GAS TURBINE ASYMMETRIC NOZZLE GUIDE VANES
A gas turbine engine includes a multiple of Nozzle Guide Vanes (NGVs) arranged asymmetrically and a multiple of NGVs clocked with respect to the multiple of fuel nozzles around a 360 degree circumference.
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Main Authors | , |
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Format | Patent |
Language | English |
Published |
27.03.2014
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Subjects | |
Online Access | Get full text |
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Summary: | A gas turbine engine includes a multiple of Nozzle Guide Vanes (NGVs) arranged asymmetrically and a multiple of NGVs clocked with respect to the multiple of fuel nozzles around a 360 degree circumference. |
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Bibliography: | Application Number: US201213626511 |