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AIRCRAFT-MISSILE STRIKE SYSTEM

机译:飞机打击系统

摘要

FIELD: aviation.;SUBSTANCE: invention relates to military modular hardware. Air-rocket strike system (ARSS) with an unmanned aerial vehicle (UAV) having a fuselage with a weapon system on launching devices (LD), a wing with control elements, a power plant engine (PPE), on-board control system (OCS), which provides telemechanical control from command station (CS) of carrier vehicle. ARSS includes optionally and remotely piloted aircraft-helicopters having asymmetric sweep wings (ASW), two-bladed rotors (TBR) and in the stern nacelle combined engine with free power turbines, leading two longitudinal TBR and/or in the annular fairing remote fan, directed backward with working/autorotating TBR or mirror-fixed skewed blades-wings (SBW) corresponding to the ASW in the configuration of ship jet-wing/gyroplane or aircraft with tandem wings of X-like sweep and controlled missiles.;EFFECT: increased weight and combat load, increased speed and range of flight, increased probability of destruction of surface, underwater and air targets located at long range, and possibility of its attack after prolonged flight in hang-up mode, return to ANC helicopter pad for repeated use.;5 cl, 1 tbl, 3 dwg
机译:技术领域本发明涉及军事模块化硬件。带有无人飞行器(UAV)的空袭系统(ARSS),其机身带有发射装置(LD)上的武器系统,带有控制元件的机翼,发电厂发动机(PPE),机载控制系统( OCS),可从运载工具的指挥站(CS)提供远程机械控制。 ARSS包括具有非对称后掠翼(ASW),两叶旋翼(TBR)的可选和远程驾驶飞机直升机,并在船尾机舱中配有自由动力涡轮机,引导两个纵向TBR和/或在环形整流罩远程风扇中,使用工作/自动旋转的TBR或与ASW相对应的镜面固定的偏斜叶片-机翼(SBW)向后定向,这是在喷射喷气机/旋翼飞机或带有X形纵掠和控制导弹的串联机翼的飞机上进行的;效果:增加重量和战斗力,增加的速度和飞行距离,在远距离处破坏水面,水下和空中目标的可能性增加,以及在挂机模式下长时间飞行后受到攻击的可能性,请返回ANC直升机停机坪重复使用。; 5厘升,1汤匙,3载重吨

著录项

  • 公开/公告号RU2721803C1

    专利类型

  • 公开/公告日2020-05-22

    原文格式PDF

  • 申请/专利权人 DUROV DMITRIJ SERGEEVICH;

    申请/专利号RU20190117416

  • 发明设计人 DUROV DMITRIJ SERGEEVICH (RU);

    申请日2019-06-04

  • 分类号B64C37;B64C27/22;B64C27;B64C39/02;

  • 国家 RU

  • 入库时间 2022-08-21 11:02:30

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