Invention Application
US20170002675A1 SEAL FOR A GAS TURBINE ENGINE 审中-公开
密封用于燃气涡轮发动机

SEAL FOR A GAS TURBINE ENGINE
Abstract:
A gas turbine engine assembly includes a shield that has a first portion and a second portion. The first portion extends radially from an axial end portion of the shield and includes a blade outer air seal contact surface. The second portion extends axially from a radially outer end of the first portion and includes a vane contact surface.
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