SUSCEPTOR ASSEMBLY COMPRISING ONE OR MORE COMPOSITE SUSCEPTOR PARTICLES
20230210185 · 2023-07-06
Assignee
Inventors
Cpc classification
H05B2206/023
ELECTRICITY
A24D1/20
HUMAN NECESSITIES
International classification
A24D1/20
HUMAN NECESSITIES
Abstract
A susceptor assembly is provided for inductively heating an aerosol-forming substrate under an influence of an alternating magnetic field, the susceptor assembly including: one or more composite susceptor particles, each one of the one or more composite susceptor particles including a particle core and a particle shell entirely encapsulating the particle core, in which the particle core includes or is made of a ferromagnetic or ferrimagnetic core material having a relative magnetic permeability of at least 200 for frequencies up to 10 kHz at a temperature of 20 degrees Celsius, and in which the particle shell includes or is made of an electrically conductive shell material. An aerosol-generating article for an inductively heating aerosol-generating device, and an aerosol-generating system including an aerosol-generating article, are also provided.
Claims
1.-15. (canceled)
16. A susceptor assembly for inductively heating an aerosol-forming substrate under an influence of an alternating magnetic field, the susceptor assembly comprising: one or more composite susceptor particles, wherein each one of the one or more composite susceptor particles comprises a particle core and a particle shell entirely encapsulating the particle core, wherein the particle core comprises or is made of a ferromagnetic or ferrimagnetic core material having a relative magnetic permeability of at least 200 for frequencies up to 10 kHz at a temperature of 20 degrees Celsius, and wherein the particle shell comprises or is made of an electrically conductive shell material.
17. The susceptor assembly according to claim 16, wherein a material of the particle shell is paramagnetic.
18. The susceptor assembly according to claim 16, wherein a material of the particle shell is one of aluminum, stainless steel, electrically conductive carbon, or bronze.
19. The susceptor assembly according to claim 16, wherein a material of the core is electrically non-conductive.
20. The susceptor assembly according to claim 16, wherein a material of the core has a Curie temperature in a range between 160 degrees Celsius and 400 degrees Celsius.
21. The susceptor assembly according to claim 16, wherein a material of the core has a Curie temperature in a range between 160 degrees Celsius and 240 degrees Celsius.
22. The susceptor assembly according to claim 16, wherein a material of the core is a ferrite powder.
23. The susceptor assembly according to claim 16, wherein a material of the core is of a manganese-magnesium ferrite, a nickel-zinc ferrite, or a cobalt-zinc barium ferrite.
24. The susceptor assembly according to claim 16, wherein each one of the one or more composite susceptor particles substantially has a ball shape.
25. The susceptor assembly according to claim 16, wherein each one of the one or more composite susceptor particles has an equivalent spherical particle diameter in a range between 10 micrometers and 500 micrometers.
26. The susceptor assembly according to claim 16, wherein each one of the one or more composite susceptor particles has an equivalent spherical particle diameter in a range between 35 micrometers and 75 micrometers.
27. The susceptor assembly according to claim 16, wherein the particle core has an equivalent spherical core diameter in a range between 5 micrometers and 499 micrometers.
28. The susceptor assembly according to claim 16, wherein the particle core has an equivalent spherical core diameter in a range between 30 micrometers and 55 micrometers.
29. The susceptor assembly according to claim 16, wherein the particle shell has a shell thickness in a range between 1 micrometer and 100 micrometers.
30. The susceptor assembly according to claim 16, wherein the particle shell has a shell thickness in a range between 5 micrometers and 12 micrometers.
31. The susceptor assembly according to claim 16, wherein the particle core is a sintered particle core, and wherein a material of the particle core is a sintered material.
32. The susceptor assembly according to claim 16, wherein a material of the particle shell is plated, deposited, coated, or cladded onto the particle core such as to form the particle shell.
33. An aerosol-generating article for an inductively heating aerosol-generating device, the aerosol-generating article comprising: at least one aerosol-forming substrate and a susceptor assembly according to claim 16, wherein the one or more susceptor particles of the susceptor assembly are embedded in the aerosol-forming substrate.
34. The aerosol-generating article according to claim 33, wherein the one or more susceptor particles of the susceptor assembly are distributed throughout the aerosol-forming substrate with a distribution gradient from a central axis of the aerosol-forming article to a periphery thereof.
