Dual-purpose ejector for aircraft load jettisoning mechanism

Aeronautics and astronautics – Aircraft structure – Passenger or cargo loading or discharging

Patent

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Details

89 15C, 89 15F, B64D 102

Patent

active

040882870

ABSTRACT:
In a telescopic retractable ejector, the driving gas is allowed to flow freely with the maximum efficiency by compensating the pressure drop resulting from the gas expansion during the piston extension with a concomitant and automatic increment in the surface area of the pistons which is exposed to the gas pressure.

REFERENCES:
patent: 2931341 (1960-04-01), Meadows et al.
patent: 3557550 (1971-01-01), LeGarra
patent: 3756545 (1973-09-01), Coutin

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