Aircraft electrical machine with improved heat transfer by means of a phase change material and associated method

Patent metadata

Field	Value
Publication number	US-12424913-B2
Application number	US-202118042157-A
Country	US
Kind code	B2
Filing date	Aug 13, 2021
Priority date	Aug 20, 2020
Publication date	Sep 23, 2025
Grant date	Sep 23, 2025

Abstract

A method for protecting coils from excessive heating in an aircraft electrical machine comprising a stator and a rotor configured to be rotationally driven with respect to one another, the stator including a plurality of notches receiving one and the same plurality or otherwise of coils, the method including the following successive steps:
inserting an electrical insulator into the notches or onto the teeth of the stator, installing the coils in the notches or on the teeth of the stator, casting a phase change material in the notches or on the teeth equipped with the coils, the electrical insulator forming a casting mold.

First claim

The invention claimed is:

1. A method for protecting coils from excessive heating in an aircraft electrical machine comprising a stator and a rotor configured to be rotationally driven with respect to one another, the stator including a plurality of notches or of teeth receiving one and the same plurality or otherwise of coils, a method including:
inserting an electrical insulator into the notches or onto the teeth of the stator,
installing the coils in the notches or on the teeth of the stator,
casting a phase change material in the notches or on the teeth equipped with the coils, the electrical insulator forming a casting mold.

2. The method as claimed in claim 1 , wherein, when the notches are open and the insulator thus sectorized, casting the phase change material is preceded by inserting a shim or a lock ring to close the notches and thus prevent the casting of the phase change material outside the notches.

3. The method as claimed in claim 2 , wherein the electrical insulator, sectorized or not, results from a first cast of a standard resin conventionally used to encapsulate the coils of electrical machines.

4. The method as claimed in claim 2 , wherein the phase change material is previously mixed with a resin of epoxy, polyurethane or silicone type.

5. The method as claimed in claim 2 , wherein the phase change material is previously mixed with a resin of epoxy, polyurethane or silicone type.

6. The method as claimed in claim 1 , wherein the electrical insulator, sectorized or not, results from a first cast of a standard resin conventionally used to encapsulate the coils of electrical machines.

7. The method as claimed in claim 1 , wherein the phase change material is previously mixed with a resin of epoxy, polyurethane or silicone type.

8. An aircraft electrical machine comprising a stator and a rotor configured to be rotationally driven with respect to one another, the stator including a plurality of notches or of teeth receiving one and the same plurality or otherwise of coils, wherein, to protect the coils from excessive heating, the machine comprises an electrical insulator inserted into the notches or onto the teeth to successively receive said coils and a phase change material for which it forms a casting mold.

9. The electrical machine as claimed in claim 8 , wherein the electrical insulator and the coil encapsulated in the phase change material can advantageously form an independent module directly insertable onto each of the stator teeth.

10. The electrical machine as claimed in claim 9 , wherein the phase change material is a nitrate or a hydroxide preferably filled with graphite having a phase change temperature between 150° C. and 300° C.

11. The electrical machine as claimed in claim 8 , wherein said electrical insulator is formed from a plurality of elements corresponding to the plurality of notches or of teeth, each of the elements thus sectorized being configured to be individually inserted into each of the notches or onto each of the teeth.

12. The electrical machine as claimed in claim 11 , wherein said electrical insulator is one of the following insulators: paper, mica, polyethylene terephthalate, polyester, glass fiber.

13. The electrical machine as claimed in claim 12 , wherein the phase change material is a nitrate or a hydroxide preferably filled with graphite having a phase change temperature between 150° C. and 300° C.

14. The electrical machine as claimed in claim 11 , wherein said electrical insulator is obtained by an additive manufacturing method or from a plastic, such as PEEK (PolyEtherEtherKetone) or Polyamide 66 (PA66), having appropriate electrical insulation and thermal resistance features.

15. The electrical machine as claimed in claim 11 , wherein the phase change material is a nitrate or a hydroxide preferably filled with graphite having a phase change temperature between 150° C. and 300° C.

16. The electrical machine as claimed in claim 8 , wherein said electrical insulator is formed from a single element adapted to the geometry of the stator and configured to be inserted jointly into all the notches.

17. The electrical machine as claimed in claim 16 , wherein said electrical insulator is obtained by an additive manufacturing method or from a plastic, such as PEEK (PolyEtherEtherKetone) or Polyamide 66 (PA66), having appropriate electrical insulation and thermal resistance features.

18. The electrical machine as claimed in claim 8 , wherein the phase change material is a nitrate or a hydroxide preferably filled with graphite having a phase change temperature between 150° C. and 300° C.

19. An independent module composed of an electrical insulator and coils encapsulated in a phase change material and directly insertable onto each of the teeth of a stator of an electrical machine as claimed in claim 8 .

20. An aircraft engine including at least one electrical machine as claimed in claim 8 .

Assignees

• Safran Helicopter Engines
• Safran

Inventors

• Serghine Camel
• Klonowski Thomas
• Quinio Pierre Gabriel Marie
• Ayat Sabrina Siham
• Rouland Eric
• Yon Sébastien
• Mutabazi Albert

Classifications

• H02K3/522

  for generally annular cores with salient poles · CPC title

• H02K15/02

  of stator or rotor bodies · CPC title

• H02K3/345 Primary

  between conductor and core, e.g. slot insulation · CPC title

• C09K5/063

  Materials absorbing or liberating heat during crystallisation; Heat storage materials · CPC title

• H02K9/20

  wherein the cooling medium vaporises within the machine casing · CPC title