Patent References 2584899 3527053 3527054 Cooling apparatus for split shaft gas turbine Multi-stage turbine with interstage spacer-manifold for coolant flow Coolant flow metering device Cooling apparatus for a bearing in a gas turbine Turbine intermediate case Air cooler for providing buffer air to a bearing compartment Air cooler for providing buffer air to a bearing compartment InventorAssigneeApplicationNo. 284476 filed on 08/04/1994US Classes:415/111, For shaft sealing, packing, lubricating or bearing means60/39.83, Cooling of auxiliary components415/116WITH DIVERSELY ORIENTED INLET OR ADDITIONAL INLET FOR DIVERSE FLUID (E.G., HEATING, COOLING OR MIXED WORKING FLUID, ETC.)ExaminersPrimary: Look, Edward K.Assistant: Larson, James A. Attorney, Agent or FirmForeign Patent References
International ClassF01D 025/12Foreign Application Priority Data1992-02-04 DEAbstractThe wall space and the mounting space for turbine bearings in the casing of an aircraft gas turbine are each supplied with cooling air via a separate pipe, a first cooling-air pipe opening into the wall space and a second cooling-air pipe extending through the wall space and opening in the mounting space. To ensure that the respective space continues to be supplied with cooling air even if one of the two pipes breaks, the cooling-air pipe extending through the wall space and opening into the mounting space has air overflow openings in the region of the wall space.Field of SearchFor shaft sealing, packing, lubricating or bearing meansWITH PASSAGE IN BLADE, VANE, SHAFT OR ROTARY DISTRIBUTOR COMMUNICATING WITH WORKING FLUID WITH DIVERSELY ORIENTED INLET OR ADDITIONAL INLET FOR DIVERSE FLUID (E.G., HEATING, COOLING OR MIXED WORKING FLUID, ETC.) SHAFT BEARING COMBINED WITH OR RETAINED BY ARM OR VANE IN SURROUNDING WORKING FLUID SPACE WORKING FLUID BYPASS INCLUDING ADDITIONAL MEANS CAUSING OR CONTROLLING FLUID FLOW FOR HEAT EXCHANGING, LUBRICATING OR SEALING Means subjected to or is working fluid Cooling of auxiliary components | |