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GAS-TURBINE ENGINE GUIDE SECTOR SECTOR, COMPRESSION STEP, COMPRESSOR AND GAS-TURBINE ENGINE

机译:燃气涡轮发动机指南行业,压缩步骤,压缩机和燃气涡轮发动机

摘要

The sector has blades (2), where each of the blades is connected to an inner shroud and to an outer shroud (4) by the blade`s connection part. Each blade has an inner radial part with a zone connected to an outer radial part by a transition zone, and an intermediate part radially arranged inside the outer shroud. Each blade has a trailing edge with a curvature radius gradually increasing in the transition zone. The radius is maximum at a connection between the transition zone and the intermediate part, and remains constant in the intermediate part and the connection part. An independent claim is also included for a compression stage comprising a rotor wheel.
机译:该扇形具有叶片(2),其中每个叶片通过叶片的连接部分连接到内罩和外罩(4)。每个叶片具有内部径向部分,该内部径向部分具有通过过渡区域连接到外部径向部分的区域,以及在径向上布置在外罩内部的中间部分。每个叶片都有一个后缘,其曲率半径在过渡区逐渐增加。该半径在过渡区域和中间部分之间的连接处最大,并且在中间部分和连接部分中保持恒定。对于包括转子轮的压缩级也包括独立权利要求。

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