| 摘要 |
In a tool (1) to measure geometrical parameters of a blade (17) or a vane (15) in a turbomachine and, more specifically, to measure a distance between a tip (3) of the blade (17) or the vane (15) and a reference plane; the tool is designed in a method such that the tool (1) comprises: a first guiding plate (4) and a second guiding plate (5); the first guiding plate (4) and the second guiding plate (5) separated from each other on a positioned formed by at least two spacers (6); the first guiding plate (4) and the second guiding plate (5) respectively equipped with a first through-hole (7), and at least one second through-holes (8, 8′, 8′′, 8′′′, 8′′′′); the first through-hole (7) designed to be inserted through a blade part (2) of the blade (17) or the vane (15); and the second through-holes holes (8, 8′, 8′′, 8′′′, 8′′′′) respectively designed to accommodate a length measuring tool (9), for example, a depth gauge. |
