Abstract: A system for determining accessibility of a tool to an object is provided. The system provides for selecting one or more sections on the object to be laser shock peened, selecting a region of interest on the one or more sections and determining a set of feasible solutions to access the selected region of interest on each of the one or more sections via use of an accessibility system.

Abstract: A system for determining accessibility of a tool to an object is provided. The system provides for selecting one or more sections on the object to be laser shock peened, selecting a region of interest on the one or more sections and determining a set of feasible solutions to access the selected region of interest on each of the one or more sections via use of an accessibility system.

Abstract: A method for determining accessibility of a tool to an object is provided. The method provides for selecting one or more sections on the object to be laser shock peened, selecting a region of interest on the one or more sections and determining a set of feasible solutions to access the selected region of interest on each of the one or more sections via use of an accessibility system. Systems and computer programs that afford functionality of the type defined by this method may be provided by the present technique.

Abstract: A method for determining accessibility of a tool to an object is provided. The method provides for selecting one or more sections on the object to be laser shock peened, selecting a region of interest on the one or more sections and determining a set of feasible solutions to access the selected region of interest on each of the one or more sections via use of an accessibility system. Systems and computer programs that afford functionality of the type defined by this method may be provided by the present technique.

Abstract: A method enables a blade assembly to be secured for manufacture. The blade assembly includes an airfoil, a dovetail, and a platform extending therebetween. The method includes providing a fixture including at least one platform support assembly and at least one dovetail clamp assembly coupled to the fixture, wherein the platform support assembly includes a support member, a lever arm, and a biasing mechanism, locating the blade assembly within the fixture using a locator, positioning the platform support assembly against the blade assembly platform, and retaining the blade assembly in alignment with respect to the fixture using the at least one dovetail clamp assembly.

Abstract: An apparatus and method for inspecting a dovetail slot of a gas turbine engine disk, including: a first pin member fixed in a stationary position; a second pin member having the ability to move between a first position and a second position, wherein the second pin member is oriented substantially parallel to the first pin member; a member actuable between a first position and a second position, wherein the member functions to automatically position the first and second pin members in a predetermined position within the dovetail slot when in the second member position; a first probe for measuring a distance between the first and second pin members when in the predetermined dovetail slot position; and, at least one plate member forming a base to which the first pin member, the second pin member, the actuable member, and the first probe are assembled in a predetermined manner.

Abstract: An apparatus and method for inspecting a dovetail slot of a gas turbine engine disk, including: a first pin member fixed in a stationary position; a second pin member having the ability to move between a first position and a second position, wherein the second pin member is oriented substantially parallel to the first pin member; a member actuable between a first position and a second position, wherein the member functions to automatically position the first and second pin members in a predetermined position within the dovetail slot when in the second member position; a first probe for measuring a distance between the first and second pin members when in the predetermined dovetail slot position; and, at least one plate member forming a base to which the first pin member, the second pin member, the actuable member, and the first probe are assembled in a predetermined manner.