首页> 外国专利> DEVICE FOR THE GLIDING PARACHUTE AERODYNAMIC CHARACTERISTICS MEASURING IN WIND TUNNEL, GLIDING PARACHUTE MODEL FOR TESTS IN WIND TUNNEL, METHOD OF GLIDING PARACHUTE AERODYNAMIC CHARACTERISTICS MEASURING IN WIND TUNNEL

DEVICE FOR THE GLIDING PARACHUTE AERODYNAMIC CHARACTERISTICS MEASURING IN WIND TUNNEL, GLIDING PARACHUTE MODEL FOR TESTS IN WIND TUNNEL, METHOD OF GLIDING PARACHUTE AERODYNAMIC CHARACTERISTICS MEASURING IN WIND TUNNEL

机译:风洞中滑翔伞气动特性的测量装置,风洞中滑翔伞模型的测试,风洞中滑翔伞气动特性的测量方法

摘要

FIELD: aviation.;SUBSTANCE: invention relates to aviation equipment and designed to measure the aerodynamic forces and moments acting on the gliding parachute (GP) dome in the wind tunnel flow (WT) at various angles of attack and slip. Device is used as follows. After entering to the flow parachute model is fixed in the WT flow in the balancing position using the proposed device. Fixation quality is monitored by the strain-gage scales measurement readings and video filming processing data and, if necessary, is corrected. Parachute model movement in the flow and the steering lines lifting are performed by means of remotely controlled drives. During the tests, simultaneously with the aerodynamic loads measurement using the strain-gage scales, the parachute model video shooting is carried out with the help of located in the WT working part video cameras, which number is chosen so that each placed on the model surface marker can be seen from at least two cameras. At the end of the test program, the aerodynamic loads onto parachute measurements are correlated with its flow actual conditions (angles of attack and slip) obtained by the video data processing.;EFFECT: technical result consists in reducing the experiment preparation and performance time, reducing errors in determining of the parachute aerodynamic characteristics, providing the possibility of carrying out tests of GP of various sizes, and also at the steering lines different positions, changing it during the experiment without the WT stopping.;8 cl, 4 dwg
机译:技术领域本发明涉及航空设备,并且被设计成以各种迎角和滑移角测量作用在风洞流(WT)中的滑翔降落伞(GP)圆顶上的空气动力和力矩。设备的用法如下。进入流程后,降落伞模型使用所提出的装置固定在WT流中的平衡位置。固定质量由应变计测量读数和视频胶片处理数据监控,并在必要时进行校正。降落伞模型在水流中的运动和转向线的提升是通过遥控驱动器执行的。在测试过程中,与使用应变计测量空气动力学负载的同时,借助位于WT工作部件摄像机中的降落伞模型视频进行拍摄,该摄像机的编号被选择为每个都放置在模型表面上至少可以从两台摄像机看到标记。在测试程序的最后,降落伞测量的空气动力学负载与通过视频数据处理获得的流量实际条件(攻角和滑移角)相关。效果:技术成果在于减少了实验准备和执行时间,减少降落伞空气动力学特性确定过程中的误差,从而提供了进行各种尺寸GP以及在转向线不同位置进行测试的可能性,从而在实验过程中无需停止WT即可对其进行更改; 8 cl,4 dwg

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