Integrated strut-vane nozzle (ISV) with uneven vane axial chords
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United States of America Patent
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Mar 6, 2018
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N/A
app pub date -
Nov 12, 2015
filing date -
Jul 24, 2015
priority date (Note) -
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Abstract
An integrated strut and turbine vane nozzle (ISV) comprising: inner and outer duct walls defining a flow passage therebetween, an array of circumferentially spaced-apart struts extending radially across the flow passage, and an array of circumferentially spaced-apart vanes extending radially across the flow passage. At least one of the struts is aligned in the circumferential direction with an associated one of the vanes and forms therewith an integrated strut-vane airfoil. The adjacent vanes on opposed sides of the integrated strut-vane airfoil have uneven axial chords relative to the other vanes.
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