Apparatus for assembling gas turbine engines

Apparatus for assembling gas turbine engines

  • CN 1,769,648 A
  • Filed: 11/04/2005
  • Published: 05/10/2006
  • Est. Priority Date: 11/04/2004
  • Status: Active Application
First Claim
Patent Images

1. the stator vane assembly (52) of a gas turbine engine (10), described blade assembly comprises a plurality of paired stator vanes (80) along the circle spacing, each described paired stator vane is included in a pair of stator vane (66) that links together on the corresponding external stator bucket platform (70) of each described blade, the configuration of each described stator vane platform makes each described paired stator vane be connected slidably with a blade guide rail (88) that stretches out from this compressor housing (36), and this compressor housing (36) extends at least in part along the circumferential direction around described stator vane assembly.

View all claims
    ×
    ×

    Thank you for your feedback

    ×
    ×