Abstract:
Laser scanning apparatus and a related method for scanning a workpiece in a raster scan pattern, to remove a series of thin, overlapping layers in the workpiece and thereby provide a stepwise approximation to a contoured, three-dimensional shape. In one embodiment, the beam follows a raster scan pattern with scans that are parallel to the removed layer's boundary. The wall bounding the layer is made to be substantially perpendicular to the plane of the removed layer, regardless of the wall's orientation, by tilting the beam about an axis normal to a specified reference plane and by elliptically polarizing the beam to a selected degree. A substantially constant proportion of the beam's average intensity is thereby absorbed at each point along the boundary wall, regardless of the wall's orientation relative to the reference plane. In another embodiment, the beam scans repeatedly along an axis parallel to a specified reference plane. Like the first embodiment, the boundary wall is made to be substantially perpendicular to the plane of the removed layer, regardless of its orientation, by tilting the beam about an axis normal to the reference plane and by elliptically polarizing the beam to a selected degree.
Abstract:
A process for preventing crack formation in nickel alloy substrates having a gamma-prime phase includes providing a substrate comprised of a nickel alloy having a gamma-prime phase. A portion of the substrate is irradiated with a laser beam and thereby forms a molten pool of the alloy. A supply of coating particles are dispersed within the pool, the particles are comprised of a nickel alloy having gamma-prime forming constitutents. Rapid relative motion between the beam and the pool is effected so that the pool rapidly solidifies and thereby minimizes the formation of gamma-prime therein and adjacent thereto.
Abstract:
A method for manufacturing bladed disks, or blisks, for turbines by press welding of blades or outer airfoil elements to blade stives or inner airfoil elements on a disk is characterized by the provision on the outer and inner airfoil elements of flanges of excess flash material having alignment holes for dowel pins that assure alignment of leading and trailing edges of the airfoil elements during pressure welding, followed by removal of the excess flash material and the included dowel pins.
Abstract:
This is a method for repairing low alloy steel steam turbine (both high pressure and low pressure sections) or generator rotors. The defective section of the original rotor is removed and a replacement end is used, with mating attachments machined on the replacement end and the original rotor. The inner portion of the weld joining the replacement end to the original rotor is provided by a narrow gap weld, either by gas metal or by submerged arc welding. The outer 1/2-2 inches of the weld is provided by gas tungsten arc welding. The mating attachment and at least the inside 1/4 inch of the weld is bored out to remove possible crack initiation sites and to provide a smooth inspectable bore. In this manner, a fast and reliable technique is provided which provides accurate alignment, fast, essentially distortion free welding, and the superior mechanical properties of gas tungsten arc welding in the outer, more highly stressed zones.
Abstract:
A method of repair of an article incorporating the application of considerable thermal energy, e.g. a welding operation, requires heating of the article both in the repair area and surrounds wherein the heating of the repair area and surrounds is carried out by flexible heating mats and wherein fixing means are used to securely fix the heating mats to the article, which fixing means may readily release at least a part of the heating mats whereby that part may be folded back or otherwise removed from the repair area to allow the repair step to be carried out. After repair, that part of the heating mats removed from the repair area may be replaced.
Abstract:
The slots for accommodating feather seals in the turbine vanes of a gas turbine engine has the end thereof sealed off by use of weld wire inserted into the slot and simultaneously welded and cut to the required length.
Abstract:
To prevent corrosion in subsequent high temperature exposure, backers for electron beam hole drilling of nickel base superalloys contain glass particulates of the borosilicate and aluminosilicate types, having an alkali metal oxide content of less than 1 weight percent and a heavy metal (Pb, Bi, Sn, Sb, As) content of less than 25 ppm. Preferably the binder is a soluble inorganic material, such as magnesium dichromate or a polymer, also free of alkali metal content.
Abstract:
A method of refurbishing vane or blade components. Used turbine vanes or blades are cleaned, annealed and in some cases slotted adjacent their ends, after which any cooling passages (in the case of vanes) are welded closed and all cracks welded over, on both leading and trailing edges. The trailing edge, for a vane or blade component having a short chord, is built up by welding along its full length with an alloy wire, after which any slots that were cut adjacent the ends are closed, also by welding. Then the worn surfaces of the vane or blade are built-up by a plasma spray process, using a metal powder with added silica, to a thickness which can be as great as 30 to 40 thousandths of an inch. The built-up vane or blade is then sintered and thereafter surface finished to conform to the original contour of the component when new. Any cooling holes are finally recut, and the vane or blade polished as required and inspected.
Abstract:
A method for producing a rotor made from discs joined together in succession in side-by-side relation by welding comprises the steps of assembling each rotor disc and the succeeding disc next to be joined such that their axes are in horizontal alignment, pressing the two discs together thereby to place their interfaces under axial pressure, pre-heating each two discs to be joined to the proper working temperature, joining the discs by welding in a circumferentially extending welding seam while maintaining the pressure, repeating the assembling, pre-heating and welding operations until all of the discs have been welded together to establish the complete rotor, thereafter heat-treating the completed rotor, and finally subjecting the completed rotor to a hot true-running test. All of these operations take place within a common heating box into which hot air is introduced to effect the heating. The apparatus for performing the method features a trolley located within the heating box and on which each next-to-be-welded-on disc is carried into face-to-face pressure contact with a previously welded-on disc. The end discs of the rotor are provided with shaft extensions and the latter serve to support the rotor on rests in order to carry out the running and truing operations. The heating box is constituted by a number of axial modules joined together in succession as the discs are welded together in succession to provide a correspondingly increasing axial length.
Abstract:
A method of bonding a laminated porous sheath to a cast strut includes the step of performing a compressible pad to have a plurality of closely spaced grooves on one surface thereon and a plurality of spaced apart lands on the opposite face thereof; locating a preformed porous laminate sheath over the outer surface of a cast strut and laser welding it thereto and thereafter assembling the preformed compressible pad to locate the plurality of grooves thereon in overlying relationship to a plurality of airflow openings in the porous laminated sheath and with ribs on either side of the grooves being located in juxtaposed relationship with the outer surface of the porous laminated sheath for uniformly distributing a load thereto; locating the preassembled casting, sheath and compressible pad within a contoured opening formed by a three piece pressure block fixture and applying a predetermined pressure to the assembled parts while subjecting them to a predetermined bond temperature while applying a vacuum.