Invention Grant
- Patent Title: Turbine engine variable area vane with feather seal
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Application No.: US14789573Application Date: 2015-07-01
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Publication No.: US09909435B2Publication Date: 2018-03-06
- Inventor: Tracy A. Propheter-Hinckley
- Applicant: United Technologies Corporation
- Applicant Address: US CT Hartford
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Hartford
- Agency: O'Shea Getz P.C.
- Main IPC: F01D11/00
- IPC: F01D11/00 ; F01D17/16 ; F01D9/04

Abstract:
An apparatus for sealing a gap between a stator vane platform including a seal slot, and a rotatable stator vane including a shaft connected to a vane end. The apparatus includes a substantially flat, semi-annular seal body, a first tab and a second tab. The seal body extends circumferentially between a first body end and a second body end, and radially between a radial inner body side and a radial outer body side. The inner body side wraps partially around the shaft, and the outer body side mates with the seal slot. The first tab extends axially from the first body end, and the second tab extends axially from the second body end. The first tab and the second tab engage the vane end and cause the seal body to move within the seal slot during rotation of the stator vane.
Public/Granted literature
- US20150300186A1 TURBINE ENGINE VARIABLE AREA VANE WITH FEATHER SEAL Public/Granted day:2015-10-22
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