USING SPIRAL CHANNELS Public/Granted day:2008-11-13
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