高温空气下C/SiC复合材料力学性能测试

测试了C/SiC复合材料在高温空气下的压缩、弯曲和拉伸性能,利用扫描电子显微镜分析复合材料在室温与高温条件下的断口微观形貌。结果表明:从室温升温到1 000 ℃测试温度时,C/SiC复合材料的压缩强度由247 MPa降低至78 MPa,性能降低68%;弯曲强度由480 MPa降低至277 MPa,性能降低42%;拉伸强度由247 MPa降低至152 MPa,性能降低38%。高温氧化导致界面退化,损伤材料基体与碳纤维结构,加剧了纤维断裂程度,改变了纤维与基体的结合状态,纤维增韧机制逐渐消失,导致复合材料性能下降。     

大深度复合同振式矢量水听器设计

针对目前深海无人移动平台缺乏与其工作深度相匹配的复合同振式矢量水听器的问题,采用薄壁铝合金球壳作为矢量通道,压电陶瓷圆环作为声压通道,设计制作了一型大深度复合同振式矢量水听器,并用理论计算、有限元仿真和实验测试的方法对其声学性能和耐压性能进行了验证。该水听器的外径为85 mm,质量为398 g,平均密度为1 240 kg/m~3,工作频段为20～3 000 Hz,矢量通道呈余弦指向性,灵敏度为-187 dB@500 Hz,声压通道无指向性,灵敏度为-191 dB@500 Hz,耐压深度为2 000 m。海上试验表明,该水听器能够搭载在水下滑翔机等深海无人平台上执行声学探测任务,在大深度声学探测领域具有重大的应用价值。     

Consumer drone evolutions: trends,spaces, temporalities,threats

ABSTRACT

While the drone has become synonymous with the War on Terror, the asymmetric iconography of the battlefield is shifting. Commercially available off-the-shelf (COTS) drones are increasingly prevalent features of global battlefields, employed by non-state actors in both visualising such spaces, and the directing and inflicting of harm. As such usage increases, so too do concerns around their evolving adoption, adaptation, and potential portability into homeland spheres. While cognizant of the range of positive drone applications, it is asserted that drones nonetheless remain simultaneously bound to an inverse potential for exploitation. In examining drone risk, this article approaches the consumer drone through a series of sites and spaces through which it is technically and socially constructed. Reflecting upon industry innovation, community-driven experimentation, and evolving airspace – it calls for greater attention to the drone’s malleability, arguing that understandings of COTS drones must remain attentive to both drone potential and potential drone threat.     

基于部件模型的无人机系统小样本车辆目标识别方法

对地目标检测与识别是无人机系统典型任务之一,但受限于任务特殊性,往往难以获取足够的目标样本数据以实现高可靠的目标识别.为此,结合人的认知特性,提出一种基于部件模型的小样本车辆目标识别方法,可有效提高无人机感知能力.采用视觉显著性检测与物体性检测相结合的检测方法,提取目标可能区域;采用基于图论的GrabCut方法与最大类...     

高超声速滑翔再入飞行器的可达区快速预测

防御方对来袭滑翔再入飞行器进行可达区的预测存在先验信息量不足且时效性要求高等难题.为此提出一种基于最优化飞行假设的可达区快速预测方法:仅需已知目标当前位置、速度与最大升阻比(可基于雷达探测数据通过实时弹道估计获得),基于平衡滑翔假设和最大横程的埃格斯解分别获得目标最大纵程和横程终点坐标,在经纬度二维平面内,可达区即可近...