THRUST INVERTER FOR AN AIRCRAFT ENGINE ASSEMBLY, NACELLE AND CORRESPONDING ENGINE ASSEMBLY

摘要

The invention relates to a thrust reverser for an aircraft engine assembly, comprising two subassemblies (430) intended to surround a reactor, each of said subassemblies (430) comprising an internal cover (431), an external sliding cover (432), an outer ring (435), a substantially vertical high bifurcation partition (436), and a substantially vertical low bifurcation partition (437). According to the invention, at least one of said subassemblies (430) comprises at least one partition (45) extending between the inner cover (431), the outer sliding cover (432) and the outer ring ( 435) of said subassembly (430), said partition wall (45) being fixedly attached to said inner cover (431) and to said outer ring gear (435), and connected to said outer sliding cover (432) by a slide connection.