发明名称 GAS TURBINE ENGINE OIL TANK
摘要 A gas turbine engine includes an engine static structure housing that includes a compressor section and a turbine section. A combustor section is arranged axially between the compressor section and the turbine section. A core nacelle encloses the engine static structure to provide a core compartment. An oil tank is arranged in the core compartment and is axially aligned with the compressor section. A heat exchanger is secured to the oil tank and arranged in the core compartment.
申请公布号 EP2847448(B1) 申请公布日期 2016.12.21
申请号 EP20130787212 申请日期 2013.04.25
申请人 United Technologies Corporation 发明人 SUCIU, Gabriel L.;SNAPE, Nathan;DYE, Christopher M.
分类号 F02C7/06;B64D33/00;F01D25/12;F01D25/18;F01M11/00;F02C7/14;F02C7/32 主分类号 F02C7/06
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