-7 s, the energy per pulse E Rin = 1-10, and J, the frequency control range of the electromagnetic pulses repetition ΔF = 1 to 300 Hz. 1 ZP f., 4 yl."/> Of small unmanned aerial vehicles AREAS FOR MONITORING fire, acts of terrorism and technological disasters
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Of small unmanned aerial vehicles AREAS FOR MONITORING fire, acts of terrorism and technological disasters

机译:小型无人机的火灾,恐怖活动和技术灾难的监视区域

摘要

The technical result of the utility model is a spatial and temporal expansion of capabilities of monitoring by the use as a fuel air, eliminates the need to store fuel on board small-sized UAVs (MBPLA), limiting the range and flight time MBPLA. MBPLA cantilever wing 1 comprises a pulsating detonation engine 2 and the monitoring means. Monitoring tools include navigation equipment 3, finder 4, teplopelengator 5 and a camera 6, connected via the on-board computer 7 with transmission-reception antenna 8 GPRS, MPLS satellite GPS, «GLONAS" or cellular to transmit monitoring results to the central aircraft management . Cantilever wing 1 is provided with aerodynamic controls 8 in height and 10 in the direction of flight MBPLA. Pulsed detonation engine 2 comprises an air intake 11, a combustion chamber 12, the nozzle 13 and the means of energy supply. Said power supply means comprise series connected MHD generator 14, electric energy storage device 15 one electrical output is connected to the feed inlet of the electric discharger 16, and the second - after pumping modulator 17 to the microwave generator 18. The MHD generator 14 is a conduction or induction type and mounted on the nozzle 13 of the engine detonation. The nozzle 13 is in the form Lovaglio nozzle. 15 electric energy accumulator is designed as a capacitive or inductive storage. For the control of traction power detonation engine 2 of its microwave generator 18 is driven by a pulse and the pulse repetition frequency. To reduce the energy consumption for the excitation of the detonation of the exothermic reaction in the combustion chamber 12 and protect the latter from overheating, it is configured with the following parameters: the wavelength of electromagnetic radiation λ = 0.5 or 1.2 cm, the duration of the microwave pulse τ≤10 -7 s, the energy per pulse E Rin = 1-10, and J, the frequency control range of the electromagnetic pulses repetition ΔF = 1 to 300 Hz. 1 ZP f., 4 yl.
机译:本实用新型的技术结果是通过用作燃料空气来进行监视能力的时空扩展,消除了将燃料存储在小型无人机上的需求,从而限制了飞行时间和飞行时间。 MBPLA悬臂翼1包括脉动爆震发动机2和监测装置。监控工具包括导航设备3,取景器4,teplopelengengator 5和摄像机6,通过车载计算机7与收发天线8 GPRS,MPLS卫星GPS,“ GLONAS”或蜂窝式连接,以将监控结果传输到中央飞机悬臂翼1在高度上具有气动控制装置8,在MBPLA的飞行方向上具有控制装置10.脉冲爆震发动机2包括进气口11,燃烧室12,喷嘴13和能量供应装置。该装置包括串联的MHD发生器14,电能存储装置15,一个电输出端连接到放电器16的进料口,第二个输出端-将调制器17泵送到微波发生器18之后。MHD发生器14是传导或感应式,安装在发动机爆震的喷嘴13上,喷嘴13为Lovaglio喷嘴形式; 15蓄能器设计为电容式或感应存储。为了控制牵引力,其微波发生器18的爆震发动机2由脉冲和脉冲重复频率驱动。为了减少激发燃烧室12中的放热反应的爆炸所消耗的能量并保护燃烧室12免受过热,其配置有以下参数:电磁辐射的波长λ= 0.5或1.2 cm,持续时间为微波脉冲τ≤10 -7 s,每脉冲能量E Rin = 1-10, J,频率控制范围电磁脉冲重复ΔF= 1至300 Hz。 1 ZP f。,4 yl。

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