Invention Grant
- Patent Title: Turbine engine with airfoil having high acceleration and low blade turning
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Application No.: US17876009Application Date: 2022-07-28
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Publication No.: US11885233B2Publication Date: 2024-01-30
- Inventor: Ernesto Sozio , Francesco Bertini , Jeffrey Donald Clements , Jonathan Ong , Lyle Douglas Dailey , Paul Hadley Vitt , Matteo Renato Usseglio
- Applicant: General Electric Company , GE Avio S.r.l.
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company,GE Avio S.r.l.
- Current Assignee: General Electric Company,GE Avio S.r.l.
- Current Assignee Address: US NY Schenectady; IT Rivolta di Torino
- Agency: McGarry Bair PC
- Priority: IT 2020000005146 2020.03.11
- Main IPC: F01D5/14
- IPC: F01D5/14 ; F04D29/32 ; F04D29/54
Abstract:
A turbine engine with at least a compressor section, combustor section, turbine section and a set of airfoils. The airfoils include geometric characteristics to create a high contraction ratio (CR), a low blade turning (BT) at a radially inward location the airfoil, a low solidity, or a low aspect ratio (AR).
Public/Granted literature
- US20230130213A1 TURBINE ENGINE WITH AIRFOIL HAVING HIGH ACCELERATION AND LOW BLADE TURNING Public/Granted day:2023-04-27
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