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Axial locating means for airfoils

  • US 3,248,081 A
  • Filed: 12/29/1964
  • Issued: 04/26/1966
  • Est. Priority Date: 12/29/1964
  • Status: Expired due to Term
First Claim
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1. IN AN AFT-FAN GAS TURBINE ENGINE, A ROTOR ASSEMBLY COMPRISING:

  • A ROTOR DISC HAVING AN UPSTREAM FACE AND A DOWNSTREAM FACE AND A PLURALITY OF CIRCUMFERENTIALLY SPACED AXIAL DOVETAIL SLOTS IN THE RIM THEREOF, THE OUTER PERIPHERY OF SAID ROTOR DISC RIM INTERMEDIATE SAID PLURALITY OF DOVETAIL SLOTS FORMING A PLURALITY OF LANDS, A PLURALITY OF AIRFOIL MEMBERS HAVING DOVETAIL BASES RECEIVED IN RESPECTIVE ONES OF SAID SLOTS AND EXTENDING RADIALLY OUTWARDLY THEREFROM, SAID PLURALITY OF AIRFOIL MEMBERS COOPERATING TO FORM A FIRST SEGMENTED RING SURROUNDING SAID ROTOR DISC RIM IN RADIALLY SPACED RELATIONSHIP THERETO, A ROW OF AIRFOIL SHAPED TURBINE BUCKETS PERIPHERALLY MOUNTED ON SAID FIRST RING, A SECOND SEGMENTED RING MOUNTED ON THE OUTER TIPS OF SAID TURBINE BUCKETS, AND A ROW OF AIRFOIL SHAPED COMPRESSOR VANES PERIPHERALLY MOUNTED ON SAID SECOND RING, A PLURALITY OF RIGID LOCATING MEMBERS, EACH OF SAID LOCATING MEMBERS POSITIONED ON A RESPECTIVE ONE OF SAID LANDS INWARDLY OF SAID FIRST RING AND

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