IP Library Granted Patent US 8,201,316
Granted Patent B2
US 8,201,316 · App. 12/378,384 · Granted Jun 19, 2012

Lamination cooling system formation method

Assignee: AeroVironment Inc.
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Quick Facts
Patent No.
US 8,201,316
App. No.
12/378,384
Granted
Jun 19, 2012
Kind
B2
Abstract

An electric motor, transformer or inductor having a cooling system. A stack of laminations have apertures at least partially coincident with apertures of adjacent laminations. The apertures define straight or angled cooling-fluid passageways through the lamination stack. Gaps between the adjacent laminations are sealed by injecting a heat-cured sealant into the passageways, expelling excess sealant, and heat-curing the lamination stack. Manifold members adjoin opposite ends of the lamination stack, and each is configured with one or more cavities to act as a manifold to adjacent passageway ends. Complex manifold arrangements can create bidirectional flow in a variety of patterns.

Claims (61)

1. A method of forming a lamination cooling system, comprising:

injecting a sealant between a plurality of laminations in a lamination stack using an adequate hydrostatic pressure to inject the sealant between the plurality of laminations, wherein each lamination defines an aperture, wherein the aperture of each lamination is at least partially coincident with the apertures of adjacent laminations such that the apertures define a cooling-fluid passageway through the lamination stack, wherein the sealant forms a seal to prevent a liquid cooling fluid in the passageway from exiting the lamination stack between adjacent laminations, and wherein the step of injecting includes injecting the sealant into the passageway, the sealant being at a pressure adequate to force the sealant to flow between adjoining laminations; and then

removing enough sealant from the passageway to configure it as a sealed conduit capable of passing cooling fluid from a first end of the passageway to a second end of the passageway;

wherein the step of injecting includes injecting the passageway with sealant, removing excess sealant from the passageway, and forcing sealant further into voids between the laminations using pressurized air.

2. The method of claim 1 , and further comprising curing the sealant by an appropriate temperature cycle, wherein the sealant is a heat-cured, low-viscosity epoxy.

3. The method of claim 1 , wherein the sealant is a material selected from the group consisting of a heat-curable low-viscosity epoxy, a varnish-type material, and a silicon-based material.

4. The method of claim 1 , wherein:

the excess sealant is removed either by allowing sealant to drain out under the force of gravity, or by passing air through the passageways, or both.

5. The method of claim 1 , wherein:

each lamination defines a second aperture, the second aperture of each lamination being at least partially coincident with the second apertures of adjacent laminations such that the second apertures define a second cooling-fluid passageway through the lamination stack; and

in the step of injecting, the sealant forms a seal to prevent a liquid cooling fluid in the second passageway from exiting the lamination stack between adjacent laminations.

6. The method of claim 1 , wherein the laminations are planar, and wherein the aperture of each lamination is completely coincident with the apertures of adjacent laminations such that the passageway is straight, extending in a direction normal to the plane of the laminations.

7. The method of claim 1 , and further comprising:

adjoining a manifold member to an end lamination on an end of the lamination stack, the manifold defining a chamber in fluid communication with the passageway;

wherein in the step of injecting, the sealant further forms a seal to prevent the liquid cooling fluid in the chamber from exiting between the end lamination and the manifold.

8. The method of claim 7 , and further comprising:

adjoining a second manifold member to a second end lamination on a second end of the lamination stack, the second manifold member defining a second chamber in fluid communication with the passageway, wherein the laminations are compressed together by the first and second manifold members;

wherein in the step of injecting, the sealant further forms a seal to prevent a liquid cooling fluid in the second chamber from exiting between the second end lamination and the second manifold member.

9. A method of forming a lamination cooling system, comprising:

forming a lamination stack from a plurality of laminations, wherein each lamination defines an aperture, and wherein the aperture of each lamination is at least partially coincident with the apertures of adjacent laminations in the lamination stack such that the apertures define a cooling-fluid passageway through the lamination stack; and

injecting a sealant between the plurality of laminations using an adequate hydrostatic pressure to inject the sealant between the plurality of laminations, wherein the sealant forms a seal to prevent a liquid cooling fluid in the passageway from exiting the lamination stack between adjacent laminations;

wherein the lamination stack is formed prior to the step of injecting;

wherein the step of injecting includes injecting the sealant into the passageway, the sealant being at a pressure adequate to force the sealant to flow between adjoining laminations; and then removing enough sealant from the passageway to configure it as a sealed conduit capable of passing cooling fluid from a first end of the passageway to a second end of the passageway; and

wherein the cooling-fluid passageway is formed in a center prong of an “E” shaped core lamination stack.

10. The method of claim 9 , wherein:

each lamination defines a second aperture, the second aperture of each lamination being at least partially coincident with the second apertures of adjacent laminations such that the second apertures define a second cooling-fluid passageway through the lamination stack; and

in the step of injecting, the sealant forms a seal to prevent a liquid cooling fluid in the second passageway from exiting the lamination stack between adjacent laminations.

11. The method of claim 10 , and further comprising:

adjoining a manifold member to an end lamination on an end of the lamination stack, the manifold defining a chamber in fluid communication with the passageways;

wherein in the step of injecting, the sealant further forms a seal to prevent a liquid cooling fluid in the chamber from exiting between the end lamination and the manifold.

