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Developing a surface stress film for use on a low-pressure turbine blade

机译:显影用于低压涡轮叶片的表面应力膜

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1. S3F successfully produced 2D shear fields for 7 and 13.5 m/s 1.1 Significant differences in stress levels between leading and trailing edges 1.1.1t 1 order of magnitude in streamwise mean shear 1.1.2t 2 orders of magnitude in streamwise shear gradien 2. Optimized LPT geometry issues 2.1 Use of separate 5-6mm streamwise strips w/ 1-2mm gaps instead of single strip 2.2 Film heights = 1.5mm better for low speed dynamic range 3. 1.5mm-25Pa S3F developed 3.1t Produced deformation fields at flow velocities from 0.7 - 4.4 m/s 3.2t Further reduction of noise will produce shearand pressure fields.
机译:1. S3F成功产生了7和13.5 m / s的2D剪切场1.1前后缘1.1.1t 1应力水平的显着差异在流向平均剪切1.1.2t 2数量级在流向剪切梯度2中。优化的LPT几何问题2.1使用带有1-2mm间隙的5-6mm分离式流向带材代替单个带材2.2对于低速动态范围,膜高= 1.5mm3。1.5mm-25Pa S3F开发3.1t在流动时产生形变场速度从0.7-4.4 m / s 3.2t进一步降低噪音将产生剪切力和压力场。

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