×

Situ Gas Turbine Prevention of Crack Growth Progression

  • US 20170218762A1
  • Filed: 02/03/2016
  • Published: 08/03/2017
  • Est. Priority Date: 02/03/2016
  • Status: Abandoned Application
First Claim
Patent Images

1. A method of remotely stopping a crack in 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 the tip adjacent to a defect within a surface of the component;

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

    drilling a hole into the base of the defect.

View all claims
  • 1 Assignment
Timeline View
Assignment View
    ×
    ×