AIRCRAFT GAS TURBINE COMPRISING AN ENGINE COWLING WITH A THRUST-REVERSER DEVICE
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United States of America Patent
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Issued Date -
Jun 25, 2015
app pub date -
Dec 18, 2014
filing date -
Dec 19, 2013
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Abstract
The present invention relates to an aircraft gas turbine comprising an engine cowling that has a rear area, with respect to the direction of the flow, which has a thrust-reverser device, wherein the rear area is embodied in such a manner as to be translatable in the axial direction, characterized in that the rear area is mounted in a translatable manner at two rails that are arranged in parallel to each other, and that it comprises a gear rack that is mounted at each rail, respectively, with the gear rack being in mesh with a respective cog wheel, which is coupled to a common motor via a gear unit, respectively.
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