Invention Grant
- Patent Title: Turbine component with a thin interior partition
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Application No.: US15934332Application Date: 2018-03-23
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Publication No.: US11459899B2Publication Date: 2022-10-04
- Inventor: Dilip M. Shah , Alan D. Cetel , Venkatarama K. Seetharaman , Raymond Surace
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Farmington
- Agency: Cantor Colburn LLP
- Main IPC: F01D5/18
- IPC: F01D5/18
Abstract:
A hollow turbine airfoil or a hollow turbine casting including a cooling passage partition. The cooling passage partition is formed from a single crystal grain structure nickel based super alloy, a cobalt based super alloy, a nickel-aluminum based alloy, or a coated refractory metal.
Public/Granted literature
- US20190292920A1 TURBINE COMPONENT WITH A THIN INTERIOR PARTITION Public/Granted day:2019-09-26
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