Aircraft
US-2019002093-A1 · Jan 3, 2019 · US
US11738848B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11738848-B2 |
| Application number | US-201917416764-A |
| Country | US |
| Kind code | B2 |
| Filing date | Dec 25, 2019 |
| Priority date | Dec 28, 2018 |
| Publication date | Aug 29, 2023 |
| Grant date | Aug 29, 2023 |
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Official abstract text for this publication.
Provided is an aerial vehicle having a structure in which a rotating body has been excluded from a portion that can be touched by a user during flight. An aerial vehicle includes: a balloon unit; a control unit provided at the bottom of the balloon unit; and a plurality of micro-mechanisms (micro blowers), each of which blows out air. The micro blowers have a structure in which a vibrating member is vibrated in a space in communication with a plurality of openings, thereby blowing out, through a second opening, the air that has flowed into the space through a first opening. The control unit controls the micro blowers to change the position or the attitude of the aerial vehicle.
Opening claim text (preview).
The invention claimed is: 1. An aerial vehicle comprising: a balloon filled with a gas that has a lighter specific gravity than air; a micro-blower including a body having a chamber with a first opening and a second opening and a vibrating member disposed with the chamber of the body, wherein the vibrating member vibrates to force air to flow through the first opening into the chamber and out of the second opening to provide a propulsive force; and a control unit that controls the micro-blower to alter the propulsive force to change at least one of a position and an attitude of the aerial vehicle. 2. The aerial vehicle according to claim 1 , further comprising a detector that detects a position or attitude of the aerial vehicle, wherein: the micro-blower includes a plurality of micro-blowers; and the control unit controls the plurality of micro-blowers to alter the propulsive force according to at least one of a detected position and attitude of the aerial vehicle. 3. The aerial vehicle according to claim 2 , wherein a direction of blow from the micro-blowers is in the same direction. 4. The aerial vehicle according to claim 2 , wherein the direction of blow from the micro-blowers is in one direction and is also in another opposing direction thereto. 5. The aerial vehicle according to claim 2 , wherein the direction of blow from the micro-blowers is different from each other. 6. The aerial vehicle according to claim 1 , including a gravity center controlling mechanism that moves a center of gravity of the aerial vehicle. 7. The aerial vehicle according to claim 1 , including: an estimation unit that estimates at least either an amount of a gas filled in the balloon or an amount of the gas filled in the balloon that has leaked outside from the balloon, and a separating mechanism that separates, from the aerial vehicle, a substance mounted in an object to the aerial vehicle by an amount corresponding to the estimated amount. 8. The aerial vehicle according to claim 1 , including: a second vibrating member that is in contact with the balloon; and a sound-emitting control unit that controls the vibration of the second vibrating member that is in contact with the balloon and vibrates a surface of the balloon to emit sound. 9. The aerial vehicle according to claim 8 , wherein the second vibrating member is a piezoelectric element. 10. The aerial vehicle according to claim 1 , wherein the vibrating member is a piezoelectric element.
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