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公开(公告)号：US20180281949A1
公开(公告)日：2018-10-04
申请号：US15758888
申请日：2016-09-08
Applicant: Altus Ip Limited
Inventor： Shaun Gordon MITCHELL
Abstract: A rotor assembly for a multirotor aircraft, and a multirotor aircraft, are disclosed herein. The rotor assembly has a first motor having a first axis of rotation and a first propeller connected to the first motor. The rotor assembly has a second motor having a second axis of rotation, and a second propeller connected to the second motor. The second propeller is smaller in length than the first propeller. The first motor and the first propeller produce a greater proportion of a total lift thrust of the rotor assembly than the second motor and the second propeller. The multirotor aircraft includes an airframe and a plurality of the rotor assemblies mounted to the airframe.
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公开(公告)号：US20170066537A1
公开(公告)日：2017-03-09
申请号：US14847332
申请日：2015-09-08
Applicant: Altus IP Limited
Inventor： Shaun Gordon MITCHELL , Ryan Harley CADWALLADER
CPC classification number: B64D17/80 , B64C39/024 , B64C2201/027 , B64C2201/108 , B64C2201/185 , B64D17/72
Abstract: A parachute deployment apparatus for use with an aircraft, including a deployment body with an internal cavity, the deployment body configured to house a parachute to be deployed through an upper opening of the internal cavity, a firing mechanism configured to release a pressurized gas into the internal cavity of the deployment body, wherein the apparatus includes a cap that engages with the upper opening to close it prior to deployment and is configured to be projected from the upper opening upon release of the pressurized gas into the internal cavity of the deployment body, and wherein the cap is connected to the parachute.
Abstract translation: 一种与飞行器一起使用的降落伞展开装置，包括具有内部空腔的展开体，所述展开体构造成容纳通过所述内部空腔的上部开口展开的降落伞;构造成将加压气体释放到 所述设备包括盖子，所述盖子与所述上部开口接合，以在展开之前将其封闭，并且构造成在将所述加压气体释放到所述展开体的内部空腔中时从所述上部开口突出， 并且其中所述盖连接到所述降落伞。
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