METHOD FOR INTEGRALLY BONDING A GLASS ELEMENT TO A SUPPORT ELEMENT, AND OPTICAL DEVICE
20240343654 ยท 2024-10-17
Assignee
Inventors
Cpc classification
C04B2237/72
CHEMISTRY; METALLURGY
C03B23/20
CHEMISTRY; METALLURGY
C04B2237/592
CHEMISTRY; METALLURGY
C04B2237/64
CHEMISTRY; METALLURGY
C03C27/00
CHEMISTRY; METALLURGY
C03C3/06
CHEMISTRY; METALLURGY
International classification
C03B23/20
CHEMISTRY; METALLURGY
Abstract
A method of integrally bonding a glass element to a support element, the method comprising a step of inserting at least one contact element into a contact recess in a surface of the support element. In addition, the method comprises a step of placing the glass element on a portion of the contact element which portion protrudes beyond the surface, and a step of locally heating the contact element in order to connect the glass element to the support element via the contact element. The method also comprises a step of coating at least a part of the contact recess with a separating layer prior to the step of insertion.
Claims
1. A method of integrally bonding a glass element to a carrier element, the method comprising: inserting at least one contact element into a contact recess in a surface of the carrier element; placing the glass element on a portion of the contact element projecting above the surface; local heating of the contact element in order to connect the glass element to the carrier element via the contact element; and coating at least a part of the contact recess with a separating layer prior to the step of insertion.
2. The method according to claim 1, comprising a step of molding the contact recess prior to the step of insertion.
3. The method according to claim 1, wherein the separating layer is designed from silicon (Si) or germanium (Ge) or a refractory metal or an oxide of said substances or a refractory metal silicide.
4. The method according to claim 1, comprising a step of heating the contact element to connect the contact element to the carrier element, wherein the step of heating is performed after the step of insertion.
5. The method according to claim 4, wherein in the step of heating the portion of the contact element protruding above the surface is widened as a collar and/or formed as a rounded cap protruding in the direction of the glass plate normal.
6. The method according to claim 1, comprising a step of reducing a thickness of the portion prior to the step of placing, for leveling a surface of the portion.
7. The method according to claim 1, wherein in the step of insertion, the contact element is inserted using a reactive welding process.
8. The method according to claim 1, wherein in the step of locally heating the contact element is heated using a laser beam.
9. The method according to claim 1, wherein in the step of insertion the contact element is shaped cylindrical or spherical or partially spherical or ellipsoidal or toroidal.
10. The method according to claim 1, wherein in the step of local heating, the glass element and the support element are joined to produce an optical device.
11. The method according to claim 1, comprising a step of providing the carrier element in the form of a ceramic element and/or the glass element in the form of an ultra low expansion glass and/or the contact element in the form of a borosilicate cat glass element.
12. The method according to claim 1, wherein in the step of insertion, a plurality of contact elements are inserted into a plurality of contact recesses in the surface of the carrier element, wherein the plurality of contact recesses are arranged on a line.
13. The method according to claim 1, wherein in the step of local heating, a pressing force is exerted on the glass element to press the glass element against the contact element.
14. An optical device having a carrier element consisting of silicon carbide (SiC) or diamond or a mixture of silicon and silicon carbide (Si/SiC) and having a contact recess, particularly a reaction-bonded, silicon infiltrated silicon carbide material, or of boron carbide (B.sub.4C) or of silicon infiltrated boron carbide (Si/B.sub.4C) or of AlN and a glass element, wherein the carrier element and the glass element are firmly connected to one another using a contact element formed from a glass and inserted into the contact recess, wherein the contact recess is coated with a separating layer.
15. The optical device according to claim 14, comprising an optical sensor apparatus for detecting lengths and/or geometric positions.
Description
[0023] Exemplary embodiments of the approach presented here are shown in the drawings and explained in more detail in the following description. Shown are:
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[0033] In the following description of advantageous exemplary embodiments of the present invention, the same or similar reference characters are used for the elements that are shown in various figures and having a similar effect, wherein a repeated description of these elements is dispensed with.
