首页> 外国专利> LAST STAGE ROTOR BLADES FOR HALF-SPEED NUCLEAR STEAM TURBINE, CORRESPONDING CIRCUMFERENTIAL ROW OF SUCH BLADES, THEIR USE, AND PROCESS OF MANUFACTURING

LAST STAGE ROTOR BLADES FOR HALF-SPEED NUCLEAR STEAM TURBINE, CORRESPONDING CIRCUMFERENTIAL ROW OF SUCH BLADES, THEIR USE, AND PROCESS OF MANUFACTURING

机译:半速核汽轮机的最后一级转子叶片,相应叶片的周向行,其用途和制造过程

摘要

A last stage blade (10) for a half speed nuclear steam turbine operating at 50Hz or 60Hz is provided. The blade (10) includes a single piece steel blade body (12) comprising an airfoil (13) having a height (h) extending between a tip (16) and a base (14) between 1850 mm to 2000 mm, and a base diameter (D) between 2900 mm to 3050 mm. Further, the airfoil (13) having an airfoil mass (M) for the defined airfoil height (H), wherein the airfoil mass (M) to height (H) ratio is in a range of 70 kg/m to 80 kg/m, enabling substantially smaller centrifugal pull on a rotor. The blade (10) further includes a blade root (18), extending from the base, configured to be attachable mounted in a rotor groove of the rotor. Such configuration is capable of withstanding 1.5 times a rotational speed of the turbine for half speed turbine. Corresponding circumferential row of last stage blades, use of such a circumferential row of last stage blades in a half speed nuclear steam turbine, and method of manufacturing a last stage blade are also provided.
机译:提供了用于以50Hz或60Hz运行的半速核汽轮机的末级叶片(10)。叶片(10)包括单件式钢叶片主体(12),其包括翼型(13),该翼型的高度(h)在尖端(16)和基部(14)之间在1850mm至2000mm之间延伸,并且基部直径(D)在2900毫米至3050毫米之间。此外,具有限定的翼型高度(H)的翼型质量(M)的翼型(13),其中翼型质量(M)与高度(H)之比在70kg / m至80kg / m的范围内,可大大减小转子的离心拉力。叶片(10)还包括从根部延伸的叶片根部(18),该叶片根部被构造为可附接地安装在转子的转子槽中。对于半速涡轮机,这种构造能够承受涡轮机转速的1.5倍。还提供了相应的末级叶片的周向排,这种末级叶片的周向排在半速核汽轮机中的使用以及制造末级叶片的方法。

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