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US07798765B2 Out-flow margin protection for a gas turbine engine 有权
燃气涡轮发动机的流量裕度保护

Out-flow margin protection for a gas turbine engine
Abstract:
A cooled turbine exhaust case assembly includes a plenum defined at least in part by a forward outer diameter flowpath ring and a turbine case, a probe positioned at a probe opening formed in the forward outer diameter flowpath ring, and an inlet opening in the turbine case for introducing cooling air to the plenum.
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