General Electric Company

James G Kelley

Todd Jay Rockstroh

Eugene Andrew Smith

Seetharamaiah Mannava

Seetha Ramaiah Mannava

Mark Wayne Wheeler

Ralph M Somers

John M Crow

Rabi N Ratnesar

Todd B Lozier

John N Minnich

Lawrence R Waldo

A method for linking together three or more powered systems to operate as a single distributed power system, the method includes identifying a first linking protocol between at least a first powered system and a second powered system, determining whether at least a third powered system is compatible with the first linking protocol, if not compatible, switching to at least a second linking protocol to find a common linking protocol between the first powered system, the second powered system, and at least the third powered system, and linking the first powered system, the second powered system, and at least the third power system to operate in a distributed power configuration when the common linking protocol is found. A system and a computer software code linking together two or more powered systems to operate as a single distributed power system are also disclosed.

System, method, and computer software code for linking a plurality of powered systems having different linking protocols to operate as a single powered system

A method of laser shock peening a gas turbine engine object continuously firing a stationary laser beam, which repeatably pulses between relatively constant periods, on a portion of the object with a low power laser beam, on the order of 3-10 joules, to vaporize material on the surface of a portion of a part made of a strong hard metal, such as a titanium alloy. Laser pulses around small laser beam spots, on the order of 1 mm in diameter, are used to vaporize material on the surface of the portion of the object with the pulses around laser beam spots formed by the laser beam on the surface and form a region having deep compressive residual stresses extending into the object from the laser shock peened surface. Flowing a curtain of water over the surface upon which the laser beam is firing while preferably moving the object until the laser shock peened surface is completely covered by laser beam spots at least once. The surface may be coated with an ablative coating such as a paint which is suitable to produce the plasma or the surface may be unpainted and the metal of the object is used to produce the plasma.

Laser shock peening using low energy laser

A gas turbine engine component includes a wall portion with at least one compound cooling hole formed therein between an external surface of the component and an interior plenum. The at least one compound cooling hole includes a non-circular diffuser opening formed by a laser beam with a non-circular cross-sectional area, and a channel with a substantially circular cross-section connecting the diffuser opening and the interior plenum. The channel is also formed by the non-circular laser beam in the same laser drilling operation as the diffuser opening. The cooling hole further includes a transition point at which the compound hole begins to convert from a substantially non-circular cross-section to a substantially circular cross-section. The location of the transition point is controlled by positioning a focal point of the non-circular laser beam to undershoot the external surface of the component by a predetermined distance.

Gas turbine engine component with compound cooling holes and method for

A method for forming an aperture in a component wall made of metal, the aperture having a diffuser which opens up and outward from a bottom of the diffuser to a first surface of the wall, the method includes the following steps: A) laser machining the wall with a laser which produces a laser beam having a pulse rate and power sufficient to vaporize the metal; B) firing and traversing the laser beam, preferably at an acute angle, across the surface to a predetermined first edge of the diffuser in a single pass starting at a centerline of the diffuser; and C) traversing the laser beam at an increasing rate of speed during the pass so that each beam pulse vaporizes the metal at a laser spot such that successive laser spots substantially overlap each other in decreasing amounts and the pulses nibble out the metal to form a continuous trench below the surface.

Laser drilling of non-circular apertures

An improved method and apparatus for laser trepanning a passage through a workpiece, gas turbine engine component or the like includes the method steps of: providing a linearly polarized beam of laser energy; focusing the laser beam on a selected location on the component; moving one of the laser beam or the workpiece relative to one another along a first selected trepanning path and along a second selected trepanning path, which is substantially opposite in direction to the first selected path, to compensate for the linear polarization of the laser beam and to reduce the processing time. The steps of moving one of the laser beam or the workpiece along the first and second trepanning paths are repeated until a passage is cut to a desired depth into the surface of the component or the passage is cut entirely through the component. An apparatus for accomplishing the method of the present invention includes a laser system for generating a linearly polarized beam of laser energy and a manipulator arrangement for moving one of the laser system or the component relative to one another. The apparatus further includes a computer controller which is programmed to move either the laser system or the component along the first and second selected trepanning paths.

Method and apparatus for laser trepanning

A laser apparatus is disclosed which is capable of protecting the laser slab or rod crystal within the laser from damage due to overheating when the laser malfunctions in a manner such that laser output ceases while optical pumping of the laser crystal continues. The laser apparatus includes a laser crystal situated within a laser cavity. The apparatus also includes an excitation lamp for pumping the crystal to generate a laser beam to project along a desired main path. A first sensor senses the cessation of the projection of the laser beam along the desired main path and a second sensor senses the continuing excitation of the excitation lamp. The apparatus further includes a extinguishing circuit for extinguishing the excitation lamp a predetermined amount of time after the cessation of the laser beam such that damage to the laser apparatus due to overheating is avoided.

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California, KY, United States of America

James G Kelley