초록 ▼

A buffer zone adjacent to the inner diameter of carbon seals of an enclosed bearing compartment is defined by an elongated element disposed adjacent the shaft of a turbine type power plant is open ended to receive pressurized, cool air bled from the compressor to apply the cooler, higher pressure ai

A buffer zone adjacent to the inner diameter of carbon seals of an enclosed bearing compartment is defined by an elongated element disposed adjacent the shaft of a turbine type power plant is open ended to receive pressurized, cool air bled from the compressor to apply the cooler, higher pressure air (higher than ambient) adjacent to the seal. One embodiment contemplates feeding the buffer zone by pipes and another embodiment shrouds the bearing compartment and flows the shrouded air to the buffer zone. The buffer air with other secondary airflow cooling requirements, is utilized to cool the high pressure turbine with an overall engine performance benefit.

대표청구항 ▼

For a gas turbine engine having a compressor, and a turbine and shaft interconnecting said compressor and said turbine, a bearing compartment housing a bearing supporting said shaft interconnecting the turbine and compressor located in an environment of hot engine air, said bearing compartment surro

For a gas turbine engine having a compressor, and a turbine and shaft interconnecting said compressor and said turbine, a bearing compartment housing a bearing supporting said shaft interconnecting the turbine and compressor located in an environment of hot engine air, said bearing compartment surrounding said shaft and having carbon contact sealing means surrounding said shaft mounted at the ends thereof in close proximity to said shaft, wall means defining open ended chambers defining buffer zones surrounding said shaft adjacent said carbon contact sealing means for receiving buffer air, a source of air extracted from said compressor, fluid connecting means for leading buffer air from said source to a point external of said engine into each of said buffer zones at a point in direct communication with the open end of a chamber so that a portion of said buffer air flows out of each of said open ends of said chambers and into said turbine for cooling purposes, said buffer air being at a pressure higher than the pressure of said hot air in said environment so that a small portion of the buffer air leaks through said carbon seal, and the remaining portion is directed toward said turbine heat exchanger means intermediate said source and said buffer zones for coolign the buffer air prior to being admitted into said buffer azones and the buffer air normally flowing out of said open end flows into said bearing compartment in the event of a failure of said carbon contact sealing means.