×

Small radial profile shroud for variable vane structure in a gas turbine engine

  • US 7,713,022 B2
  • Filed: 03/06/2007
  • Issued: 05/11/2010
  • Est. Priority Date: 03/06/2007
  • Status: Active Grant
First Claim
Patent Images

1. A shroud for supporting a variable vane in a compressor for a gas turbine engine comprising:

  • at least two components extending circumferentially, to support a radially inner trunnion on a variable vane and said at least two components being connected by a threaded fastener member extending through a hole in a first of said at least two components and into a blind hole in a second of said at least two components and wherein one of said components has additional material extending therefrom that is adapted to engage said threaded fastener and wherein said additional material is disposed within a slot within said other component.

View all claims
  • 4 Assignments
Timeline View
Assignment View
    ×
    ×