Door latch positioning mechanism
AssigneeTextron Innovations Inc.
InventorsRichard Stoddard Conkling, Evan M. Johnson, Joseph Allan Smarsh
Life of this patent
Estimating the term…
Loading patent…
AssigneeTextron Innovations Inc.
InventorsRichard Stoddard Conkling, Evan M. Johnson, Joseph Allan Smarsh
Estimating the term…
A latch positioning mechanism for an aircraft door includes one or more locking members configured to be partially driven into a frame around the door via rotation of a pivot pin. A frame bumper extends outside of the door in a pre-catch position for contacting the frame. A catch bellcrank is operatively coupled to the frame bumper, and a biasing member biases rotation of the catch bellcrank to bias the frame bumper into the pre-catch position. The catch bellcrank is configured to contact a catch cam when the catch bellcrank is biased into the pre-catch position such that the catch cam prevents release of the one or more locking members for locking the door. Upon the frame bumper contacting the frame when the door is closed, the catch cam is released enabling the one or more locking members to be moved into a locked position.
A latch positioning mechanism for a door of an aircraft configured to retain a latching and locking system of the door in a pre-catch position when the door is open, and release the latching and locking system from the pre-catch position when the door is closed, the latch positioning mechanism comprising:
A latch positioning mechanism for a door of an aircraft, comprising:
A pre-catch latch positioning method for a door of an aircraft, comprising:
Dependencies are inferred from the claim text.