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[0036] In one exemplary embodiment, the method 100 has a step 200 of providing the carrier element in the form of a ceramic element and the glass element in the form of an ultra low expansion glass and the contact element in the form of a borosilicate cat glass element. The contact element is made of borosilicate glass and the carrier element is made of Si/SiC ceramic. In this exemplary embodiment, the borosilicate glass has a different coefficient of thermal expansion between welding temperature and room temperature than the Si/SiC carrier element. For example, the coefficient of thermal expansion of the borosilicate glass is 3.25 ppm/K between room temperature and 300? C. and that of the Si/SiC is 4.0 ppm/K. In this exemplary embodiment, the contact element has relatively small dimensions so that the thermal expansion difference does not lead to the contact element tearing off the carrier element during cooling.
[0037] In one exemplary embodiment, the step 200 of providing is followed by a step 205 of forming the contact recess. The contact recess is only inserted into the carrier element by means of a bore, for example, and is matched to the dimensions of the contact element.
[0038] In one exemplary embodiment, the contact recess is subsequently coated with a separating layer in step 210 of the coating process. In this exemplary embodiment, the separating layer, which can also be referred to as a barrier layer, is designed with silicon in order to chemically separate the carrier element from the contact element. In another exemplary embodiment, the separating layer may, for example, additionally or alternatively have germanium (Ge) or a refractory metal or an oxide of said fabrics and additionally or alternatively a refractory metal silicide. In this exemplary embodiment, step 210 of coating is followed by step 105 of insertion of the contact element into the coated contact recess of the carrier element. In one exemplary embodiment, a plurality of contact recesses can also be formed in the surface of the carrier element in the forming step, into which a plurality of contact elements can be inserted in the insertion step. In this case, the plurality of contact recesses can be arranged in a line. For example, the plurality of contact recesses can be arranged in the form of a line seam along a closed curve, such as a circle, or along a rectangular shape.
[0039] In one exemplary embodiment, the step 105 of insertion is followed by a step 215 of heating the contact element in order to connect the contact element to the carrier element. For example, the contact element and optionally also the carrier element are heated to a connection temperature that enables a material-locking connection between the contact element and the carrier element. By way of example only, the heating step 215 is performed as a furnace process using a normal melting furnace. In another exemplary embodiment, heating can be performed using a vacuum furnace or by means of a laser beam. In this exemplary embodiment, a portion of the contact element protruding above the surface of the carrier element is expanded as a collar by heating, in which it is merely melted by way of example. Subsequently, the component is cooled in this exemplary embodiment in order to permanently connect the contact element to the carrier element. Since the borosilicate glass element and the Si/SiC ceramic element in this exemplary embodiment have different thermal expansion coefficients, the step 215 of heating, including cooling to only a room temperature of, for example, 20? C., can nevertheless be performed with substantially low mechanical stress by using contact elements of small dimensions. In another exemplary embodiment, mechanical stresses or unevenness can be caused by soldering. During soldering, for example, the totality of the component can be heated to the soldering temperature. When cooling to room temperature, the joining position can be fixed at the solidification temperature of the solder, so that if the expansion coefficients of the soldered parts differ, a thermally induced stress is created by the cooling, which can lead to bending of the surface. The effect is equivalent to bonding, wherein the solidification temperature of the solder can correspond to the glass transition temperature of the adhesive.
[0040] In one exemplary embodiment, in the method 100 shown here, the heating step 215 is followed by a reducing step 220. For example, only one thickness of the portion of the cooled contact element protruding above the surface of the carrier element is ground and polished, resulting in a flat surface of the contact element. This removes any remaining deformation of the surface of the contact element. In an exemplary embodiment with a plurality of contact elements, the surfaces of several existing contact elements can also be leveled into a common plane. A flatness of less than 1 ?m is only achieved as an example. The glass element is placed on this flat surface facing away from the carrier element in the following step 110.
[0041] This is followed by step 115 of local heating to connect the glass element to the carrier element via the contact element. Thereby, in this exemplary embodiment, the step 115 of localized heating is performed using a laser beam. Here, the laser beam is only guided over the surface of the contact element, for example, in order to securely connect the contact element to the glass element. At the same time, in this step 115 of local heating, a pressure force is exerted on the glass element in order to press the glass element against the contact element. The pressure force can be exerted over the entire surface, for example by placing another glass element on the glass element, or only locally in the area of the contact element(s). In this exemplary embodiment, the glass element has a lower coefficient of thermal expansion than the carrier element, although this does not lead to any mechanical stress due to the point-shaped connection between the glass element and the carrier element, which is only created by local heating.
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