Bearing configuration for an electronic motor
A motor including a rotor, a first arm, a mount, a stator, a first bearing, and a second bearing. The motor is configured to rotate the rotor. The mount connected to the first arm. The stator coupled to the mount. The first bearing located between and connecting the rotor to the stator. The second bearing located between and connecting the rotor to the mount. The first arm prevents movement of the stator and the mount.
1 . An aerial vehicle comprising:
a first arm;
a motor comprising:
a motor shell;
a rotor located within the motor shell, the motor configured to rotate the rotor;
a fixed component comprising:
a mount located within the motor shell and coupled to a portion of the first arm that is located in the motor shell; and
a stator coupled to the mount;
a first bearing located between and connecting the rotor to the stator; and
a second bearing located between and connecting the rotor to the mount,
wherein the fixed component is mutually coupled to the first arm.
2 . The aerial vehicle of claim 1 , wherein:
the first bearing comprises:
a first inner race that is connected to the rotor; and
a first outer race that is connected to the stator, wherein a first plurality of rolling elements are located between the first inner race and the first outer race so that the first inner race and the first outer race are configured to move relative to one another, and
the second bearing comprises:
a second inner race that is connected to the rotor; and
a second outer race that is connected to the mount, wherein a second plurality of rolling elements are located between the second inner race and the second outer race so that the second inner race and the second outer race are configured to move relative to one another.
3 . The aerial vehicle of claim 1 , further comprising:
a first plurality of rolling elements located in the first bearing; and
a second plurality of rolling elements located in the second bearing, wherein the first plurality of rolling elements and the second plurality of rolling elements are a spherical ball or a cylindrical element.
4 . The aerial vehicle of claim 1 , further comprising:
a third bearing connected to the rotor and the mount, and wherein the third bearing is located between the first bearing the second bearing.
5 . The aerial vehicle of claim 3 , wherein a third bearing includes a third plurality of rolling elements, and wherein a respective radii of the second plurality of rolling elements are larger than a respective radii of the third plurality of rolling elements by a ratio of at least 1.5.
6 . The aerial vehicle of claim 4 , wherein the third bearing includes a third plurality of rolling elements, and wherein a respective radii of a first plurality of rolling elements and the respective radii of the third plurality of rolling elements differ by a factor of 0.1 or less.
7 . The aerial vehicle of claim 1 , wherein the motor shell includes a first motor shell and a second motor shell.
8 . The aerial vehicle of claim 7 , further comprising:
a rotor screw connecting the second motor shell to the rotor.
9 . The aerial vehicle of claim 1 further comprising:
a motor shell that couples to the mount and houses the stator, the first and second bearings, and at least a portion of the rotor.
10 . An aerial vehicle comprising:
a motor comprising:
a motor shell;
a rotor located within the motor shell, the motor configured to rotate the rotor;
a fixed component comprising:
a mount; and
a stator connected to the mount;
a first bearing including:
a first inner race in communication with the rotor,
a first outer race in communication with the stator, and
a first plurality of rolling elements located between the first inner race and the first outer race; and
a second bearing including:
a second inner race in communication with the rotor,
a second outer race in communication with the mount, and
a second plurality of rolling elements located between the second inner race and the second outer race; and
a first arm having a portion located in the motor shell that connects to the mount;
wherein the fixed component is coupled to and fixed relative to the portion of the first arm located in the motor shell.
11 . The aerial vehicle of claim 10 , wherein the first plurality of rolling elements and the second plurality of rolling elements are spherical balls or cylindrical elements.
12 . The aerial vehicle of claim 10 , further comprising:
a third bearing including:
a third inner race connected to the rotor,
a third outer race connected to the mount, and
a third plurality of rolling elements located between the third inner race and the third outer race.
13 . The aerial vehicle of claim 12 , wherein the third bearing is located between the first bearing and the second bearing.
14 . The aerial vehicle of claim 12 , wherein a radius of the second outer race is greater than a radius of the third outer race by a ratio of at least 1.5.
15 . The aerial vehicle of claim 12 , wherein a radius of the second outer race and a radius of the third outer race differ by a factor of 0.1 or less.
16 . The aerial vehicle of claim 10 , wherein the motor shell comprises:
a first motor shell; and
a second motor shell,
wherein the first motor shell is connected to the mount.
17 . The aerial vehicle of claim 16 , wherein one or more screws connect the first motor shell to the mount.
18 . An aerial vehicle comprising:
a motor comprising:
a first motor shell;
a second motor shell, wherein the first motor shell and the second motor shell form an interior cavity;
a rotor configured to be a rotational part of the motor;
a fixed component comprising:
a mount located within the interior cavity;
a stator coupled to the mount; and
one or more screws connecting the first motor shell to the mount;
a first bearing located between and connecting the rotor to the stator; and
a second bearing located between and connecting the rotor to the mount,
a first arm comprising a portion located in the interior cavity and coupled to the mount;
wherein the fixed component is coupled to the portion of the first arm located within the interior cavity.
19 . The aerial vehicle of claim 18 , further comprising:
a rotor screw connecting the second motor shell to the rotor.
20 . The aerial vehicle of claim 18 , wherein the first motor shell is connected to the mount.