Seal for a gas turbine engine
一种燃气涡轮、发动机的技术,应用在发动机的密封、发动机元件、燃气轮机装置等方向,能够解决弹性密封件破裂和破碎等问题
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[0022] Referring to the drawings, wherein like reference numerals refer to like elements throughout the various views, figure 1 An exemplary gas turbine engine 10 is shown. Although the example shown is a high bypass turbofan engine, the principles of the present invention are also applicable to other types of engines, such as low bypass turbofans, turbojets, turboprops, etc., and with any number of compressor turbines Spool of turbo engine. Engine 10 has a longitudinal centerline or axis 11 .
[0023] Note that as used herein, the terms "axial" and "longitudinal" both refer to a direction parallel to the centerline axis 11, while "radial" refers to a direction perpendicular to the axial direction, and "tangential" or "circumferential" Refers to directions that are mutually perpendicular to the axial and radial directions. As used herein, the term "forward" or "forward" refers to a relatively upstream location in the airflow through or around the component, and the term "re...
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