发明名称 Turbine starter lubricant cooling
摘要 A cooling system for turbine starter lubricant includes one or more outflow transfer passages (54) extending from the turbine starter (10) to a secondary component (40). At least one heat exchange passage (56) affixed at a first end to an end of an outflow transfer passage (54) of the one or more outflow transfer passages (54), is located in the secondary component (40) having a lower interior temperature than the turbine starter (10). One or more return transfer passages (60) are affixed to a second end of the at least one heat exchange passage (56) and extend from the secondary component (40) to the turbine starter (10). Flowing a volume of starter lubricant (42) through the one or more outflow transfer passages (54), the at least one heat exchange passage (56), and the one or more return transfer passages (60) removes thermal energy from the volume of starter lubricant (42) and returns the volume of starter lubricant (42) to the turbine starter (10).
申请公布号 US8910463(B2) 申请公布日期 2014.12.16
申请号 US201012709961 申请日期 2010.02.22
申请人 Hamilton Sundstrand Corporation 发明人 Telakowski Robert
分类号 F02C7/12;B64F1/34;F02C7/14;F02C7/277;F01D25/18;F02C7/06 主分类号 F02C7/12
代理机构 Cantor Colburn LLP 代理人 Cantor Colburn LLP
主权项 1. A cooling system for turbine starter lubricant comprising: one or more outflow transfer passages extending from a compressed gas driven turbine starter to a gearbox assembly; at least one heat exchange passage extending through the gearbox assembly at least partially vertically, affixed at a first end to an end of an outflow transfer passage of the one or more outflow transfer passages, the gearbox assembly having a lower interior temperature than the turbine starter during operation; one or more return transfer passages affixed to a second end of the at least one heat exchange passage and extending from the gearbox assembly to the turbine starter, whereby flowing a volume of starter lubricant through the one or more outflow transfer passages, the at least one heat exchange passage, and the one or more return transfer passages removes thermal energy from the volume of starter lubricant and returns the volume of starter lubricant to the turbine starter, the one or more return transfer passages are disposed inside the turbine starter at a higher elevation than the one or more outflow transfer passages; and an internal pump disposed inside a turbine starter housing to circulate the volume of starter lubricant through the at least one heat exchange passage; wherein thermal energy is removed from the starter lubricant via transfer from the starter lubricant flowing through the at least one heat exchange passage to a gearbox coolant circulating in the gearbox assembly at an exterior of the at least one heat exchange passage.
地址 Windsor Locks CT US