Flying vehicle systems and methods

US12030668B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-12030668-B2
Application numberUS-202117223589-A
CountryUS
Kind codeB2
Filing dateApr 6, 2021
Priority dateApr 6, 2020
Publication dateJul 9, 2024
Grant dateJul 9, 2024

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

An unmanned aerial vehicle according to certain embodiments generally includes a chassis, a control system, and at least one rotor. The chassis includes a first battery compartment configured to receive sliding insertion of a first battery, and a second battery compartment configured to receive sliding insertion of a second battery. The control system is operable to receive power from the first battery and the second battery when the first battery is received in the first battery compartment and the second battery is received in the second battery compartment. The at least one rotor is operable to generate lift under control of the control system when both the first battery and the second battery are installed to the chassis. The control system is configured to remain at least partially active under power supplied by the first battery when the second battery is removed from the second battery compartment.

First claim

Opening claim text (preview).

What is claimed is: 1. An unmanned aerial vehicle, comprising: a chassis comprising: a first battery compartment configured to receive sliding insertion of a first battery; and a second battery compartment configured to receive sliding insertion of a second battery; a control system operable to receive power from the first battery and the second battery when the first battery is received in the first battery compartment and the second battery is received in the second battery compartment; at least one rotor operable to generate lift under control of the control system when both the first battery and the second battery are installed to the chassis; and a latch mechanism operable to selectively limit movement of the first battery along a first insertion/removal axis, the latch mechanism comprising: a first component comprising a first channel; and a second component comprising a spline configured for insertion in the first channel; wherein the control system is configured to remain at least partially active under power supplied by the first battery when the second battery is removed from the second battery compartment; wherein one of the first component or the second component is a movable component and further comprises a flange; wherein the latch mechanism has a closed state in which the movable component is in a first rotational position, the spline is received in the first channel, and the flange prevents removal of the first battery from the first battery compartment; and wherein the latch mechanism has an open state in which the movable component is in a second rotational position, the spline is removed from the first channel, and the flange does not prevent removal of the first battery from the first battery compartment. 2. The unmanned aerial vehicle of claim 1 , wherein engagement between the first channel and the spline prevents rotation of the movable component from the first rotational position to the second rotational position when the spline is received in the first channel. 3. The unmanned aerial vehicle of claim 2 , wherein the movable component is rotatable between the first rotational position and the second rotational position upon lifting of the movable component in a vertical direction to remove the spline from the first channel. 4. The unmanned aerial vehicle of claim 1 , wherein the first component further comprises a second channel; and wherein with the latch mechanism in the open state, the spline is received in the second channel. 5. The unmanned aerial vehicle of claim 4 , wherein engagement between the second channel and the spline prevents rotation of the movable component from the second rotational position to the first rotational position when the spline is received in the second channel. 6. The unmanned aerial vehicle of claim 1 , wherein the movable component further comprises a knob configured to facilitate movement of the movable component.

Assignees

Inventors

Classifications

  • Information or communication technologies improving the operation of electric vehicles · CPC title

  • Plug-in electric vehicles · CPC title

  • Electric charging stations · CPC title

  • Electric energy management in electromobility · CPC title

  • Hoisting, lifting, hauling or pushing, not otherwise provided for · CPC title

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What does patent US12030668B2 cover?
An unmanned aerial vehicle according to certain embodiments generally includes a chassis, a control system, and at least one rotor. The chassis includes a first battery compartment configured to receive sliding insertion of a first battery, and a second battery compartment configured to receive sliding insertion of a second battery. The control system is operable to receive power from the first…
Who is the assignee on this patent?
Workhorse Group Inc
What technology area does this patent fall under?
Primary CPC classification B64F1/364. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Jul 09 2024 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 12 related publications on this page (citations in our corpus or others sharing the same primary CPC).