首页> 外国专利> METHOD TO TEST A DEVELOPED TORQUE OF AN ELECTRO-PNEUMATIC STEERING GEAR OF GUIDED MISSILES AND PROJECTILES

METHOD TO TEST A DEVELOPED TORQUE OF AN ELECTRO-PNEUMATIC STEERING GEAR OF GUIDED MISSILES AND PROJECTILES

机译:测试制导导弹和弹丸的电动气动转向装置扭矩的方法

摘要

FIELD: defense engineering; production of guided missiles and projectiles.;SUBSTANCE: the invention is pertinent to the field of defense engineering, in particular, to production of guided missiles and projectiles. The technical result of the invention is simplification of testing, increased accuracy, decreased labor input and cost of the testing. The method of testing of a developed torque of an electro-pneumatic steering gear of guided missiles and projectiles is based on a torque measurement of the steering gear with the help of a reference load and an easily removable balance lever put on a rudder. Then the steering gear with a detector of the rudders motion are installed on a customizing table. The detector of the rudders motion is made in the form of a separate contact or non-contact sensor or for the purpose they use an available in the steering gear as a feedback gauge - the gauge of a piston linear motion or a gauge of angular motion of rudders. The rudders turning at a maximum angle in one side is made using application of a torque of the corresponding sign by a reference load with the weight on a definite length of an arm of a placement of the load on the lever in respect to the axis of rotation of the rudders equal to a developed torque of the steering gear at the given pressure of the feeding. Switch on the power of the gauge, measure the voltage on the gauge output by a voltmeter, remove a torque by removal of the reference load, turn the rudders at a maximum angle in other side using application of a torque of an opposite sign equal to a maximum torque of a hinged load on the rudders in respect to the rudders turning angle and an angle of attack of a missile or a projectile. Switch on power supply of the booster of the steering gear and feed onto an input of the steering gear compressed air under pressure of P =1.5Pgvn., feed onto the input of the steering gear a maximum control signal of management corresponding to the motion of the rudders at a maximum angle, measure the voltage on the output of the gauge, which should meet the first given ratio. By a smooth reduction of pressure of the feeding in the pneumo-circuit) of the steering gear and according to reduction of voltage on the output of the gauge determine pressureP+1at which the voltage will meet the second given ratio. At that the pressure P+1should be no more than Pgvn ,remove a pneumatic feeding and the power supply of the booster of the steering gear and switch off the control signal and the power of the gauge. After that using an analogous method they measure voltages and determine the pressure at application of the corresponding torques and a control signal of an opposite sign and determine a developed torque of the steering gear according to the mathematical formula.;EFFECT: the invention ensures simplification of testing, increased accuracy, decreased labor input and cost of the testing.;5 cl, 1 dwg
机译:领域:国防工程;物质:本发明与国防工程领域有关,特别是与制导导弹和射弹有关。本发明的技术结果是简化了测试,提高了准确性,减少了人工投入并降低了测试成本。测试制导导弹和弹丸的电动气动操舵装置产生的扭矩的方法是基于借助参考负载和方向舵上易于拆卸的平衡杆对操舵装置的扭矩进行测量的。然后将带有方向舵运动检测器的转向器安装在定制台上。方向舵运动检测器以单独的接触式或非接触式传感器的形式制成,或者为此目的,它们将转向器中可用的传感器用作反馈量规-活塞线性运动量规或角运动量规舵。方向舵在一侧以最大角度转动是通过参考负载施加相应符号的扭矩并在臂的一定长度上施加一定重量的重量来实现的。在给定的进给压力下,方向舵的旋转等于操舵装置产生的扭矩。接通仪表的电源,通过电压表测量仪表输出上的电压,通过去除参考负载来消除扭矩,使用等号相反的扭矩将方向舵转向另一侧的最大角度相对于舵的转向角和导弹或弹丸的攻角,舵上的铰链负载的最大扭矩。接通转向器助力器的电源,并在P = 1.5P gvn的压力下将其输入到转向器的压缩空气中。,将最大控制值输入到转向器的输入中对应于最大角度方向舵运动的管理信号,测量仪表输出端的电压,该电压应满足第一个给定的比率。通过平稳地减小转向装置的气动回路中的供给压力,并根据仪表输出端的电压降低,确定压力P + 1,在该压力下P + 1将满足第二给定比率。此时压力P + 1不应大于P ,取消气动供给和转向器助力器的电源,并关闭控制信号和仪表的电源。此后,他们使用类似的方法测量电压,并在施加相应扭矩和相反符号的控制信号时确定压力,并根据数学公式确定转向器产生的扭矩。效果:本发明确保简化了测试,提高准确性,减少人工投入和测试成本。; 5 cl,1 dwg

著录项

  • 公开/公告号RU2249173C1

    专利类型

  • 公开/公告日2005-03-27

    原文格式PDF

  • 申请/专利权人

    申请/专利号RU20030121676

  • 发明设计人 FIMUSHKIN V.S.;TOSHNOV F.F.;GUSEV A.V.;

    申请日2003-07-14

  • 分类号F42B10/60;F42B15/01;B64C13/36;

  • 国家 RU

  • 入库时间 2022-08-21 22:02:08

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号