Invention Grant
- Patent Title: Ablatable shaft feature in a gas turbine engine
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Application No.: US15819011Application Date: 2017-11-21
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Publication No.: US10753281B2Publication Date: 2020-08-25
- Inventor: Kaliya Balamurugan , Jason Husband
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: RAYTHEON TECHNOLOGIES CORPORATION
- Current Assignee: RAYTHEON TECHNOLOGIES CORPORATION
- Current Assignee Address: US CT Farmington
- Agency: Cantor Colburn LLP
- Main IPC: F01D5/02
- IPC: F01D5/02 ; F02C7/06 ; F01D21/04 ; F02C7/36 ; F01D1/26 ; F02C3/067 ; F02K3/06

Abstract:
A multi-shaft assembly includes an inner shaft and an outer shaft coaxially aligned with the inner shaft to establish a shared axis of rotation. The multi-shaft assembly also includes an ablatable shaft feature with a lubricant surface coating on an interior surface of the outer shaft and an ablatable metallic alloy layer overlaying a portion of the lubricant surface coating with a radial air gap formed between the ablatable metallic alloy layer and an exterior surface of the inner shaft.
Public/Granted literature
- US20190153945A1 ABLATABLE SHAFT FEATURE IN A GAS TURBINE ENGINE Public/Granted day:2019-05-23
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