Fan outlet guide vane shroud insert repair

Rotary kinetic fluid motors or pumps – With sound or vibratory wave absorbing or preventing means...

Reexamination Certificate

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C415S191000, C415S200000, C415S209100, C415S209200, C415S209300, C029S889220

Reexamination Certificate

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07980813

ABSTRACT:
A method of repairing a turbine engine component that contains a series of lined apertures. The component is removed from the engine, and then at least one of the aperture liners is also removed. The area adjacent the aperture is machined to remove a portion of the parent material of the component. An insert which replaces the material removed by machining is secured adjacent the aperture. The liner about the aperture is then replaced.

REFERENCES:
patent: 4655682 (1987-04-01), Kunz et al.
patent: 5074752 (1991-12-01), Murphy et al.
patent: 5083900 (1992-01-01), Carletti et al.
patent: 5494404 (1996-02-01), Furseth et al.
patent: 5765993 (1998-06-01), Weiss
patent: 6619917 (2003-09-01), Glover et al.

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