Connecting gas turbine engine annular members

Connecting gas turbine engine annular members

  • CN 104,246,196 A
  • Filed: 04/26/2013
  • Published: 12/24/2014
  • Est. Priority Date: 04/27/2012
  • Status: Active Application
First Claim
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1. a gas turbine assembly, comprising:

  • Gas turbine engine first and second annular element (41,48), it has the first and second different thermal expansion coefficient,Described first and second annular elements (41,48) utilize both arms V-arrangement bracket (50) to link together,Each in described both arms V-arrangement bracket (50) comprises the first and second arms (62,64) angularly separated from pallet centerline (70),Described first and second arms (62,64) remotely axially extend from pallet base (72),Described pallet base (72) is attached to first in described first and second annular elements (41,48), andDescribed first and second arms (62,64) are attached to second in described first and second annular elements (41,48).

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