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AssigneeRaytheon Technologies Corporation
InventorsKerry E. Muenchow, Georgios S. Zafiris, John Harner, Raymond P. Martina, Jr., Imad Hanhan, Darin S. Lussier, Mark W. Costa, Michael R. LaFavor, Scott A. Smith
Estimating the term…
A method for preparing an abradable panel for a rub strip of a fan case of a gas turbine engine includes forming an abradable material into a plurality of panels each comprising an abradable structure; curing the abradable material in the plurality of panels; and installing the plurality of panels into the fan case. The panels can be cured and assembled into a fully assembled rubstrip, and then the assembled rubstrip can be installed into the fan case.
A method for preparing an abradable panel for a rub strip of a fan case of a gas turbine engine, comprising:
A method providing an abradable panel on an inside surface of a fan case, comprising bonding a panel containing an abradable material potted in a support structure to the inside surface of the fan case.
Dependencies are inferred from the claim text.