Invention Application
- Patent Title: TURBINE BLADE ATTACHMENT CURVED RIB STIFFENERS
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Application No.: US15009366Application Date: 2016-01-28
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Publication No.: US20170218776A1Publication Date: 2017-08-03
- Inventor: Charles Thistle , Mohamed Hassan
- Applicant: United Technologies Corporation
- Applicant Address: US CT Hartford
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Hartford
- Main IPC: F01D5/14
- IPC: F01D5/14 ; F01D5/30 ; F01D5/18

Abstract:
The present disclosure provides a fir tree coupling for gas turbine engine parts comprising a load beam having a longitudinal axis, a rounded base, a first side, and a second side, wherein the rounded base has a radius of curvature from the first side to the second side, a tooth running parallel to the longitudinal axis and disposed on the first side of the load beam. The fir tree coupling may comprise a channel through the rounded base across a portion of the radius of curvature from the first side to the second side. The channel may comprise a sidewall having a sidewall step cut into a portion of the channel sidewall.
Public/Granted literature
- US10047611B2 Turbine blade attachment curved rib stiffeners Public/Granted day:2018-08-14
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