Invention Grant
- Patent Title: Turbine air flow conditioner
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Application No.: US14313198Application Date: 2014-06-24
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Publication No.: US09803864B2Publication Date: 2017-10-31
- Inventor: Arjun Singh , Chandrasekhar Pushkaran , Nishant Govindbhai Parsania
- Applicant: General Electric Company
- Applicant Address: US NY Schnectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schnectady
- Agency: Nixon & Vanderhye P.C.
- Main IPC: F23R3/10
- IPC: F23R3/10 ; F23R3/28 ; F23R3/04 ; F23R3/06

Abstract:
A turbine combustor section has a flow conditioner including a plurality of conduits arranged to convey pressurized air to an air chamber for entrance into a plurality of fuel nozzles. Each conduit includes an inlet configured to receive the pressurized air from an annular passage and an outlet configured to deliver the pressurized air to the air chamber. A cross-sectional area of each conduit varies between the inlet and the outlet so as to reduce a pressure drop across the flow conditioner.
Public/Granted literature
- US20150369488A1 TURBINE AIR FLOW CONDITIONER Public/Granted day:2015-12-24
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