发明名称 ЗАМОК ДЛЯ ПОВОРОТНОГО КРЕПЕЖНОГО ЭЛЕМЕНТА И ШАРНИРНЫЙ УЗЕЛ МЕХАНИЧЕСКОЙ СИСТЕМЫ УПРАВЛЕНИЯ ПОВЕРХНОСТЯМИ УПРАВЛЕНИЯ САМОЛЕТА С ИСПОЛЬЗОВАНИЕМ УПОМЯНУТОГО ЗАМКА
摘要 FIELD: mechanical engineering. ^ SUBSTANCE: lock comprises locking side and stop that is in a contact with the locking side. The lock is also provided with the additional stop and transverse lock and made of jaw lug that defines the stops and base with the adjusting pawl. The base is provided with the centering opening for rotatable locking member interposed between the stops. The pivoting unit of the mechanism for control of the all-moving surfaces comprises jaw and rod members with lugs interconnected through a bolt with the nut cottered at its end, transverse lock for the bolt head, main bushing for the bolt, and, at least, one bearing. The unit is provided with lock for the bolt mounted on one of the jaw lugs and additional bushing. Each bushing is set in the opening in the appropriate wall of the jaw member. The bearing is mounted directly on the rod section of the bolt. ^ EFFECT: enhanced reliability. ^ 4 cl, 12 dwg
申请公布号 RU2003134842(A) 申请公布日期 2005.05.10
申请号 RU20030134842 申请日期 2003.12.01
申请人 ФГУП "ЭМЗ им. В.М. М сищева" (RU) 发明人 Королев Виктор Михайлович (умер);Малышевский Александр Николаевич (RU)
分类号 F16B1/00;B64C13/00;F16B39/10 主分类号 F16B1/00
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