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AIRCRAFT CARRIER AIRCRAFT TAKEOFF CATAPULT EQUIPMENT

机译:航空母舰航空器起飞直升机装备

摘要

Aircraft carrier aircraft takeoff catapult equipment, comprising a flight deck (18) having a gap (19), front and rear pulleys (20 and 23), and steel cables (36) wrapped around the pulleys. A connector block (45) connects both ends of the steel cables together. A block base (47) is provided on the connector block. A takeoff driving motor (25) can directly drive a pullable swinging arm (7) on the nose gear of an aircraft via the rear pully, the steel cables, and the block base (47) on the connector block or drive an aircraft to run and take off via a reciprocating shuttle. Because the friction between the pulleys and the steel cables can be increased by providing multiple steel cables and increasing the force of a tightening mechanism, this aircraft catapult equipment can easily achieve the driving force required by the aircraft to take off; moreover, the overall structure of the equipment is simplified, is also easy to process and manufacture, and is very suitable for use in catapulting a heavy aircraft taking off from an aircraft carrier. The equipment also is suitable for being miniaturized for installation on a ship or vehicle, specialized in catapulting the takeoff of a small-sized unmanned aerial vehicle.
机译:航空母舰起飞弹射器设备,包括具有间隙(19)的驾驶舱(18),前后滑轮(20和23)以及缠绕在滑轮上的钢缆(36)。连接器块(45)将钢缆的两端连接在一起。在连接器块上设有块座(47)。起飞驱动马达(25)可以通过连接器滑轮组上的后皮带轮,钢缆和滑轮组底座(47)直接驱动飞机前起落架上的可拉动摇臂(7)或驱动飞机运行并通过往复穿梭飞机起飞。由于通过设置多根钢缆并增加紧固机构的力可以增加滑轮与钢缆之间的摩擦力,因此该飞机弹射器设备可以轻松实现飞机起飞所需的驱动力。此外,设备的整体结构得到简化,易于加工和制造,并且非常适合用于弹射从航空母舰上起飞的重型飞机。该设备还适合于小型化,以安装在船舶或车辆上,专门用于弹射小型无人机的起飞。

著录项

  • 公开/公告号WO2019205726A1

    专利类型

  • 公开/公告日2019-10-31

    原文格式PDF

  • 申请/专利权人 HAN PEIZHOU;

    申请/专利号WO2019CN00068

  • 发明设计人 HAN PEIZHOU;

    申请日2019-04-16

  • 分类号B64F1/06;B64F1/08;

  • 国家 WO

  • 入库时间 2022-08-21 11:52:43

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