35. An aerosol-generating system comprising an aerosol-generating article according to claim 16 and an inductively heating aerosol-generating device for the inductively heating aerosol-generating device.
Description
[0096] Examples will now be further described with reference to the figures in which:
[0097]
[0098]
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[0100]
[0101]
[0102] As regard the present invention, the aerosol-forming rod segment 110 comprises an aerosol-forming substrate 130 as well as a susceptor assembly 120 for heating the substrate 130 when being exposed to an alternating magnetic field. As can be seen in
[0103] As illustrated in
[0104]
[0105] According to the present invention, the magnetic core has another important function: Due its high magnetic permeability, the particle 121 acts as a flux concentrator which increases the magnetic flux through the particle shell 122. According to Faraday's law of induction, an increase of the magnetic flux causes an increase of eddy current losses in the particle shell 122. Hence, the high magnetic permeability of the magnetic particle core 121 increases the amount of heat generated in particle shell during use. Advantageously, this also allows to make the particle shell rather thin, and thus to save material and costs for the manufacturing of the susceptor particles.
[0106] When reaching about the Curie temperature of the core material, the magnetic properties of the particle core 121 change from ferrimagnetic to paramagnetic. As a consequence, the overall effective magnetic permeability of the magnetic particle core 121 drops to unity. This causes the heat generation in the particle core 121 to stop as the magnetic hysteresis of the core material disappears. Even more, the change in the magnetic permeability also affects the heat generation in the particle shell 122 as the decrease of the magnetic permeability of the magnetic particle core 121 causes a decrease of the magnetic flux through the electrically conductive particle shell 122. This in turn leads to a reduction of the electromotive force and thus to a reduction of heat generating eddy current losses in the particle shell 122, when the susceptor assembly reaches the Curie temperature of the core material.
[0107] In addition, the change in the magnetic permeability affects the heat generation in the particle shell 122 also because the decrease of the magnetic permeability causes an increase of the skin depth in the particle shell 122 as described further above. This in turn causes the effective resistance of the aluminum particle shell 122 to decrease. Hence, when reaching the Curie temperature of the core material, heat generation in the particle shell 122 is also reduced since the decrease of the effective resistance also causes a reduction of eddy current losses in the shell material.
[0108] Accordingly, at the Curie temperature, the heat generation by eddy current losses in the particle shell 122 is reduced due to both, a reduction of the magnetic flux through the particle shell and a reduction of the effective resistance of the shell material. In addition, the overall heat generation is reduced due to the hysteresis losses in the particle core 121 disappearing at the Curie temperature of the core material. In particular, the reduction of the overall heat generation results by itself, so that rapid overheating of the as aerosol-forming substrate can be effectively avoided, preferably without the need for an active temperature control.
[0109] Preferably, the specific core material is chosen such as to have a Curie temperature at about a predefined operating temperature of the susceptor assembly 120 at which the aerosol-forming substrate 130 is to be heated. For solid aerosol forming substrates containing tobacco material, the operating temperature may be in a range between 200 degree Celsius and 360 degree Celsius.
[0110] As be further seen in
[0111] The particle core may be manufactured may sintering a green body of the ferromagnetic or ferrimagnetic core material, and subsequently applying the shell material onto the particle core 121, for example, by vapor deposition such as to provide a particle shell 122 that is firmly bonded to the particle core 121.
[0112]
[0113] For the purpose of the present description and of the appended claims, except where otherwise indicated, all numbers expressing amounts, quantities, percentages, and so forth, are to be understood as being modified in all instances by the term “about”. Also, all ranges include the maximum and minimum points disclosed and include any intermediate ranges therein, which may or may not be specifically enumerated herein. In this context, therefore, a number A is understood as A ±5 percent of A. Within this context, a number A may be considered to include numerical values that are within general standard error for the measurement of the property that the number A modifies. The number A, in some instances as used in the appended claims, may deviate by the percentages enumerated above provided that the amount by which A deviates does not materially affect the basic and novel characteristic(s) of the claimed invention. Also, all ranges include the maximum and minimum points disclosed and include any intermediate ranges therein, which may or may not be specifically enumerated herein.