发明名称 DRIVE OF CARRYING CONTROL PLANE OF AIRBORNE VEHICLE
摘要 FIELD: machine building.SUBSTANCE: invention refers to disclosure and automatic setting to working position of carrying control plane of an airborne vehicle (AV). Drive of AV carrying control plane includes a rigidly installed housing, a power cylinder, a piston with a stock, which is kinematically connected to the control plane. Power cylinder is installed in the housing on bearings with possibility of being rotated relative to its longitudinal axis. Above-piston cavity of the power cylinder chamber is made in the form of tight and non-tight gas cavities, and tight cavity under the piston is filled with liquid. In the non-tight gas cavity the kinematic connection of the piston stock to the control plane is made in the form of a rocking bar, a lever and axes that connect them. Axes of the rocking bar and the lever are installed on the power cylinder housing. The lever is rigidly attached to the control cavity. A hole in the rocking bar for setting of a rocking bar attachment axis with the piston stock is made in the form of a slot.EFFECT: reduction of weight and overall dimensions of a drive of AV carrying control plane at its performance of longitudinal and rotational movements.2 dwg
申请公布号 RU2503919(C1) 申请公布日期 2014.01.10
申请号 RU20120143219 申请日期 2012.10.09
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO "VOENNO-PROMYSHLENNAJA KORPORATSIJA "NAUCHNO-PROIZVODSTVENNOE OB"EDINENIE MASHINOSTROENIJA" 发明人 MIKHEEV SERGEJ GRIGOR'EVICH;BELJUSTIN LEV VLADIMIROVICH;MARTSUN JURIJ VIKTOROVICH
分类号 F42B10/14;B64C13/28;F42B10/64 主分类号 F42B10/14
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