Invention Grant
- Patent Title: Diverging-converging cooling passage for a turbine blade
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Application No.: US15062952Application Date: 2016-03-07
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Publication No.: US10260355B2Publication Date: 2019-04-16
- Inventor: Jason Smoke , David K Jan , Amandine Miner , Deanna Pinar Chase , Michael Kahrs , Lorenzo Crosatti
- Applicant: HONEYWELL INTERNATIONAL INC.
- Applicant Address: US NJ Morris Plains
- Assignee: HONEYWELL INTERNATIONAL INC.
- Current Assignee: HONEYWELL INTERNATIONAL INC.
- Current Assignee Address: US NJ Morris Plains
- Agency: Lorenz & Kopf, LLP
- Main IPC: F01D5/18
- IPC: F01D5/18 ; F01D5/04 ; F01D1/08 ; F01D5/30

Abstract:
A turbine blade and a radial turbine having at least one blade is provided. The turbine blade includes a trailing edge and a leading edge opposite the trailing edge. The turbine blade also includes a cooling passage defined internally within the turbine blade. The cooling passage is in fluid communication with a source of cooling fluid via a single inlet to receive a cooling fluid. The cooling passage diverges at a first point downstream from the single inlet into at least two branches that extend along the at least one blade from the first point to a second point near a tip of the leading edge and the cooling passage converges at the second point.
Public/Granted literature
- US20170254209A1 DIVERGING-CONVERGING COOLING PASSAGE FOR A TURBINE BLADE Public/Granted day:2017-09-07
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