Method and apparatus for improved polishing of turbine blades

Claim 3

A method for polishing the surface of a turbine blade using an apparatus as claimed in claim 1 comprising the following steps: (1) selecting an arbitrary center of rotation of the turbine blade for mounting the turbine blade on said spindle, (2) defining each of a plurality of profiles of the turbine blade in a respective number of planes perpendicular to said spindle axis, each profile being defined as a series of circle segments each circle segment having a center and an angular length, (3) measuring each respective distance from the center of rotation to each circle segment center, (4) plotting on a data receiving medium the hypothetical paths of the center of rotation of the turbine blade in each of said planes perpendicular to the spindle axis, each said hypothetical path being the path the center of rotation would follow if the center of rotation were rotated in series about each of said circle segment centers through each of said respective angular lengths, each of said hypothetical paths being a series of circle segments defined by a series of end points, each end point corresponding to each of said circle segments, (5) synchronizing (a) movement of the shoe axis in the vertical direction and (b) movement of the blade in a horizontal direction perpendicular to the spindle axis of rotation and (c) rotation of the blade on the spindle axis such that as the blade rotates through an angular length defined in step 2, the horizontal position of the blade and vertical position of the shoe are moved in a circular path, said path having a radius equal to the corresponding distance measured in step 3, in the respective plane perpendicular to the spindle axis from the respectine end point corresponding to the respective angular length to the next respective end point in the series of end points defined in step 4, (6) repeating step 5 for each circle segment in series, (7) incrementing the position of the blade in a horizontal direction parallel to the spindle axis, and (8) repeating steps 5 through 7 for each profile of the turbine blade until the blade is completely polished.

Claim 4

An apparatus as claimed in claim 1 further comprising means for rotating said shoe axis of rotation about a vertical axis and means for rotating said shoe axis of rotation about a horizontal axis.

Claim 5

An apparatus as claimed in claim 1 further comprising means for rotating said shoe axis of rotation about vertical axis and means for rotating said shoe axis of rotation about a horizontal axis, and means for synchronizing the rotation of the shoe axis about said vertical and horizontal axes with said rotation of said spindle and said movement of said platform.

Claim 6

A method for polishing the surface of a turbine blade using an apparatus as claimed in claim 4 comprising the following steps: (1) selecting an arbitrary center of rotation of the turbine blade for mounting the turbine blade on said spindle, (2) defining each of a plurality of adjacent profiles of the turbine blade in a respective number of planes perpendicular to said spindle axis, each profile being defined as a series of circle segments each circle segment having a center and an angular length, (3) measuring each respective distance from the center of rotation to each circle segment center, (4) plotting on a data receiving medium the hypothetical paths of the center of rotation of the turbine blade in each of said planes perpendicular to the spindle axis, each said hypothetical path being the path the center of rotation would follow if the center of rotation were rotated in series about each of said first circle segment centers through each of said respective angular lengths, each of said hypothetical paths being a series of circle segments defined by a series of end points, each end point corresponding to each of said circle segments, (5) measuring the angles of rise or fall between corresponding circle segments of each of said adjacent profiles, (6) synchronizing (a) movement of the shoe axis in the vertical direction and (b) movement of the blade in a horizontal direction perpendicular to the spindle axis of rotation and (c) rotation of the blade on the spindle axis such that as the blade rotates through each respective angular length, the horizontal position of the blade and vertical position of the shoe are moved in a circular path, said path having a radius equal to each respective distance, in the respective plane perpendicular to the spindle axis from the respective end point corresponding to the respective angular length to the next respective end point in the series of end points, (7) synchronizing rotation of the shoe axis about the horizontal and vertical axes with said movement of the blade in a horizontal direction perpendicular to the spindle axis of rotation and said rotation of the blade on the spindle axis such that the shoe axis assumes an angle equal to said angle of rise or fall between adjacent profiles, (8) repeating steps 6 and 7 for each second circle segment, (9) incrementing the position of the blade in a horizontal direction parallel to the spindle axis, and (10) repeating steps 5 through 9 for each profile of the turbine blade until the blade is completely polished.