IP Library Granted Patent US 11,581,769
Granted Patent B2
US 11,581,769 · App. 16/132,420 · Granted Feb 14, 2023

Stator winding heat sink configuration

Inventors: Zaher Abdallah Daboussi (Arcadia, CA); Lindsay Aspinwall Sheppard (Azusa, CA); Bart Dean Hibbs (Simi Valley, CA); Wally Ewald Rippel (Altadena, CA)
Assignee: AeroVironment, Inc.
H02K3/14H02K3/30H02K3/32H02K3/47H02K7/14H02K9/02H02K9/06H02K9/14H02K9/227H02K16/02H02K21/12Y02E10/72Y10T29/49009
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Quick Facts
Patent No.
US 11,581,769
App. No.
16/132,420
Granted
Feb 14, 2023
Kind
B2
Abstract

In one possible implementation, a motor is provided including a rotor and a stator. Front cooling fins are thermally coupled to a front of the stator, and rear cooling fins are thermally coupled to a rear portion of the stator. The winding is between the front and rear cooling fins.

Claims (37)

1. A motor comprising:

a) a permanent magnet rotor; and

b) a stator comprising:

i) front cooling fins thermally coupled to a front of the stator via a front stator yoke;

ii) a ring of rear cooling fins thermally coupled to a rear portion of the stator via a rear stator yoke, wherein the rear cooling fins have a solid outer annular face, the rear cooling fins oriented radially and extend radially between the rear stator yoke and the outer annular face; and

iii) a winding between and separating the front stator yoke and the front cooling fins from the rear stator yoke and the ring of rear cooling fins.

2. The motor of claim 1 , wherein the front stator yoke is mounted to a front end of the winding and surrounds three sides of the front end of the winding.

3. The motor of claim 2 , wherein the front cooling fins have a solid front annular face, the front cooling fins being oriented radially and extending laterally between the front annular face and the front stator yoke.

4. The motor of claim 1 , wherein the rear stator yoke is mounted to a rear end of the winding and surrounds three sides of the rear end of the winding.

5. The motor of claim 1 , wherein the front cooling fins have an outer radius and an inner radius, the outer radius being about a same outer radius as the winding.

6. The motor of claim 5 , wherein the rotor comprises and outer rotor, and wherein the rear cooling fins have an outer radius and an inner radius, the inner radius being about at a same radius as an outer radius of the outer rotor.

7. The motor of claim 1 , wherein the rotor comprises and outer rotor, and wherein the rear cooling fins have an outer radius and an inner radius, the inner radius being about at a same radius as an outer radius of the outer rotor.

8. The motor of claim 1 , wherein the motor is an aircraft motor comprising a spinner, and wherein the front cooling fins are housed within the spinner.

9. A motor comprising:

a) an inner and outer rotor connected together;

b) a stator between the inner and outer rotors, the stator comprising:

i) a coreless winding comprising conductors encased in a thermally conductive material;

ii) a thermally conductive front yoke mounted to a front end of the winding;

iii) front cooling fins mounted to the front yoke;

iv) a thermally conductive rear yoke mounted to a rear end of the winding; and

v) rear cooling fins mounted to and surrounding the rear yoke, wherein the rear cooling fins have a solid outer annular face, the rear cooling fins being oriented radially and extending radially between the rear stator yoke and the outer annular face; and

c) wherein the winding is disposed between and separates the front yoke and the front cooling fins from the rear yoke and the rear cooling fins.

10. The motor of claim 9 , wherein the front cooling fins are mounted to a front end of the front yoke.

11. The motor of claim 10 , wherein the front yoke surrounds three sides of the front end of the winding, and wherein the rear yoke surrounds three sides of the rear end of the winding.

12. The motor of claim 9 , wherein the rear cooling fins are mounted to an outer surface of the rear yoke.

13. An aircraft motor comprising:

a) an inner and outer rotor connected together; and

b) a stator between the inner and outer rotors, the stator comprising:

i) a coreless winding comprising conductors encased in a thermally conductive material;

ii) a thermally conductive front yoke mounted to a front end of the winding;

iii) front cooling fins mounted to the front yoke, the front cooling fins have a solid front annular face, the front cooling fins being oriented radially and extending laterally between the front annular face and the front yoke;

iv) a thermally conductive rear yoke mounted to a back end of the winding; and

v) rear cooling fins mounted to the rear yoke the rear cooling fins have a solid outer annular face, the rear cooling fins oriented radially and extend radially between the rear yoke and the outer annular face.

14. The motor of claim 13 , wherein the front cooling fins have an outer radius and an inner radius, the outer radius being about a same outer radius as the winding.

15. The motor of claim 14 , wherein the rear cooling fins have an outer radius and an inner radius, the inner radius being about at a same radius as an outer radius of the outer rotor.

16. The motor of claim 13 , wherein the rear cooling fins have an outer radius and an inner radius, the inner radius being about at a same radius as an outer radius of the outer rotor.

17. The motor of claim 13 , further comprising a spinner, and wherein the front cooling fins are housed within the spinner.

Assignments (2)
NOTICE OF GRANT OF SECURITY INTEREST IN PATENTS Recorded Feb 19, 2021
From: AEROVIRONMENT, INC.
To: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT
Reel/Frame 055343/0926 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 3, 2018
From: DABOUSSI, ZAHER ABDALLAH; HIBBS, BART DEAN; SHEPPARD, LINDSAY ASPINWALL; RIPPEL, WALLY EWALD
To: AEROVIRONMENT, INC.
Reel/Frame 047190/0212 →
Continuity (7)
Continuation 15668577 · Aug 3, 2017
Continuation 14187011 · Feb 21, 2014
Continuation 12565710 · Sep 23, 2009
Provisional Application 61194099 · Sep 23, 2008
Provisional Application 61194098 · Sep 23, 2008
Provisional Application 61194056 · Sep 23, 2008
Related Publication 20190103780A1 · Apr 4, 2019