发明名称 Aircraft gearbox gaseous cooling system
摘要 The cooling system of the present disclosure is configured to promote heat transfer in a gearbox. The system can include a container for housing a gas, the gas having a sufficient percentage of helium so that once the gas is introduced into the gearbox, the helium increases heat transfer from the heat generating components of the gearbox. The method of the present disclosure can include selectively introducing the helium gas into the gearbox.
申请公布号 US8951157(B2) 申请公布日期 2015.02.10
申请号 US201213687143 申请日期 2012.11.28
申请人 Bell Helicopter Textron Inc. 发明人 McGlaun Monte A.;Riley Walter W.
分类号 F16H57/04 主分类号 F16H57/04
代理机构 代理人 Tevis Noah A.
主权项 1. The cooling system for a gearbox, the system comprising: a container configured to house a gas; a gas line configured to provide a flow of the gas to an interior of the gearbox; and a valve configured to selectively supply the gas to the interior of the gearbox in the event of a failure to a gearbox lubrication system; wherein the gas comprises at least one percent of a helium gas.
地址 Fort Worth TX US