FIELD: transport.
SUBSTANCE: invention relates to aerospace engineering and may be used for pressure release from aircraft of its separated assembly unit. Proposed device comprises power cylinder with spring accommodated therein, rod, ears and cover. Power cylinder is composed of hollow bar with spring accommodated therein. Spring ends are locked in face walls of said hollow rod composed of two parts fitted on axle to displace thereon. Structural part three ears are arranged above both rod halves and at axle center while cover two ears are arranged there between. Power cylinder is provided with spring ends relocking mechanism. For this, ledges are made at rod both parts while lengthwise grooves to accommodate said ledges are made in case and cover ears. Said grooves are made at different angles to vertical.
EFFECT: higher stability and reliability.
11 dwg
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