主权项 |
1. A method of assembling a turbine engine stator comprising a plurality of vanes, each of the plurality of vanes having a camber angle, the method comprising the steps of:
(a) selecting a group of vanes based on the camber angle of each of the plurality of vanes; (b) selecting a nominally cambered vane; (c) positioning at least one over-cambered vane on a first side of the nominally cambered vane and at least one under-cambered vane on an opposite, second side of the nominally cambered vane, each of the nominally cambered vane and an endmost of each of the under-cambered and over-cambered vanes in a group of vanes having a respective inspection feature, each inspection feature having a length; (d) repeating steps (a) to (c) to form a plurality of groups of vanes; and (e) positioning the groups of vanes in a pre-determined order such that each group of vanes is positioned at a predefined circumferential position in the assembled stator stage; (f) measuring the length and circumferential position of each of the inspection features; (g) identifying the nominally cambered vane, and the under-cambered and over-cambered vanes at respective opposite ends of the sequence of vanes in each group on the basis of the length of the respective inspection feature; (h) confirming that the circumferential position of each of the nominally cambered vanes and the over-cambered and under-cambered end vanes in each group matches the corresponding predefined circumferential position; and (i) confirming that the sequence of vanes in each group matches the respective pre-determined sequence on the basis of the quantities of over-cambered and under-cambered vanes which are present on respective opposite sides of the nominally cambered vane. |