IP Library › Granted Patent US 11,588,363
Granted Patent B2
US 11,588,363 · App. 16/938,952 · Granted Feb 21, 2023

Integrated electric propulsion assembly

Inventor: Manon Danielle Belzile (Fairfield, VT)
Assignee: BETA AIR, LLC
H02K3/04B64D27/24H02K1/12H02K1/27H02K11/30
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Quick Facts
Patent No.
US 11,588,363
App. No.
16/938,952
Granted
Feb 21, 2023
Kind
B2
Abstract

An integrated stator assembly incorporated in an electric motor including a rotor that includes a plurality of rotor magnets, each rotor magnet of the plurality of magnets having a polar axis running from a rotor magnet south pole to a rotor magnet north pole. The assembly comprising a mandrel of dielectric material, wherein the mandrel includes a first cylindrical surface coaxial to an axis of rotation of the rotor, an upper edge, and a lower edge. A plurality of electrically conductive stator windings wound upon the mandrel, each winding of the plurality of windings including a plurality of turns traversing the first cylindrical surface, wherein each turn of the plurality turns further comprises a first upper section disposed on the first cylindrical surface, wherein the first upper section intersects the upper edge of the mandrel, and the first upper section forms a first angle to the axis of rotation.

Claims (58)

1. An integrated stator assembly incorporated in an electric motor including a rotor that includes a plurality of rotor magnets, each rotor magnet of the plurality of magnets having a polar axis running from a rotor magnet south pole to a rotor magnet north pole, the assembly comprising:

a mandrel of dielectric material, wherein the mandrel includes:

a first cylindrical surface coaxial to an axis of rotation of the rotor;

an upper edge; and

a lower edge;

a plurality of electrically conductive stator windings wound upon the mandrel, each winding of the plurality of windings including a plurality of turns traversing the first cylindrical surface, wherein each turn of the plurality turns further comprises:

a first upper section disposed on the first cylindrical surface, wherein:

the first upper section intersects the upper edge of the mandrel; and

the first upper section forms a first angle to the axis of rotation;

a first lower section disposed on the first cylindrical surface, wherein:

the first lower section intersects the lower edge of the mandrel; and

the first lower section forms a second angle to the axis of rotation; and

a first middle section disposed on the first cylindrical surface, between the first upper section and the first lower section, wherein:

the first middle section forms a third angle with respect to the axis of rotation; and

the third angle is perpendicular to each polar axis of each rotor magnet of the plurality of rotor magnets.

2. The assembly of claim 1 , wherein:

the mandrel further comprises a first plurality of walls projecting from the first cylindrical surface;

the first plurality of walls form a first plurality of channels across the first cylindrical surface; and

the plurality turns are channeled in the plurality of channels.

3. The assembly of claim 2 , wherein the plurality of walls further comprises a plurality of retention tabs projecting over the first plurality of channels.

4. The assembly of claim 1 , wherein:

the mandrel further comprises a second cylindrical surface coaxial to the axis of rotation; and

the second cylindrical surface is opposite the first cylindrical surface.

5. The assembly of claim 4 , wherein each turn of the plurality of turns further comprise:

a second upper section disposed on the second cylindrical surface, wherein:

the second upper section intersects the upper edge of the mandrel; and

the second upper section forms a fourth angle to the axis of rotation;

a second lower section disposed on the second cylindrical surface, wherein:

the second lower section intersects the lower edge of the mandrel; and

the second lower section forms a fifth angle to the axis of rotation; and

a second middle section disposed on the second cylindrical surface, between the upper section and the lower section, wherein:

the middle section forms a sixth angle with respect to the axis of rotation; and

the sixth angle is perpendicular to each polar axis of each rotor magnet of the plurality of rotor magnets.

6. The assembly of claim 4 , wherein:

the mandrel further comprises a first plurality of walls projecting from the first cylindrical surface, wherein:

the first plurality of walls form a plurality of channels across the first cylindrical surface; and

the plurality turns are channeled in the plurality of channels;

the mandrel further comprises a second plurality of walls projecting from the second cylindrical surface, wherein:

the second plurality of walls form a second plurality of channels across the first cylindrical surface; and

the plurality of turns are channeled in the second plurality of channels.

7. The assembly of claim 6 , wherein the second plurality of walls further comprises a plurality of retention tabs projecting over the second plurality of channels.

8. The assembly of claim 6 , wherein the plurality of first channels connect to the plurality of second channels at the upper edge and the lower edge.

9. The assembly of claim 6 further comprising a plurality of projecting tabs extending beyond the upper edge and the lower edge, the plurality of projecting tabs connecting the first plurality of walls to the second plurality of walls.

10. The assembly of claim 6 , wherein:

the mandrel includes a through-hole passing from the first cylindrical surface to the second surface; and

the through-hole connects a channel of the first plurality of channels to a channel of the second plurality of channels.

11. The assembly of claim 1 , wherein the mandrel includes:

a first mandrel half having a first end and a second end; and

a second mandrel half having a third end and a fourth end.

12. The assembly of claim 11 , wherein the plurality of windings includes a first winding on the first mandrel half and a second winding around the second mandrel half.

13. The assembly of claim 12 , wherein the first winding includes a first phase that traverses a first set of channels from the first end, passes through a through-hole at the second end, and traverses a second set of channels back to the first end.

14. The assembly of claim 13 , wherein the first phase further passes through a second through hole at the first end, traverses a third set of channels to the second end, passes through a third hole at the second end, and traverses a fourth set of channels back to the first end.

15. The assembly of claim 13 , wherein the first winding includes at least a second phase electrically isolated from the first phase.

16. The assembly of claim 12 , wherein the first winding is connected to at least a first inverter.

17. The assembly of claim 12 , wherein the second winding includes a third phase that traverses a fifth set of channels from the fourth end to a fourth through-hole at the third end, and traverses a sixth set of channels back to the fourth end.

18. The assembly of claim 17 , wherein the third phase passes through a fifth through hole at the fourth end, traverses a seventh set of channels to the second end, passes through a sixth through-hole at the third end, and traverses an eighth set of channels back to the fourth end.

19. The assembly of claim 12 , wherein the a second winding includes at least a fourth phase electrically isolated from the first phase.

20. The assembly of claim 12 , wherein the second winding is connected to at least a second inverter.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 21, 2020
From: BELZILE, MANON DANIELLE
To: BETA AIR, LLC
Reel/Frame 054120/0665 →
Continuity (1)
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