Thrust reverser for an aircraft engine, pod assembly and corresponding powerplant
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United States of America Patent
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Jun 5, 2018
Issued Date -
Jun 9, 2016
app pub date -
Dec 4, 2015
filing date -
Dec 5, 2014
priority date (Note) -
In Force
status (Latency Note)
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Abstract
A thrust reverser for an aircraft engine assembly, comprising two sub-assemblies configured to surround an engine, each of the sub-assemblies comprising an inner fixed structure, a translating cowl, a torque box, a substantially vertical 12 o'clock bifurcation, and a substantially vertical 6 o'clock bifurcation. At least one of the sub-assemblies comprises at least one separating partition extending between the inner fixed structure, the translating cowl and the torque box of the sub-assembly, the separating partition being rigidly fixed to the inner fixed structure and the torque box, and connected to the translating cowl via a sliding connection.
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