Thrust reverser assembly
AssigneeMRA Systems, Inc.
InventorsTimothy Robert Beasman, Andrew Michael Roach, Graham Frank Howarth
Life of this patent
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AssigneeMRA Systems, Inc.
InventorsTimothy Robert Beasman, Andrew Michael Roach, Graham Frank Howarth
Estimating the term…
A thrust reverser assembly for high-bypass turbofan engine. The thrust reverser assembly includes a translating cowl mounted to a nacelle of an engine. The thrust reverser assembly includes blocker doors axially guided adjacent first ends thereof by a fixed structure and pivotally and slidably connected along lengths thereof to an inner wall of the translating cowl so that translation of the translating cowl in the aft direction causes the blocker door to move from a stowed position to a deployed position. The thrust reverser assembly includes a stop disposed on the core engine or on the blocker door, receiving the load from the high pressure airflow, otherwise borne by an actuation system when deploying the translating cowl and blocker door.
A gas turbine engine, comprising:
A thrust reverser assembly for a gas turbine engine including a core engine, a nacelle surrounding at least a portion of the core engine to define a bypass duct between the nacelle and the core engine, comprising:
A method of carrying aerodynamic loading on a blocker door of a thrust reverser for a gas turbine engine having a core engine surrounded by a nacelle to define a bypass duct, the method comprising:
Dependencies are inferred from the claim text.