12. The method of claim 11 , and further comprising:

adjoining a second manifold member to a second end lamination on a second end of the lamination stack, the second manifold defining a second chamber in fluid communication with the passageways;

wherein in the step of injecting, the sealant further forms a seal to prevent a liquid cooling fluid in the second chamber from exiting between the second end lamination and the second manifold member.

13. A method of forming a lamination cooling system, comprising:

injecting a sealant between a plurality of laminations in a lamination stack using an adequate hydrostatic pressure to inject the sealant between the plurality of laminations, wherein each lamination defines an aperture, wherein the aperture of each lamination is at least partially coincident with the apertures of adjacent laminations such that the apertures define a cooling-fluid passageway through the lamination stack, wherein the sealant forms a seal to prevent a liquid cooling fluid in the passageway from exiting the lamination stack between adjacent laminations, and wherein the step of injecting includes injecting the sealant into the passageway, the sealant being at a pressure adequate to force the sealant to flow between adjoining laminations;

adjoining a manifold member to an end lamination on an end of the lamination stack, the manifold defining a chamber in fluid communication with the passageway;

removing enough sealant from the passageway to configure it as a sealed conduit capable of passing cooling fluid from a first end of the passageway to a second end of the passageway; and

wherein in the step of injecting, the sealant further forms a seal to prevent the liquid cooling fluid in the chamber from exiting between the end lamination and the manifold.

14. The method of claim 13 , and further comprising curing the sealant by an appropriate temperature cycle, wherein the sealant is a heat-cured, low-viscosity epoxy.

15. The method of claim 13 , wherein the sealant is a material selected from the group consisting of a heat-curable low-viscosity epoxy, a varnish-type material, and a silicon-based material.

16. The method of claim 13 , wherein:

the excess sealant is removed either by allowing sealant to drain out under the force of gravity, or by passing air through the passageways, or both.

17. The method of claim 13 , wherein:

each lamination defines a second aperture, the second aperture of each lamination being at least partially coincident with the second apertures of adjacent laminations such that the second apertures define a second cooling-fluid passageway through the lamination stack; and

in the step of injecting, the sealant forms a seal to prevent a liquid cooling fluid in the second passageway from exiting the lamination stack between adjacent laminations.

18. The method of claim 13 , wherein the laminations are planar, and wherein the aperture of each lamination is completely coincident with the apertures of adjacent laminations such that the passageway is straight, extending in a direction normal to the plane of the laminations.

19. The method of claim 13 , and further comprising:

adjoining a second manifold member to a second end lamination on a second end of the lamination stack, the second manifold member defining a second chamber in fluid communication with the passageway, wherein the laminations are compressed together by the first and second manifold members;

wherein in the step of injecting, the sealant further forms a seal to prevent a liquid cooling fluid in the second chamber from exiting between the second end lamination and the second manifold member.

20. A method of forming a lamination cooling system, comprising:

forming a lamination stack from a plurality of laminations, wherein each lamination defines an aperture, and wherein the aperture of each lamination is at least partially coincident with the apertures of adjacent laminations in the lamination stack such that the apertures define a cooling-fluid passageway through the lamination stack;

adjoining a manifold member to an end lamination on an end of the lamination stack, the manifold defining a chamber in fluid communication with the passageways; and

injecting a sealant between the plurality of laminations using an adequate hydrostatic pressure to inject the sealant between the plurality of laminations, wherein the sealant forms a seal to prevent a liquid cooling fluid in the passageway from exiting the lamination stack between adjacent laminations;

wherein the lamination stack is formed prior to the step of injecting; and

wherein the step of injecting includes injecting the sealant into the passageway, the sealant being at a pressure adequate to force the sealant to flow between adjoining laminations; and then removing enough sealant from the passageway to configure it as a sealed conduit capable of passing cooling fluid from a first end of the passageway to a second end of the passageway;

wherein each lamination defines a second aperture, the second aperture of each lamination being at least partially coincident with the second apertures of adjacent laminations such that the second apertures define a second cooling-fluid passageway through the lamination stack;

wherein in the step of injecting, the sealant forms a seal to prevent a liquid cooling fluid in the second passageway from exiting the lamination stack between adjacent laminations; and

wherein in the step of injecting, the sealant further forms a seal to prevent a liquid cooling fluid in the chamber from exiting between the end lamination and the manifold.

21. The method of claim 20 , and further comprising:

adjoining a second manifold member to a second end lamination on a second end of the lamination stack, the second manifold defining a second chamber in fluid communication with the passageways;

wherein in the step of injecting, the sealant further forms a seal to prevent a liquid cooling fluid in the second chamber from exiting between the second end lamination and the second manifold member.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 29, 2018
From: AEROVIRONMENT, INC.
To: WEBASTO CHARGING SYSTEMS, INC.
Reel/Frame 046970/0124 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 11, 2009
From: RIPPEL, WALLY E.; KOBAYASHI, DARYL M.
To: AEROVIRONMENT INC.
Reel/Frame 022319/0390 →
Continuity (4)
Continuation 11242823 · Oct 3, 2005
Division 10431324 · May 6, 2003
Provisional Application 60378276 · May 6, 2002
Related Publication 20090188621A1 · Jul 30, 2009