IN2014CH00506AIN506CH2014AIN2014CH00506AIN 2014CH00506 AIN2014CH00506 AIN 2014CH00506AIN 506CH2014 AIN506CH2014 AIN 506CH2014AIN 2014CH00506 AIN2014CH00506 AIN 2014CH00506A
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Priority to IN506CH2014priorityCriticalpatent/IN2014CH00506A/en
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Output director vane for an aircraft turbine engine, with an improved lubricant cooling function using a heat conduction matrix housed in a vane inner duct