CPC E05F 15/643 (2015.01) [B64C 1/1438 (2013.01); B64C 29/0033 (2013.01); E05F 11/04 (2013.01); E05Y 2201/21 (2013.01); E05Y 2201/254 (2013.01); E05Y 2201/26 (2013.01); E05Y 2201/408 (2013.01); E05Y 2900/502 (2013.01); E05Y 2900/531 (2013.01)] | 20 Claims |
1. A door management system on an aircraft comprising:
a fuselage extending along a longitudinal axis in a fore-aft direction parallel to forward flight;
an opening in a sidewall of the fuselage;
a door mounted on the sidewall to slide in the fore-aft direction between a closed position covering the opening and an open position revealing the opening;
a cable attached to the fuselage via a plurality of pulleys and the door via a connector; and
a speed governor attached to the door, wherein the speed governor is operatively coupled to the cable to limit a velocity of the door as it moves between the open position and the closed position.
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