Invention Grant
- Patent Title: Helicopter gearbox auxiliary cooling system
- Patent Title (中): 直升机变速箱辅助冷却系统
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Application No.: US13661269Application Date: 2012-10-26
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Publication No.: US09272777B2Publication Date: 2016-03-01
- Inventor: Monte A. McGlaun , K. Myron Jackson
- Applicant: BELL HELICOPTER TEXTRON INC.
- Applicant Address: US RI Providence
- Assignee: Textron Innovations Inc.
- Current Assignee: Textron Innovations Inc.
- Current Assignee Address: US RI Providence
- Agent James E. Walton
- Main IPC: B60H1/00
- IPC: B60H1/00 ; B64C27/12 ; F28D15/02 ; F16H57/04 ; B64D33/08 ; F28D21/00

Abstract:
A cooling system using one or more heat pipes rotating about a central axis to transfer heat energy from one medium to another. The heat pipes are oriented within a rotating member such that the axis of the heat pipe is non-coaxial with that of a central axis of the rotating member. Centrifugal forces are used to assist the movement of the working fluid within the heat pipe. The cooling system also includes heat pipes associated with a planetary carrier assembly and supplemental heat exchangers for use in aircraft and other machinery.
Public/Granted literature
- US20140116654A1 Helicopter Gearbox Auxiliary Cooling System Public/Granted day:2014-05-01
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