FIELD: aviation technology.
SUBSTANCE: invention relates to the field of aviation technology. The control system for the emergency opening of the aircraft canopy or its part includes a pneumatic cylinder (1) for emergency resetting of the canopy or its part, a gas generator (2), at least one electric detonator (3) connected to the gas generator (2). The electric detonator (2) is made with the possibility of operation during ejection. The system also contains a mechanical initiating device (4) connected to the gas generator (2) and configured to operate without ejection.
EFFECT: invention provides a reduction in the time of formation of an emergency exit, an increase in the probability of rescuing the crew in a dangerous situation, the safety of the crew, and an increase in the reliability of the emergency opening of the lantern or its part.
3 cl, 2 dwg
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Authors
Dates
2022-11-15—Published
2022-04-15—Filed