Invention Grant
- Patent Title: Effect of the nozzle width to harness on engine pulse energy
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Application No.: US16766775Application Date: 2018-11-22
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Publication No.: US11542862B2Publication Date: 2023-01-03
- Inventor: Stephen David Hughes
- Applicant: Cummins Ltd
- Applicant Address: GB London
- Assignee: Cummins Ltd
- Current Assignee: Cummins Ltd
- Current Assignee Address: GB London
- Agency: Faegre Drinker Biddle & Reath LLP
- Priority: GB1719591 20171124
- International Application: PCT/GB2018/053381 WO 20181122
- International Announcement: WO2019/102200 WO 20190531
- Main IPC: F02C6/12
- IPC: F02C6/12 ; F01D9/02 ; F01D17/14 ; F02B37/02 ; F04D29/42

Abstract:
A turbine comprises a turbine wheel for rotation within a turbine housing, the turbine housing including at least one volute arranged to deliver a fluid to the turbine wheel via the turbine nozzle. A method for determining a width of a turbine nozzle for the turbine, comprises selecting from a relationship between a turbine stage efficiency and an effective nozzle area, at least one target effective nozzle area. As used here, the effective nozzle area is dependent on both the width of the turbine nozzle and a whirl angle induced by the at least one volute. The method further comprises determining, in dependence on the whirl angle, the width of the turbine nozzle as a width that will achieve the at least one target effective nozzle area.
Public/Granted literature
- US20200300160A1 THE EFFECT OF THE NOZZLE WIDTH TO HARNESS ON ENGINE PULSE ENERGY Public/Granted day:2020-09-24
Information query
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