Manufacture of cooling holes for ceramic matrix composite components
AssigneeGeneral Electric Company
InventorsAlan Joseph Parvis, Timothy Francis Andrews, Mark Samuel Bailey
Life of this patent
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AssigneeGeneral Electric Company
InventorsAlan Joseph Parvis, Timothy Francis Andrews, Mark Samuel Bailey
Estimating the term…
Systems and methods for machining openings of a component are provided. In one exemplary aspect, a laser system includes features for machining an opening into a component, such as a cooling hole for a CMC component of a gas turbine engine. The component can be oriented in a first position and lasered while oriented in the first position to form a portion of the opening. The component is then oriented to a second position and lasered while oriented in the second position to form another portion of the opening. The component is alternated between the first and second positions until the predetermined geometry of the opening is formed. The component is oriented in the first and second positions such that the laser beam can machine the component without clipping areas that are not desired to be machined.
A method for laser machining one or more walls of an opening of a component using a conically-shaped laser beam, the one or more walls defining a first wall portion and a second wall portion, the method comprising:
A laser system for machining an opening into a component, the laser system defining a vertical direction, a lateral direction, and a transverse direction each perpendicular to one another, the component defining a first section and a second section, the laser system comprising:
A method for laser machining an opening into a component using a conically-shaped laser beam, the opening defining a first section and a second section opposite the first section, the method comprising:
Dependencies are inferred from the claim text.