发明名称 DEVICE FOR FIXATION OF MODULAR ELEMENT IN AIRCRAFT
摘要 FIELD: construction.SUBSTANCE: device for fixation comprises a pin, at the first end of which there is a thickened head for gripping in a support slot of a support structure and a section adjacent to the heat with the first transverse dimension and the second transverse dimension, substantially perpendicular to the first transverse size and larger than the first transverse dimension. At the opposite second end of the pin there is a lever, which is connected with the pin for rotation and is arranged as capable of displacement into the open position and the closed position. A bushing installed on the pin as capable of longitudinal displacement is arranged as capable of support of an outer wall of a modular element on it and an electroconductive flat spring provided for contact at one side at the outer side of the outer wall, and at the other side, with the support structure. An eccentric controlled by the lever is arranged as capable of bushing displacement along the pin in direction of the head as the lever moves into its closed position.EFFECT: simplicity and reliability of installation.16 cl, 7 dwg
申请公布号 RU2478166(C1) 申请公布日期 2013.03.27
申请号 RU20110136556 申请日期 2010.02.10
申请人 EHJRBAS OPEREHJSHNZ GMBKH 发明人 SHMITS GJUNTER
分类号 F16B2/18 主分类号 F16B2/18
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