Multi-layer susceptor assembly for inductively heating an aerosol-forming substrate

Patent metadata

Field	Value
Publication number	US-11516893-B2
Application number	US-201816494848-A
Country	US
Kind code	B2
Filing date	Mar 29, 2018
Priority date	Mar 31, 2017
Publication date	Nov 29, 2022
Grant date	Nov 29, 2022

Abstract

The present invention relates to a multi-layer susceptor assembly for inductively heating an aerosol-forming substrate which comprises at least a first layer and a second layer intimately coupled to the first layer. The first layer comprises a first susceptor material. The second layer comprises a second susceptor material having a Curie temperature lower than 500° C. The susceptor assembly further comprises a third layer intimately coupled to the second layer. The third layer comprises a specific stress-compensating material and specific layer thickness for compensating differences in thermal expansion occurring in the multi-layer susceptor assembly after a processing of the assembly such that at least in a compensation temperature range an overall thermal deformation of the susceptor assembly is essentially limited to in-plane deformations. The compensation temperature range extends at least from 20 K below the Curie temperature of the second susceptor material up to the Curie temperature of the second susceptor material.

First claim

The invention claimed is:

1. A multi-layer susceptor assembly for inductively heating an aerosol-forming substrate, the susceptor assembly comprising at least:
a first layer comprising a first susceptor material;
a second layer intimately coupled to the first layer, comprising a second susceptor material having a Curie temperature lower than 500 ° C.;
a third layer intimately coupled to the second layer, comprising a specific stress-compensating material and specific layer thickness for compensating differences in thermal expansion occurring in the multi-layer susceptor assembly after intimately coupling the layers to each other and/or after a heat treatment of the multi-layer susceptor assembly such that at least in a compensation temperature range an overall thermal deformation of the susceptor assembly is essentially limited to in-plane deformations, wherein the compensation temperature range extends at least from 20 K below the Curie temperature of the second susceptor material up to the Curie temperature of the second susceptor material.

2. The susceptor assembly according to claim 1 , wherein a coefficient of thermal expansion of the stress-compensating material is essentially equal to a coefficient of thermal expansion of the first susceptor material.

3. The susceptor assembly according to claim 1 , wherein the stress-compensating material of the third layer is the same as the first susceptor material of the first layer.

4. The susceptor assembly according to claim 1 , wherein a coefficient of thermal expansion of the second susceptor material is larger than a coefficient of thermal expansion of the first susceptor material and smaller than a coefficient of thermal expansion of the stress-compensating material.

5. The susceptor assembly according to claim 1 , wherein a coefficient of thermal expansion of the second susceptor material is smaller than a coefficient of thermal expansion of the first susceptor material and larger than a coefficient of thermal expansion of the stress-compensating material.

6. The susceptor assembly according to claim 1 , wherein the stress-compensating material of the third layer is different from the first susceptor material of the first layer.

7. The susceptor assembly according to claim 1 , wherein the first susceptor material includes aluminum, iron or an iron alloy, in particular a grade 410, 420, 430 or 430 stainless steel.

8. The susceptor assembly according to claim 1 , wherein the second susceptor material includes nickel or a nickel alloy, in particular a soft Fe-Ni-Cr alloy or a Fe-Ni-Cu-X alloy, wherein X is one or more elements taken from Cr, Mo, Mn, Si, Al, W, Nb, V and Ti.

9. The susceptor assembly according to claim 1 , wherein the stress-compensating material of the third layer includes an austenitic stainless steel.

10. The susceptor assembly according to claim 1 , wherein the layer thickness of the third layer is in a range of 0.5 to 1.5, in particular 0.75 to 1.25, times a layer thickness of the first layer, preferably the layer thickness of the third layer is equal to a layer thickness of the first layer.

11. The susceptor assembly according to claim 1 , wherein the first layer, the second layer and the third layer are adjacent layers of the multilayer susceptor assembly.

12. The susceptor assembly according to claim 1 , wherein the third layer is arranged upon and intimately coupled to the second layer, and wherein the second layer is arranged upon and intimately coupled to the first layer.

13. An aerosol-generating article comprising an aerosol-forming substrate and a susceptor assembly according to claim 1 .

14. The aerosol-generating article according to claim 13 , wherein the susceptor assembly is located in the aerosol-forming substrate.

Assignees

• Philip Morris Products Sa

Inventors

• Rossoll Andreas Michael
• Fursa Oleg

Classifications

• A24F40/465 Primary

  specially adapted for induction heating · CPC title

• H05B2206/023

  using the curie point of the material in which heating current is being generated to control the heating temperature · CPC title

• H05B6/105 Primary

  using a susceptor · CPC title

• A61M2205/02

  characterised by a particular materials · CPC title

• A24F40/46 Primary

  Shape or structure of electric heating means · CPC title