Stress reduction during laser resealing through a temperature increase
11084716 · 2021-08-10
Assignee
Inventors
Cpc classification
B81C1/00293
PERFORMING OPERATIONS; TRANSPORTING
B81C1/00119
PERFORMING OPERATIONS; TRANSPORTING
B81C2203/0145
PERFORMING OPERATIONS; TRANSPORTING
B81B7/02
PERFORMING OPERATIONS; TRANSPORTING
International classification
B81C1/00
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A method for producing a micromechanical component having a substrate and a cap that are connected to each other and that enclose a first cavity, where a first pressure prevails inside the first cavity and a first gas mixture having a first chemical composition is enclosed within the first cavity, includes, in a first method step, developing in the substrate or cap an access opening connecting the first cavity to an environment of the micromechanical component, in a second method step, setting the first pressure and/or the first chemical composition in the first cavity, in a third method step, sealing the access opening using a laser by introduction of energy or heat into an absorbing part of the substrate or the cap, and, in a fourth method step, performing a thermal treatment of the substrate or the cap, thereby reducing temperature gradients in the substrate or in the cap.
Claims
1. A method for producing a micromechanical component that includes a substrate and a cap that are connected to each other and that enclose a first cavity, a first pressure prevailing in the first cavity, and a first gas mixture having a first chemical composition being enclosed within the first cavity, the method comprising: in a first step, forming in the substrate or in the cap an access opening that connects the first cavity to an environment external to the micromechanical component; in a second method step, setting at least one of the first pressure and the first chemical composition in the first cavity; in a third method step, laser sealing the access opening by introducing energy or heat into an absorbing part of the substrate or the cap, thereby liquefying the absorbing part, the liquefied absorbing part thereafter cooling and solidifying; and in a fourth method step, which is carried out temporally at least one of before, during, and after the third method step, performing a thermal treatment of the substrate or the cap at least in a region that is adjacent to the absorbing part and that does not liquefy in the third method step, the thermal treatment reducing temperature gradients in the substrate or in the cap between the absorbing part and the region that is adjacent to the absorbing part.
2. The method of claim 1, wherein the thermal treatment includes raising a temperature of an entirety of the substrate or the cap.
3. The method of claim 1, wherein the thermal treatment is carried out on a heating plate.
4. The method of claim 1, wherein the thermal treatment is carried out using a spatially restricted heat source.
5. The method of claim 1, wherein the thermal treatment is carried out using at least one of a laser, a light-emitting diode (LED), a laser diode, and a flash lamp.
6. The method of claim 1, wherein the thermal treatment is performed includes raising the temperature of only the region that is adjacent to the absorbing part, the region consisting of a surface of the substrate or the cap that faces away from the first cavity.
7. The method of claim 1, wherein the thermal treatment is carried out using a homogenous irradiation.
8. The method of claim 1, wherein the fourth method step is carried out before the third method step.
9. The method of claim 1, wherein the fourth method step is carried out during the third method step.
10. The method of claim 1, wherein the fourth method step is carried out after the third method step.
11. The method of claim 1, further comprising, in a fifth method step that is carried out prior to the first method step, bonding the substrate and the cap to each other.
12. The method of claim 1, further comprising, in a fifth method step that is carried out after the first method step, bonding the substrate and the cap to each other.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1)
(2)
(3)
DETAILED DESCRIPTION
(4)
(5) For example, a first pressure prevails inside first cavity 5, especially if access opening 11 is sealed, as shown in
(6) It is provided, for instance, that the first pressure in first cavity 5 be lower than the second pressure in the second cavity. It is also provided, for example, that a first micromechanical sensor unit for a rotation-rate measurement, which is not shown in
(7)
(8) Temporally after third method step 103, mechanical stresses can occur in a lateral region 15, exemplarily shown in
(9)
(10) For example, it is provided that the thermal treatment be carried out with the aid of a heat source. According to the present invention, for instance, the term ‘heat source’ encompasses all devices that are capable of allowing for the introduction of the further energy or the further heat into the substrate or into the cap.
(11) In addition, it is provided, for instance, that, in fourth method step 104, substrate 3 and cap 7, a lateral region 15 at a surface of substrate 3 or cap 7 that faces away from first cavity 5, or an environment of the welding spot is brought to a higher temperature. It is also provided, for instance, that multiple substrates 3 or caps 7 or micromechanical components 1 of a wafer are brought to a higher temperature in fourth method step 104. It is likewise provided, for example, that multiple wafers of a wafer stack are brought to a higher temperature in fourth method step 104.
(12) In the event that substrate 3 and cap 7 are brought to a higher temperature, it is provided, for instance, that the thermal treatment be carried out on a heating plate and/or using homogeneous irradiation.
(13) In the event that multiple substrates 3 or caps 7 or micromechanical components 1 of a wafer or of multiple wafers of a wafer stack are brought to a higher temperature, it is provided, for example, that the thermal treatment be carried out on a heated wafer coating and/or using homogeneous irradiation, e.g., during third method step 103.
(14) In the event that lateral region 15 is brought to the higher temperature, it is provided, for example, that the thermal treatment be performed using a spatially restricted heat source or a heat source that is locally restricted in space. In other words, it is provided, for example, that the further absorbing part of substrate 3 or cap 7 be developed locally, e.g., locally around access opening 11, for instance. In this context, it is provided that the thermal treatment be carried out using a further laser, a light-emitting diode (LED), a laser diode, and/or a flash lamp, for example. This advantageously allows for a locally restricted temperature increase. For instance, it is provided here that the energy or heat be introduced in third method step 103 using a laser pulse or multiple laser pulses of the laser or using a welding pulse of the laser. It is provided, for example, that the thermal treatment be carried out temporally before, during, and/or after the welding pulse, so that a three-dimensionally restricted heating of the welding-spot environment or a three-dimensionally restricted further absorbing part of substrate 3 or cap 7 is induced. For example, it is alternatively or additionally provided that a one-dimensionally restricted direct heat introduction be achieved, e.g., using a large-surface and pulsed illumination of substrate 3 or the cap using a flash lamp or multiple flash lamps, for example. In the context of the present invention, a one-dimensionally restricted heat introduction, for instance, means that the heat introduction into the depth of the substrate or the cap is restricted, in the sense of a surface of the substrate or the cap that is facing away from the first cavity, and in the direction of the first cavity. In other words, the meaning of a one-dimensionally restricted heat introduction, for instance, is that the wafer or the substrate or the cap is superficially heated, such as on a surface of the substrate or the cap that faces away from the first cavity. In this context, it is provided that the surface be heated across its full extension, for instance.
(15) As a result, the present invention provides a global and/or a local temperature management of the substrate and/or the cap, in which the stresses left behind in the component by the temperature management are able to be reduced in comparison with the related art.
(16) For instance, it is provided that the temperature management includes a reduction of temperature gradients in the substrate and/or the cap. The reduction of the temperature gradients in the substrate and/or in the cap in this instance is achieved through a global increase of the substrate temperature and/or through a local increase of the temperature in the environment of the welding spot immediately prior to, during, and/or immediately following the third method step, for example. As a result, the present invention provides a particularly simple and cost-effective method that makes it possible to avoid a component failure due to tears, or to minimize the likelihood of a component failure as a result of tears.