Invention Publication
- Patent Title: COMPOSITE AIRFOIL ASSEMBLY HAVING A DOVETAIL PORTION
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Application No.: US18088957Application Date: 2022-12-27
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Publication No.: US20240209741A1Publication Date: 2024-06-27
- Inventor: Nicholas Joseph Kray , Elzbieta Kryj-Kos , Tod Winton Davis , Gary Willard Bryant, JR.
- Applicant: GENERAL ELECTRIC COMPANY
- Applicant Address: US NY Schenectady
- Assignee: GENERAL ELECTRIC COMPANY
- Current Assignee: GENERAL ELECTRIC COMPANY
- Current Assignee Address: US NY Schenectady
- Main IPC: F01D5/28
- IPC: F01D5/28 ; F01D5/14 ; F01D5/30
Abstract:
A composite blade assembly for a turbine engine. The composite blade assembly having a core, a first skin and a second skin. The core having a composite structure. The first skin having at least one composite ply. The second skin having at least one composite ply. The first skin having a first radius. The second skin having a second radius.
Public/Granted literature
- US12253006B2 Composite airfoil assembly having a dovetail portion Public/Granted day:2025-03-18
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