Motor structure of unmanned aerial vehicle
US-2017074272-A1 · Mar 16, 2017 · US
US11338906B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11338906-B2 |
| Application number | US-201916679516-A |
| Country | US |
| Kind code | B2 |
| Filing date | Nov 11, 2019 |
| Priority date | Dec 13, 2018 |
| Publication date | May 24, 2022 |
| Grant date | May 24, 2022 |
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A propeller system includes a rotatable housing having at least one propeller blade mounted thereon and an electric pitch control motor within the rotatable housing. A pitch control member is coupled to the propeller blade and extends through a wall of the rotatable housing. The pitch control motor is configured to move the pitch control member and to thereby vary the pitch of the propeller blade.
Opening claim text (preview).
The invention claimed is: 1. A propeller system comprising: a rotatable housing having at least one propeller blade mounted thereon; an electric pitch control motor within the rotatable housing; and a pitch control member coupled to the propeller blade and extending through a wall of the rotatable housing; wherein the pitch control motor is configured to move the pitch control member and to thereby vary the pitch of the propeller blade; wherein: the propeller blade extends radially outwards from the rotatable housing and has an inner end mounted to the housing such that the propeller blade is able to rotate about its longitudinal axis; and the pitch control member is engaged with a lateral side of the propeller blade such that when the pitch control motor moves the pitch control member, the propeller blade is rotated about its longitudinal axis so as to vary the pitch of the propeller blade. 2. The propeller system of claim 1 , wherein the pitch control member extends from the propeller blade, through an elongated slot in the rotatable housing, and to an inner portion; wherein one or more magnet is arranged on the inner portion of the pitch control member. 3. The propeller system of claim 2 , wherein the elongated slot is a straight or curved slot extending substantially parallel to a rotational axis about which the rotatable housing rotates. 4. The propeller system of claim 2 , wherein the pitch control motor comprises a winding for generating a magnetic field when supplied with an electric current, and wherein said one or more magnet on the inner portion of the pitch control member comprises one or more permanent magnet. 5. A propeller system comprising: a rotatable housing having at least one propeller blade mounted thereon; an electric pitch control motor within the rotatable housing; and a pitch control member coupled to the propeller blade and extending through a wall of the rotatable housing; wherein the pitch control motor is configured to move the pitch control member and to thereby vary the pitch of the propeller blade; wherein the pitch control motor is a linear motor for moving the pitch control member in a direction that is substantially parallel to a rotational axis about which the rotatable housing rotates. 6. A propeller system comprising: a rotatable housing having at least one propeller blade mounted thereon; an electric pitch control motor within the rotatable housing; a pitch control member coupled to the propeller blade and extending through a wall of the rotatable housing, wherein the pitch control motor is configured to move the pitch control member and to thereby vary the pitch of the propeller blade; and a propulsion motor configured to rotate the rotatable housing, wherein the propulsion motor is an electric motor having an inner stator and an outer rotor, and wherein the rotatable housing forms part of the outer rotor. 7. The propeller system of claim 6 , wherein the propulsion motor comprises a winding on the stator configured to generate a magnetic field when supplied with an electric current, and at least one permanent magnet on the rotor for being moved by the magnetic field. 8. The propeller system of claim 6 , wherein the rotatable housing is mounted on one or more supports by bearings and the pitch control motor and propulsion motor are axially located between the bearings. 9. The propeller system of claim 8 , wherein the one or more supports is a shaft and a stator of the pitch control motor and/or a stator of the propulsion motor are located on the shaft. 10. The propeller system of claim 8 , in combination with an aerospace vehicle or a maritime vehicle.
mechanical · CPC title
characterised by being influenced by other control systems, e.g. fuel supply · CPC title
electric · CPC title
characterised by use of non-mechanical actuating means, e.g. electrical (B63H3/002 takes precedence) · CPC title
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