发明申请
US20130213057A1 Gas Turbine Engines and Related Systems Involving Blade Outer Air Seals 有权
燃气轮机发动机和相关系统涉及刀片外部气密封

Gas Turbine Engines and Related Systems Involving Blade Outer Air Seals
摘要:
Gas turbine engines and related systems involving blade outer air seals are provided. In this regard, a representative blade outer air seal segment for a set of rotatable blades includes: a blade arrival end; and a blade departure end; each of the blade arrival end and the blade departure end being angularly offset with respect to a longitudinal axis about which the blades rotate.
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