×

STATOR VANE FOR A GAS TURBINE ENGINE

  • US 20100150710A1
  • Filed: 12/23/2009
  • Published: 06/17/2010
  • Est. Priority Date: 06/28/2007
  • Status: Active Grant
First Claim
Patent Images

1. A guide vane for a gas turbine comprising:

  • a vane body having a leading edge and a trailing edge; and

    a shroud extending at least between the leading edge and the trailing edge, the shroud having a first side wall and a second side wall extending essentially radially and in a longitudinal direction of the gas turbine, the first side wall having a groove disposed in a region of the trailing edge extending in a longitudinal direction of the shroud and configured to receive a sealing plate, the first side wall further having a clearance extending from the groove in a region of the trailing edge, wherein a depth of the clearance in a circumferential direction of the gas turbine is equal to a depth of the groove, and wherein a width of the clearance in the longitudinal direction of the shroud is between one to three times the depth of the clearance.

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