Patent ID: 11873781
Assignee: ROHR, INC.
Field: Engines, pumps, turbines (Mechanical engineering)
Classification: CPC F | IPC F

Claim 0:
1. An apparatus for an aircraft propulsion system, comprising:
a thrust reverser system including a thrust reverser door and a thrust reverser cascade;
the thrust reverser door configured to move relative to the thrust reverser cascade between a stowed position and a deployed position;
the thrust reverser cascade extending longitudinally between a cascade forward end and a cascade aft end, the thrust reverser cascade extending laterally between a cascade first side and a cascade second side, and the thrust reverser cascade extending radially between a cascade inner face and a cascade outer face;
the thrust reverser cascade including a plurality of vanes and a wall;
the plurality of vanes arranged in a longitudinally extending array along the cascade inner face, and the plurality of vanes including a first vane and a second vane; and
the wall configured to block gas flow radially through the thrust reverser cascade between the first vane and the second vane when the thrust reverser door is in the deployed position, and wherein the wall is disposed at the cascade inner face.