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 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|