Actuator for aircraft turbine engine nacelle with notably one-piece annular rear part
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United States of America Patent
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Aug 14, 2018
Grant Date -
Sep 18, 2014
app pub date -
May 27, 2014
filing date -
Nov 24, 2011
priority date (Note) -
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Abstract
An actuator for an aircraft turbine engine nacelle with a one-piece annular rear part, includes an engine assembly having a nut which is capable of rotating but not of translational movement, and a shaft for turning this nut. The actuator also includes a screw assembly having a screw capable of translational movement without rotating, in mesh with the nut, and a ball joint at one end of this screw intended to be fixed to the annular rear part.
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