VANE FOR AN AIRCRAFT TURBINE ENGINE
A rotor vane for an aircraft turbine engine, the vane having an axis of rotation once it has been rigidly connected to a rotor and a stacking axis. The vane includes a blade extending between an internal platform and an external platform bearing at least one projecting lip. The external platform is...
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Format: | Patent |
Sprache: | eng ; fre ; ger |
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