×

GAS TURBINE ENGINE TURBINE DIAPHRAGM WITH ANGLED HOLES

  • US 20140086727A1
  • Filed: 09/26/2012
  • Published: 03/27/2014
  • Est. Priority Date: 09/26/2012
  • Status: Active Grant
First Claim
Patent Images

1. A gas turbine engine turbine diaphragm, comprising:

  • an inner cylindrical portion;

    a mounting portion located radially outward from the inner cylindrical portion; and

    a disk portion extending radially between the inner cylindrical portion and the mounting portion, the disk portion havinga plurality of angled holes, each angled hole following a vector which is angled in at least one plane with a component of the vector being located on a plane perpendicular to a radial extending from an axis of the diaphragm, the component of the vector being angled relative to an axial direction of the diaphragm.

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