发明名称 |
Icing prevention of a gas turbine engine pressure sensing assembly |
摘要 |
A combination of a gas turbine pressure sensing assembly and an engine electronics unit. The pressure sensing assembly includes a pressure manifold having an air inlet and one or more air outlets. The pressure sensing assembly further includes one or more pressure sensors connected to the air outlets to sense the pressure of air entering through the air inlet. The engine electronics unit in operation produces waste heat. The pressure sensing assembly further includes a heat conduction path which thermally connects the engine electronics unit to the manifold such that the manifold acts as a sink for the waste heat. The temperature rise of the manifold produced by the waste heat preventing icing of the manifold. |
申请公布号 |
GB201520389(D0) |
申请公布日期 |
2016.01.06 |
申请号 |
GB20150020389 |
申请日期 |
2015.11.19 |
申请人 |
ROLLS-ROYCE CONTROLS AND DATA SERVICES LIMITED |
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