Flying body

US12006049B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-12006049-B2
Application numberUS-202017757439-A
CountryUS
Kind codeB2
Filing dateNov 19, 2020
Priority dateDec 25, 2019
Publication dateJun 11, 2024
Grant dateJun 11, 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.

Flying body including body portion and a plurality of propellers radially disposed to be laterally symmetrical from body portion is provided with: a plurality of motors respectively rotating the plurality of propellers; a plurality of power storage packs respectively supplying currents to the plurality of motors; and sub power storage pack connected to the plurality of power storage packs by power wirings, respectively. The same number of motors of the plurality of motors are installed on each of the left and right sides, and the same number of power storage packs of the plurality of power storage packs are installed on each of the left and right sides. Sub power storage pack is installed on a lateral center line of body portion.

First claim

Opening claim text (preview).

The invention claimed is: 1. A flying body comprising: a body portion; a plurality of propellers which are radially disposed and are laterally symmetrical from the body portion; a plurality of motors, each of which rotates a respective one of the plurality of propellers; a plurality of power storage packs, each of which supplies currents to a respective one of the plurality of motors, respectively; a sub power storage pack connected to each of the plurality of power storage packs by a respective one of power wirings, a plurality of switches disposed between the plurality of power storage packs and the sub power storage pack, respectively; and a power supply control unit that includes a microcomputer and controls the plurality of switches, wherein: the sub power storage pack is installed on a lateral center line of the body portion, and a same number of motors of the plurality of motors are installed on each of a left side and a right side of a lateral center line of the sub power storage pack, and a same number of power storage packs of the plurality of power storage packs are installed on each of the left side and the right side, and the power supply control unit specifies at least one power storage pack having a higher current value than other power storage packs, having a corresponding motor having a higher rotational speed than other motors, or having a smaller voltage value than other power storage pack, and turns on at least one of the plurality of switches corresponding to at least one power storage pack to supply an auxiliary current from the sub power storage pack to the at least one power storage pack. 2. The flying body according to claim 1 , wherein the sub power storage pack is installed at a center-of-gravity portion of the flying body. 3. The flying body according to claim 1 , wherein: the sub power storage pack is connected to each of the plurality of power storage packs by a respective one of the power wirings, and wiring resistances of the power wirings are equal between the sub power storage pack and the plurality of power storage packs. 4. The flying body according to claim 1 , wherein: the plurality of power storage packs are distributed at equal distances laterally from the lateral center line of the body portion, and the power wirings each connecting the sub power storage pack to a respective one of the plurality of power storage packs are set to have an equal length. 5. The flying body according to claim 1 , wherein the sub power storage pack includes a capacity that is smaller than capacities of the plurality of power storage packs. 6. The flying body according to claim 5 , wherein the sub power storage pack has an equal output performance to the plurality of power storage packs. 7. The flying body according to claim 1 , further comprising a DC-DC convertor disposed between the plurality of switches and the sub power storage pack.

Assignees

Inventors

Classifications

  • B64C27/10Primary

    arranged coaxially · CPC title

  • for imaging, photography or videography · CPC title

  • Arrangement of on-board electronics, e.g. avionics systems or wiring · CPC title

  • with four distinct rotor axes, e.g. quadcopters · CPC title

  • Efficient propulsion technologies, e.g. for aircraft · CPC title

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Frequently asked questions

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What does patent US12006049B2 cover?
Flying body including body portion and a plurality of propellers radially disposed to be laterally symmetrical from body portion is provided with: a plurality of motors respectively rotating the plurality of propellers; a plurality of power storage packs respectively supplying currents to the plurality of motors; and sub power storage pack connected to the plurality of power storage packs by po…
Who is the assignee on this patent?
Panasonic Ip Man Co Ltd
What technology area does this patent fall under?
Primary CPC classification B64C27/10. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Jun 11 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).