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

Claim 16:
17. An apparatus for an aircraft propulsion system, comprising:
a propulsion system structure including a flowpath and a thrust reverser system;
the flowpath extending within the propulsion system structure to an exhaust nozzle;
the thrust reverser system comprising a thrust reverser cascade;
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 distributed longitudinally along the cascade inner face, and the plurality of vanes including a first vane and a second vane longitudinally aft of the first vane; and
the wall longitudinally between and connected to the first vane and the second vane; and
the plurality of vanes exposed to the flowpath when the thrust reverser system is stowed.