首页> 外国专利> TURBINE MOVING BLADE SERVICE LIFE EVALUATING METHOD, TURBINE MOVING BLADE CREEP ELONGATION STRAIN MEASURING DEVICE AND TURBINE MOVING BLADE

TURBINE MOVING BLADE SERVICE LIFE EVALUATING METHOD, TURBINE MOVING BLADE CREEP ELONGATION STRAIN MEASURING DEVICE AND TURBINE MOVING BLADE

机译:汽轮机叶片使用寿命评估方法,汽轮机叶片蠕变伸长率测量装置及汽轮机叶片

摘要

PPROBLEM TO BE SOLVED: To provide a turbine moving blade service life evaluating method for quantitatively evaluating the service life of a turbine moving blade, a turbine moving blade creep elongation strain measuring device and the turbine moving blade suitable for applying the turbine moving blade service life evaluating method. PSOLUTION: This turbine moving blade service life evaluating method adopts a method for evaluating that the turbine moving blade falls within a service life range when creep elongation strain is less than 0.5% of the initial length, and evaluating that the turbine moving blade exceeds the service life when the strain is 0.5% or more of the initial length. The turbine moving blade creep elongation strain measuring device 20 adopts a constitution having the first fixing end 21 installed on one end side of the turbine moving blade 10, the second fixing end 22 installed on the other end side and a dial gauge 24 for measuring an interval dimension of these ends. The turbine moving blade 10 also adopts a constitution carved with a longitudinal directional dimension in an initial state. PCOPYRIGHT: (C)2004,JPO&NCIPI
机译:

要解决的问题:提供一种用于定量评估涡轮机动叶片的使用寿命的涡轮机动叶片使用寿命的评估方法,一种涡轮机动叶片蠕变伸长率测量装置以及适用于应用涡轮机运动的涡轮机动叶片。叶片使用寿命评估方法。

解决方案:该涡轮机动叶片使用寿命评估方法采用以下方法:当蠕变伸长率应变小于初始长度的0.5%时,评估涡轮机动叶片处于使用寿命范围内,并评估涡轮机动叶片当应变为初始长度的0.5%或更大时,超过使用寿命。涡轮动叶片蠕变伸长率测定装置20采用在涡轮动叶片10的一端侧安装有第一固定端21,在另一端侧安装有第二固定端22,并且对千分表24进行测量的结构。这些末端的间隔尺寸。涡轮动叶片10还采用在初始状态下以纵向方向的尺寸进行雕刻的结构。

版权:(C)2004,日本特许厅和日本国家唱片公司

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