Invention Grant
- Patent Title: Airfoil core inlets in a rotating vane
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Application No.: US16055761Application Date: 2018-08-06
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Publication No.: US11668202B2Publication Date: 2023-06-06
- Inventor: Corey D. Anderson
- 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: Snell & Wilmer L.L.P.
- Main IPC: F01D9/06
- IPC: F01D9/06 ; F01D9/04 ; F01D17/16
Abstract:
A component for a gas turbine engine includes an airfoil, including therein a first cavity and a second cavity, and an outer spindle extending from the airfoil, the outer spindle including a first channel in fluid communication with the first cavity and a second channel in fluid communication with the second cavity.
Public/Granted literature
- US20200040760A1 AIRFOIL CORE INLETS IN A ROTATING VANE Public/Granted day:2020-02-06
Information query
