Anti-ice supply system for inlet guide vanes
Disclosed is a gas turbine engine including a plurality of inlet guide vanes. The gas turbine engine further includes an inlet case supporting each of the plurality of inlet guide vanes, and the inlet case is provided with at least one passageway in communication with a source of fluid. The at least...
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Main Author | |
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Format | Patent |
Language | English |
Published |
26.04.2016
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Subjects | |
Online Access | Get full text |
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Summary: | Disclosed is a gas turbine engine including a plurality of inlet guide vanes. The gas turbine engine further includes an inlet case supporting each of the plurality of inlet guide vanes, and the inlet case is provided with at least one passageway in communication with a source of fluid. The at least one passageway is configured to communicate the fluid to each of the plurality of inlet guide vanes. |
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Bibliography: | Application Number: US201213714788 |