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Method and apparatus for launching unmanned aircraft, including the releasable fastening of the aircraft during launch and braking of the rear clamping movement

机译:用于发射无人飞机的方法和设备,包括在发射和制动后夹紧运动期间可释放地固定飞机

摘要

Apparatus for unmanned aircraft carrying a (150) comprising: a support (141), a ready release trolley (120) movably in the carrier (141); It comprising: a clip (180) movably coupled to the launching trolley (120) including the clip (180) at least unaparte clamping positioned to engage releasably the fuselage (151) of the plane (150) way, pudiéndosemover the clamp (180) relative to the launch carriage (120) between a first position with at least unaparte of positioned subject to abut with the fuselage (151) and a second position with by atleast a holding portion positioned to I remain without contact with the fuselage (151), characterized hechode comprising a brake (690) positioned at least close to the gripper (180) can change the brake (690) of a first configuration in which the brake ( 690) prevents a first amount of movement of the gripper (180), and a second configuration in which the brake (690) does not prevent the movement of the gripper (180) for I alcarro release (120), or prevents a second amount motion of p inza (180) less than the primeracantidad.
机译:用于携带(150)的无人飞行器的设备,包括:支撑件(141),可移动地在载体(141)中的准备释放小车(120);它包括:夹子(180),其可移动地耦合到发射台车(120),包括夹子(180),该夹子(180)至少无段地定位成可释放地接合飞机(150)的机身(151),在夹子(180)上固定相对于发射架(120),在第一位置和第二位置之间,第一位置至少与主体(151)相邻,第二位置至少保持与机身(151)不接触,包括至少定位在夹持器(180)附近的制动器(690)的特征性的舱罩可以改变第一构造的制动器(690),其中制动器(690)阻止夹持器(180)的第一运动。第二种构造,其中制动器(690)不会阻止抓爪(180)的运动以释放Alcarro(120),也不会阻止P inza(180)的第二次运动小于引物。

著录项

  • 公开/公告号ES2390056T3

    专利类型

  • 公开/公告日2012-11-06

    原文格式PDF

  • 申请/专利权人 THE INSITU GROUP;

    申请/专利号ES20040821333T

  • 申请日2004-03-25

  • 分类号B64F1/06;B64C3/56;B64C39/02;

  • 国家 ES

  • 入库时间 2022-08-21 17:21:00

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