Invention Grant
- Patent Title: Bulged nozzle for control of secondary flow and optimal diffuser performance
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Application No.: US14884140Application Date: 2015-10-15
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Publication No.: US09988917B2Publication Date: 2018-06-05
- Inventor: Soumyik Kumar Bhaumik , Rohit Chouhan
- Applicant: General Electric Company
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: Fletcher Yoder P.C.
- Main IPC: F01D9/04
- IPC: F01D9/04

Abstract:
A turbine nozzle disposed in a turbine includes a suction side having a bulge, and a pressure side. The suction side and the pressure side extend opposite one another between a leading edge and a trailing edge in an axial direction transverse to a longitudinal axis of the turbine nozzle, and extends a radial direction along the longitudinal axis. The bulge is disposed on the suction side protruding relative to the other portion of the suction side in a direction transverse to both the radial and axial directions. The turbine nozzle has a first periphery defined at a first cross-section at a first location along the height of the turbine nozzle by selected coordinate sets listed in Table 1.
Public/Granted literature
- US20170107835A1 BULGED NOZZLE FOR CONTROL OF SECONDARY FLOW AND OPTIMAL DIFFUSER PERFORMANCE Public/Granted day:2017-04-20
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