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AERIAL VEHICLE WITH DEPLOYABLE COMPONENTS

机译：具有可配置组件的航空车辆

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摘要

An unmanned aerial vehicle with deployable components (UAVDC) is disclosed. The UAVDC may comprise a fuselage, at least one wing, and at least one control surface. In some embodiments, the UAVDC may further comprise a propulsion means and/or a modular payload. The UAVDC may be configured in a plurality of arrangements. For example, in a compact arrangement, the UAVDC may comprise the at least one wing stowed against the fuselage and the at least one control surface stowed against the fuselage. In a deployed arrangement, the UAVDC may comprise the at least one wing deployed from the fuselage and the least one control surface deployed from the fuselage. In an expanded arrangement, the UAVDC may comprise the at least one wing telescoped to increase a wingspan of the deployed arrangement.

机译：公开了一种具有可展开部件的无人机（UAVDC）。 UAVDC可包括机身，至少一个机翼和至少一个控制表面。在一些实施例中，UAVDC可以进一步包括推进装置和/或模块化有效载荷。 UAVDC可以以多种布置来配置。例如，在紧凑的布置中，UAVDC可以包括至少一个机翼被收纳在机身上，以及至少一个控制面被收纳在机身上。在展开的布置中，UAVDC可包括从机身展开的至少一个机翼和从机身展开的至少一个控制面。在扩展的布置中，UAVDC可以包括至少一个被伸缩以增加展开布置的翼展的机翼。

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公开/公告号US2020102065A1

专利类型
公开/公告日2020-04-02

原文格式PDF
申请/专利权人 AREA-I INC.;
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申请/专利号US201916700436
发明设计人 NICHOLAS ROBERT ALLEY;JOSHUA LEMMING STEELE;JESSE OWEN WILLIAMS;DANIEL KUEHME;JONATHAN CALEB PHILLIPS;
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申请日2019-12-02
分类号B64C3/40;B64C1/36;B64C11/28;B64C5/12;B64C5/16;B64C3/54;B64C13/24;B64C39/02;B64C3/56;B64C13/30;B64C5/02;
国家 US
入库时间 2022-08-21 11:20:37

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