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In Situ Gas Turbine Prevention of Crack Growth Progression

  • US 20170218764A1
  • Filed: 02/03/2016
  • Published: 08/03/2017
  • Est. Priority Date: 02/03/2016
  • Status: Active Grant
First Claim
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1. A method of remotely joining material a surface area of a component of a gas turbine engine, the method comprising:

  • inserting an integrated repair interface attached to a cable delivery system within a gas turbine engine;

    positioning a tip of the integrated repair interface adjacent to a defect defined within a surface of the component;

    temporarily attaching the tip adjacent to the defect within the surface of the component; and

    supplying a new material to the area to fill the defect.

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