Invention Grant
- Patent Title: First stage turbine nozzle with erosion coating surface finish
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Application No.: US14584499Application Date: 2014-12-29
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Publication No.: US10214804B2Publication Date: 2019-02-26
- Inventor: Craig M. Beers , Kevin M. Rankin
- Applicant: Hamilton Sundstrand Corporation
- Applicant Address: US NC Charlotte
- Assignee: Hamilton Sundstrand Corporation
- Current Assignee: Hamilton Sundstrand Corporation
- Current Assignee Address: US NC Charlotte
- Agency: Kinney & Lange, P.A.
- Main IPC: C23C4/129
- IPC: C23C4/129 ; B64D13/08 ; B64D13/02 ; B22D25/02 ; F01D9/04 ; C23C4/06 ; F04D29/32 ; B64D13/06 ; F04D25/04

Abstract:
A first stage turbine nozzle includes a first stage hub portion extending axially along a central axis, a first stage disk portion attached to the first stage hub portion and centered on the central axis, and a plurality of first stage vanes positioned radially around and attached to the first stage disk portion. Each vane extends a vane height H away from the first stage disk portion and each vane has a first end positioned at a diameter D away from the central axis. The first stage turbine nozzle also includes a plurality of first stage throats defined between radially adjacent first stage vanes. Each first stage throat has a throat width W between radially adjacent first stage vanes. The first stage turbine nozzle also includes a coating on a sidewall of each first stage vane.
Public/Granted literature
- US20160186586A1 FIRST STAGE TURBINE NOZZLE WITH EROSION COATING SURFACE FINISH Public/Granted day:2016-06-30
Information query
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