Reconfigurable battery-operated vehicle system

Abstract

A quadrotor UAV including ruggedized, integral-battery, load-bearing body, two arms on the load-bearing body, each arm having two rotors, a control module mounted on the load-bearing body, a payload module mounted on the control module, and skids configured as landing gear. The two arms are replaceable with arms having wheels for ground vehicle use, with arms having floats and props for water-surface use, and with arms having pitch-controlled props for underwater use. The control module is configured to operate as an unmanned aerial vehicle, an unmanned ground vehicle, an unmanned (water) surface vehicle, and an unmanned underwater vehicle, depending on the type of arms that are attached.

Description

[0001]This application is a Continuation application of International PCT Application No. PCT / US2011 / 000953, filed May 26, 2011, which claims the benefit of U.S. provisional Application No. 61 / 396,459, filed May 26, 2010, and U.S. provisional Application No. 61 / 399,168, filed Jul. 7, 2010, each of which are incorporated herein by reference for all purposes.[0002]The present invention relates generally to an unmanned, battery-operated vehicle (e.g., a UAV) and, more particularly, to a battery-operated vehicle that can be reconfigured for a wide variety of purposes.BACKGROUND OF THE INVENTION[0003]Quadrotor UAVs (unmanned aerial vehicles) are typically characterized by a center body having four arms coming out laterally in an X configuration (when viewed from above). Each arm supports one helicopter-type rotor directed upward. Typical control for a quadrotor aircraft is accomplished by varying the speed of each rotor, which typically is counter-rotating with respect to the rotors on e...

AI Technical Summary

Benefits of technology

The present invention provides a battery-operable vehicle system that can be safely transported without damaging the battery. The battery module acts as the primary structural member of the vehicle, carrying the loads between the propulsion modules and supporting the control module and payload. The vehicle forms a quadrotor aircraft with four angled propellers that allow for maxed-up backward viewing and minimized air resistance during cruise flight. The arms connect to the battery module on opposite ends of the vehicle body, with each arm connector bearing all vertical loads from the battery unit without the need for a heavy end cap. This results in a more reliable and lightweight structure.

Problems solved by technology

Due to the risks in shipping lithium batteries, there are strict Department of Transportation requirements on shipping containers for lithium batteries and battery packs (i.e., groups of interconnected batteries).

Once the shipping is completed and the batteries are disseminated to end users, the batteries and / or battery packs may lose the protection of the robust packing container, and be subject to damage until they are installed into their respective vehicles.

Thus, the provision of batteries is susceptible to damage, and meeting shipping requirements can be challenging when a wide array of battery types must be shipped.

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