Patent ID: 8528857

Claim:
A thrust reverser with cascade vanes configured to form at least part of a downstream section of a nacelle which houses a jet engine, comprising: a front frame attached to a fixed part of the nacelle and supporting peripheral thrust reversal cascade vanes and rams, wherein the rams translationally actuate at least one movable cowling along a longitudinal axis of the nacelle, wherein the front frame comprises, a fixed part for attaching the front frame to the fixed part of the nacelle and for supporting the deflection cascade vanes, and a movable part mounted in a translationally movable manner along the longitudinal axis of the nacelle, wherein, the rams comprise, a first end connected to the movable part, and a second end connected to the cowling, wherein, the fixed part and the movable part of the front frame are connected in a detachable manner by locking means.