Fluid transport system having divided transport tube
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United States of America Patent
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Mar 27, 2018
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app pub date -
Oct 20, 2014
filing date -
Oct 24, 2013
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Abstract
A fluid transport system for a gas turbine engine includes a plenum configured to provide a fluid, an airfoil having an internal cavity, and a transfer tube arranged to transfer the fluid between the plenum and the internal cavity of the airfoil. The transfer tube includes an inlet, an outlet, a cavity extending from the inlet to the outlet, and at least one partition wall dividing the cavity into multiple flow passages.
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