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Небесная энциклопедия

Космические корабли и станции, автоматические КА и методы их проектирования, бортовые комплексы управления, системы и средства жизнеобеспечения, особенности технологии производства ракетно-космических систем

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Применить Всего найдено 2. Отображено 2.
13-07-2022 дата публикации

Anti-recoil assembly

Номер: GB0002602701A
Автор: JOHN HAMPTON [US], KASSIDY L CARSON [US], RYAN L ROSEKE [US]
Принадлежит:

An anti-recoil assembly, for example in an ejection seat stability system, includes a housing 210, a shaft 220, and an energy attenuator 230. The housing defines a cavity 215 and has a first end portion 212 and a second end portion 214. The shaft is partially disposed within the cavity and is configured to move within the cavity in a first direction 22 from the first end portion to the second end portion. The energy attenuator is disposed within the cavity at the second end portion. In response to movement of the shaft, in the first direction, the energy attenuator inhibits the shaft from recoiling in a second direction 24 opposite the first direction. Also provided is an ejection seat stability system configured to control seat pitch during an ejection event, the system comprising a stabilizing gyro 26, a shaft comprising gear teeth 226, a housing defining a cavity, an actuator 28, and an energy attenuator. The gyro comprises a pinion engaged by the gear teeth of the shaft. The actuator ...

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Номер записи: 1
07-09-2022 дата публикации

Aircraft escape system and ejection seat sequencer for ejection systems

Номер: GB0002604432A
Автор: JOHN HAMPTON [US]
Принадлежит:

An aircraft ejection system 100 for controlling deployment of aircraft escape and ejection seat subsystems comprises a sequencer 120 configured to receive a power input 140, 142, to send a first deploy signal to a first aircraft escape subsystem, and to send a second deploy signal to a first ejection seat subsystem. The first aircraft escape subsystem may comprise at least one of a canopy removal system 124 and a seat catapult system 126. The first ejection seat subsystem may comprise at least one of a drogue parachute assembly 132, a main parachute assembly 130, a restraint release assembly 134 and an inertia reel assembly 138. The sequencer may send a third deploy signal to a second aircraft escape subsystem, the first aircraft escape subsystem comprising a canopy removal system and the second aircraft escape subsystem comprising a seat catapult system. The sequencer may determine if a first electrical connector 186 electrically coupled to the canopy removal system is disconnected from ...

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Номер записи: 2