Apparatus and method for electric spark peening of gas turbine components

I.V. Timoshkin (Inventor), S.J. MacGregor (Inventor), Rolls-Royce PLC (Patent applicant) (Inventor)

Research output: Patent

Abstract

Peening provides compression of component (6, 46, 56) surfaces in order to create residual surface compressions to resist crack propagation in components such as aerofoils. Previously peening techniques have had problems with respect to achieving adequate treatment depths, speed of treatment and with respect to effectiveness. By the present method arrangement an electrical conductor (1, 41, 51) in the form of a wire is subject to electrical pulses to cause evaporation and subsequent breakdown with high power ultrasound (HPU) propagation in a volume of dielectric fluid towards a component and so peening. The electrical conductor (1, 41, 51) ensures that there is limited possibility of electrical discharge to the component (6, 46, 51) surface whilst the positioning of the wire (1, 41, 51) relative to the surface can be adjusted to achieve best effect particularly if reflector (5) devices are utilised to concentrate (HPU) pulse presentation to the component (6, 46, 56). Furthermore, the component (6, 46, 56) can be surface treated in order to provide protection from potentially damaging emissions from evaporation and electrical discharge to the wire (1, 41, 51).
Original languageEnglish
Patent number20100008786
Publication statusPublished - 14 Jan 2010

Keywords

  • patent
  • electric spark peening
  • gas turbines

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  • Cite this

    Timoshkin, I. V., MacGregor, S. J., & Rolls-Royce PLC (Patent applicant) (2010). Apparatus and method for electric spark peening of gas turbine components. (Patent No. 20100008786).