A stretcher loading system for an aircraft is disclosed. The loading system comprises a cabin interface arrangement configured to mount the stretcher loading system to an aircraft cabin, a longitudinal guide arrangement attached to the cabin interface arrangement; and a trolley assembly configured to slidably engage with the longitudinal guide arrangement and moveable along the longitudinal guide arrangement from an extended stretcher receiving position where the trolley assembly engages with a stretcher to a retracted retained position where the stretcher is located in the aircraft cabin and loaded in the aircraft.
STRETCHER LOADER SYSTEM
2021-06-17
Patent
Electronic Resource
English
NTRS | 1967
|NTIS | 1971
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