Abstract:
A method of using a machining assembly to machine a plurality of different turbine components that include a dovetail having a contoured profile. The method includes removably coupling a first set of retainers into the machining assembly, the first set of retainers include an upper portion having a profile that substantially mirrors a portion of the first dovetail, and a lower portion having a profile that substantially mirrors an opposite side of the first dovetail, coupling a first turbine component between the upper and lower portions such that the first turbine component is secured by the first set of retainers, coupling the machining assembly into a milling machine, and machining at least one seal groove into the dovetail of the first turbine component.
Abstract:
A blade processing fixture has first and second jaws. The second jaw is movable relative to the first jaw from a disengaged position for accepting a root of the blade. The blade is accepted in a receiving area between the first and second jaws. The second jaw is movable to an engaged position clamping the blade between the first and second jaws. A gas flow path extends from an inlet port to an outlet port. The outlet port is positioned to introduce gas to a blade inlet port when the blade is installed.
Abstract:
A marking system includes a fixture having a base and means for receiving a pair of jaws in an installed condition. The fixture includes means for articulating the installed jaws relative to the base with at least first and second rotational degrees of freedom. A pair of the jaws includes a first jaw having a surface portion generally concave and complementary to a suction side portion of an airfoil of a first turbine engine element. A second jaw has a surface portion generally convex and complementary to a pressure side portion of the airfoil.
Abstract:
An apparatus for machining a turbine blade assembly including an airfoil and a dovetail, wherein the apparatus includes a fixture, at least one airfoil locator, at least one airfoil clamp, and at least one dovetail clamp assembly. The airfoil locator and the airfoil clamp are fixedly coupled to the fixture. The airfoil locator and the airfoil clamp are configured to secure the airfoil therebetween. The dovetail clamp assembly includes a clamp arm that is moveable with respect to the dovetail.
Abstract:
A method for securing a component for manufacture. The method includes fixedly coupling a first clamping member and a biasing mechanism to a tool that includes a fixture. The fixture includes a first clamping member, a second clamping member, and a biasing mechanism. The method further includes coupling the second clamping member to the fixture, using the biasing mechanism to align the component within the tool between the first and second clamping members such that the component is maintained in position relative to the fixture, securing the component between the first and second clamping members such that the first clamping member, the second clamping member, and the component are fixedly secured in position with respect to the fixture, and retaining the component in position with respect to the fixture using the first and second clamping members.
Abstract:
A gas turbine component such as a turbine blade is clamped into a fixture having a base upon which a remainder of the fixture is supported, a stop which limits the movement of the gas turbine component, and two clamp arms affixed to the base and controllably clamping against the lower side of the platform of the gas turbine component to force the gas turbine component against the stop. When the gas turbine component is clamped in this position, its root may be readily shaped as by grinding.
Abstract:
A gas turbine component blank is shaped by clamping the gas turbine component blank into a fixture that accurately positions the gas turbine component blank in three dimensions. The positioning is accomplished against stops accurately machined into a base of the fixture, by first supporting the gas turbine component blank on one set of stops that prevents movement in the direction perpendicular to a plane of the base, and then operating a movable clamp to force the gas turbine component blank against other sets of stops that limit the movement of the gas turbine component blank in directions lying in the base plane. The clamp has a compound movement that simultaneously forces the gas turbine component blank against stops that prevent movement in orthogonal directions lying in the base plane. The gas turbine component blank is thereafter shaped, preferably by grinding the sides of the root precursor of the gas turbine component blank.
Abstract:
An apparatus for machining a turbine blade assembly includes at least one locator for positioning the blade assembly with respect to the apparatus. The apparatus also includes at least one biasing mechanism for maintaining a relative position of the blade assembly with respect to said apparatus and at least one clamping device that includes a predetermined locking position. The clamping device retains the blade assembly.
Abstract:
A method for forming a precisely shaped part includes providing a blank having at least two spaced apart locators, providing a fixture having a U-shaped base with two spaced apart end walls, one supporting a clamping mechanism and the other supporting an abutment, securing the blank into the fixture such that the clamping mechanism mates with one of the locators and forces another of the locators into contact with the abutment, and subsequently machining the blank. The locators on the blank are shaped to mate with corresponding features on the fixture, such that the fixture uses the locators to secure the blank. The locators are disposed in a plane from which critical design features are referenced. Once the blank is clamped into the fixture details can be accurately machined into the blank forming a precisely shaped part.
Abstract:
A fixture for workpieces which cannot be directly engaged by the work holder of a machine tool has a pallet for several work holding elements each of which has a head releasably engaging a workpiece and a section which is embedded in hardened casting material of the pallet so that the casting material does not contact the workpieces. The pallet can be a one-piece casting or is assembled of several reusable modules, and it has several mounting surfaces which facilitate predictable mounting in the work holder of a machine tool.