FIELD: aircraft emergency escape systems.
SUBSTANCE: method of emergency escape by the crew of an aircraft consists of ejecting the crew of the aircraft and parachute system with the gradual destruction of the cockpit glazing using a telescopic-type firing mechanism and a power element of the parachute system. When turned, the deflectable headrest (1) completes the destruction of the cockpit glazing, forming a hole in the canopy sufficient for the free and safe passage of the ejected pilot. After the destruction of the cabin glazing, the deflectable headrest is returned to its initial position using the force of the oncoming air flow. The control element for opening the lock of the initial position and rotating the tilted headrest (1) at the moment of ejection are the breaking elements (6).
EFFECT: improved pilot safety during an emergency exit from the aircraft through the glazing.
2 cl, 4 dwg
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Authors
Dates
2024-02-06—Published
2022-11-02—Filed