FIELD: aeronautical engineering. SUBSTANCE: system provides for shifting the canopy in longitudinal plane and jettisoning it upward at angle relative to longitudinal plane. System is provided with retainers for locking the canopy in working position, actuator made in form of cylinder, locking mechanism with bell crank engageable with actuating cylinder and connected with control lever by means of rod. Control lever is engageable with bearing pad of canopy by means of spherical head. Lower end of control lever is provided with grip engageable with bearing sector of fuselage. System is provided with guide mechanism made in form of telescopic rods with retainers. Front ends of telescopic rods are secured on canopy and rear ends are connected with inclined axles by means of split hinges. EFFECT: avoidance of collision of canopy with pilot's seat during its ejection; enhanced safety. 1 dwg
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Authors
Dates
1999-05-27—Published
1997-10-22—Filed