Invention Application
- Patent Title: UNDER-ROOT SPACER FOR GAS TURBINE ENGINE FAN BLADE
- Patent Title (中): 用于气体涡轮发动机叶片的底盘
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Application No.: US14161760Application Date: 2014-01-23
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Publication No.: US20140219807A1Publication Date: 2014-08-07
- Inventor: Santiago Lattanzio , Michael A. Weisse
- 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: F01D5/30
- IPC: F01D5/30

Abstract:
A gas turbine engine rotor includes a hub having a slot. A blade includes a root received in the slot. An under-root area is provided between the root and the fan hub in the slot. A spacer includes first and second portions that cooperate with one another to provide an adjustment feature with discrete height settings. The adjustment feature provides different radial heights of the spacer. The spacer is arranged in the under-root area beneath the root.
Public/Granted literature
- US09562438B2 Under-root spacer for gas turbine engine fan blade Public/Granted day:2017-02-07
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