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    • 1. 发明申请
    • AERODYNAMIC TOTE PACKAGE
    • 气动TOTE包
    • WO2017066748A1
    • 2017-04-20
    • PCT/US2016/057315
    • 2016-10-17
    • X DEVELOPMENT LLC
    • SOPPER, ClarkDAY, MattWOODWORTH, AdamCOHEN, Joanna
    • B65D5/18B65D5/36B65D5/42B65D5/468
    • B64D1/08B64C39/024B64C2201/128B65D5/18B65D5/2033B65D5/241B65D5/4208B65D5/4266B65D5/4608B65D81/00
    • An example tote package is disclosed for carrying a load external to a UAV. The tote package may be generated by folding a sheet of material. The sheet may include a middle section, a first side section, and a second side section. When the sheet is folded, the middle section may create a bottom portion of the tote package. Additionally, the first side section may create a first side portion tapering up from the edge of the bottom portion to the middle of the top portion of the tote package. Furthermore, the second side section may create a second side portion tapering up from the opposite edge to the middle of the top portion. At the top portion, the first and second sections may connect to create a handle. The first side, second side, and middle sections may be folded to create front and back portions of the tote package.
    • 公开了用于在无人飞行器外部承载负载的示例性手提包(tote package)。 手提包可以通过折叠一张材料来生成。 片材可以包括中间部分,第一侧部分和第二侧部分。 当折叠片材时,中间部分可以形成手提包的底部。 此外,第一侧面部分可以形成从底部部分的边缘逐渐变细到手提包的顶部中间的第一侧面部分。 此外,第二侧面部分可以形成第二侧面部分,该第二侧面部分从顶部的相对边缘向中间渐缩。 在顶部,第一和第二部分可连接以创建手柄。 第一面,第二面和中间部分可以折叠以形成手提包的正面和背面部分。
    • 2. 发明申请
    • PAYLOAD DELIVERY SYSTEM
    • 有效载荷传递系统
    • WO2017204892A1
    • 2017-11-30
    • PCT/US2017/023886
    • 2017-03-23
    • X DEVELOPMENT LLC
    • SOPPER, ClarkPRAGER, André
    • B64D1/22B64C39/02
    • B64D1/22B64C39/024B64C2201/128B66D5/026
    • Described herein are apparatuses that provided various features related to unmanned aerial vehicles. An example apparatus may include, (i) a support structure, (ii) at least one shaft coupled to the support structure via at least one swing arm, wherein the swing arm allows upward movement, and restricts downward movement of, the at least one shaft from a resting position, (iii) a spool, wherein in the spool is shaped so as to rest on the at least one shaft when the at least one shaft is in the resting position, and wherein the spool is operable to unwind a tether coupled to a payload, and (iv) at least one fan coupled to the at least one shaft, wherein rotation of the spool when unwinding the tether also causes rotation of the at least one fan coupled to the at least one shaft, thereby controlling a descent rate of the payload.
    • 这里描述的是提供与无人驾驶飞行器相关的各种特征的装置。 示例装置可以包括(i)支撑结构,(ii)经由至少一个摆臂耦合到支撑结构的至少一个轴,其中摆臂允许向上运动并限制至少一个 (iii)线轴,其中在所述线轴中,当所述至少一个轴处于所述静止位置时,所述线轴成形为搁置在所述至少一个轴上,并且其中所述线轴可操作以展开系绳 (iv)耦合到所述至少一个轴的至少一个风扇,其中当展开所述系绳时所述卷轴的旋转还导致耦合到所述至少一个轴的所述至少一个风扇的旋转,从而控制 有效载荷的下降率。