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    • 1. 发明专利
    • Missile launching machine
    • 发射机
    • JP2003056997A
    • 2003-02-26
    • JP2001241658
    • 2001-08-09
    • Komatsu Ltd株式会社小松製作所
    • OUCHI MINORU
    • F41A23/34F41A23/42F41G1/00F41H5/013
    • F41A23/42F41A23/20F41A23/34
    • PROBLEM TO BE SOLVED: To obtain a missile launching machine in which a missile can be launched at a low launching angle and can be searched or observed from a high position ensuring an excellent visibility. SOLUTION: In a missile launching machine where a missile case 16 is fixed to a machine base 15 such that elevation/lowering and launching angle can be adjusted freely and a sighting unit 17 is fixed to the missile case 16 such that elevation/lowering and the angle can be adjusted freely, a missile can be launched while locating the missile case 16 at an upper position of a crew seat 13 when it is mounted on a vehicle 10 and thereby a missile can be launched at a low launching angle. Furthermore, the missile can be searched or visually confirmed from a high position ensuring an excellent visibility because the sighting unit 17 can be moved upward with respect to the missile case 16.
    • 要解决的问题:获得能够以低发射角度发射导弹的导弹发射机,并且可以从高位置进行搜索或观察,确保良好的可见性。 解决方案:导弹发射机将导弹箱16固定在机座15上,使仰角/下降角度能够自由调节,瞄准单元17固定在导弹箱16上,使升/降 可以自由调整角度,当将导弹箱16安装在车辆10上时将导弹箱16定位在乘员座椅13的上部位置时可以发射导弹,从而可以以低发射角度发射导弹。 此外,由于可以使瞄准单元17相对于导弹箱16向上移动,所以可以从高位置搜索或视觉确认导弹,从而确保良好的可视性。
    • 6. 发明专利
    • LAUNCHER FOR FLYING OBJECT
    • JPH0355497A
    • 1991-03-11
    • JP19114089
    • 1989-07-24
    • JAPAN TECH RES & DEV INSTNISSAN MOTOR
    • TANAKA KAZUOTAKAMIYA TOSHIO
    • F41A23/34F41F3/04F41G5/14
    • PURPOSE:To prevent the vibration of a feed-back system accompanying a pitching phenomenon of a vehicle by allowing the launcher to compare a target inclination with the output of an inclination sensor to restrain and hold the launcher at a target inclination position at the time when the inclination of the launcher reaches the inclination of the target. CONSTITUTION:Since the inclination of a launcher 3 is detected by an inclination sensor 3, an opening instruction operation processing part 17 in accordance with the deviation of both is allowed to instruct to a proportional control valve 13 until the output of the inclination sensor 6 coincides with a target point and the launcher 3 continues to incline and move. When the launcher 3 reaches just before the inclination of the target point, a movement speed of the launcher 3 is decelerated to reach the target inclination position at a low speed. When the inclination of the ejector 3 is in the allowable range, the operation processing part 7 judges that the inclination coincides with the target point, and the opening of the proportional control valve 13 is instructed to be zero regardless of the deviation from a comparison to be zero regardless of the deviation from a comparison part 16. As the result since the inflow and outflow of oil pressure of a hydraulic cylinder 10 the launcher 3 is restrained and held in an inclination position within a previous allowable range.