METHOD AND APPARATUS FOR THE OPTICAL CONTACT BONDING OF COMPONENTS
20240036345 ยท 2024-02-01
Inventors
- Stefan SCHUETTER (Herbrechtingen, DE)
- Eduard Schweigert (Syrgenstein, DE)
- Benjamin ROSS (Aalen, DE)
- Sebastian FAAS (Dornstadt, DE)
Cpc classification
B81C2203/038
PERFORMING OPERATIONS; TRANSPORTING
G02B27/62
PHYSICS
B81B1/006
PERFORMING OPERATIONS; TRANSPORTING
International classification
G02B27/62
PHYSICS
B81C3/00
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A method for optical contact bonding components includes: placing a first surface (2a) of a first component (2) onto a second surface (3a) of a second component (3), to form an air film, and pressing the first surface against the second surface for optical contact bonding of the two components. Placing and pressing the first component is carried out by a robot (4). A laminar gas flow (10) is generated between the first and second surfaces with a ventilation device (9). A related apparatus (1) includes: the robot, configured to place the first surface onto the second surface thereby forming an air film. The robot presses the first surface against the second surface, to optically contact bond the first and second components. A holding device (8) holds the second component during the placing and pressing. A ventilation device generates the laminar gas flow between the first and second surfaces.
Claims
1. A method for optical contact bonding of components, comprising: placing a first surface of a first component onto a second surface of a second component, thereby forming an air film, wherein said placing of the first component is carried out by robot, pressing the first surface of the first component against the second surface of the second component, thereby forming the optical contact bonding of the first component to the second component and generating a laminar gas flow between the first surface of the first component and the second surface of the second component with a ventilation device.
2. The method as claimed in claim 1, wherein said pressing of the first component is carried out by robot.
3. The method as claimed in claim 1, further comprising orienting the second component at an angle () with respect to a horizontal plane during said placing of the first component.
4. The method as claimed in claim 3, wherein the second component is oriented vertically with respect to the horizontal plane during said placing of the first component.
5. The method as claimed in claim 1, wherein the laminar gas flow is oriented at an angle () with respect to a horizontal plane.
6. The method as claimed in claim 1, further comprising, prior to said placing, bringing a subregion of the first surface of the first component into contact with the second surface of the second component.
7. The method as claimed in claim 6, wherein the subregion brought in contact with the second surface of the second component comprises a lateral edge of the first surface.
8. The method as claimed in claim 6, further comprising: detecting the contact between the subregion of the first surface and the second surface.
9. The method as claimed in claim 8, wherein said detecting of the contact between the subregion of the first surface and the second surface comprises exerting a torque on the robot by the second component.
10. The method as claimed in claim 6, wherein the first surface of the first component and the second surface of the second component are oriented at a predefined angle () with respect to one another during the contacting of the subregion.
11. The method as claimed in claim 6, wherein the first component is rotated about the subregion until the first surface of the first component abuts areally against the second surface of the second component.
12. The method as claimed in claim 1, further comprising: detecting an areal abutment of the first surface of the first component against the second surface of the second component.
13. The method as claimed in claim 12, wherein said detecting of an areal abutment comprises minimizing the torque exerted on the robot by the second component.
14. The method as claimed in claim 1, further comprising: detecting an interference fringe pattern of an air film formed between the first and the second surfaces areally abutting against one another.
15. The method as claimed in claim 14, wherein a pressing position, at which the first surface is pressed against the second surface, is defined in dependence on the detected interference fringe pattern.
16. The method as claimed in claim 14, wherein at least one parallel-oriented trench-like is formed on the first surface of the first component and/or on the second surface of the second component, and wherein an orientation of the first component during the areal abutment is selected in dependence on the orientation of the interference fringe pattern relative to a longitudinal direction (Y) of the at least one trench-like depression.
17. An apparatus for automated optical contact bonding of components, comprising: a robot configured to place a first surface of a first component onto a second surface of a second component, to form an air film, a holding device configured to hold the second component during said placing, and a ventilation device configured to generate a laminar gas flow between the first surface of the first component and the second surface of the second component.
18. The apparatus as claimed in claim 17, wherein the robot is further configured to press the first surface of the first component against the second surface of the second component, to thereby optically contact bond the first component to the second component.
19. The apparatus as claimed in claim 17, wherein the robot comprises at least one sensor, configured to detect the areal abutment of the first surface of the first component against the second surface of the second component.
20. The apparatus as claimed in claim 17, wherein the holding device is configured to orient the second component at an angle () with respect to a horizontal plane.
21. The apparatus as claimed in claim 17, wherein the ventilation device is configured to orient the laminar gas flow at an angle () with respect to a horizontal plane.
22. The apparatus as claimed in claim 17, further comprising: a spatially resolving detector configured to detect an interference fringe pattern of an air film formed between the first and the second surfaces areally abutting against one another.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0053] Exemplary embodiments are illustrated in the schematic drawing and are explained in the following description. In the figures:
[0054]
[0055]
[0056]
[0057]
[0058]
[0059]
[0060]
DETAILED DESCRIPTION
[0061] In the following description of the drawings, identical reference signs are used for identical or functionally identical components.
[0062]
[0063] The robot 4 comprises a gripping device in the form of a robot hand 6, which is connected to the rest of the robot 4 by way of a joint 7. Fastened to the robot hand 6 is the first component 2 which is intended to be optically contact bonded to the second component 3. The fastening or the holding of the first component can be effected with the aid of the robot hand 6.
[0064] The second component 3 is mounted on a holding device 8 vertically, i.e. at an angle of 90, relative to a horizontal plane X, Y, which corresponds to the support plane of the loading table 5. As a result of the vertical orientation of the second component 3, the accumulation of particles on a second surface 3a of the second component 3, said second surface being intended to be optically contact bonded to a first surface 2a of the first component 2, is reduced, since the particles are no longer able to abut against the vertically oriented second surface 3a.
[0065] In the case of the apparatus 1 shown in
[0066] The apparatus 1 also comprises a spatially resolving detector 14 in the form of a camera, which is mounted on a side of the second component 3 that faces away from the second surface 3a. The detector 14 allows the second surface 3a and also the first surface 2a to be observed through the second component 3. In the example shown, the second component 3, like the first component 2, is formed from titanium-doped quartz glass, more precisely from ULE, which is transparent to visible wavelengths, thus making the observation through the second component 3 possible. However, the first component 2 and the second component 3 may also be formed from other materials.
[0067] In the example shown in
[0068] As can be seen in
[0069] In the example shown, the robot 4 is controlled during the optical contact bonding operation described below by a control device 16 which also controls the loading of the apparatus 1 with first and/or second components 2, 3 with a loading device 17. The control device 16 is also connected to the detector 14 in terms of signaling and comprises an evaluation device in order to evaluate the image captured by the detector 14.
[0070] The method sequence during the optical contact bonding is explained below with reference to
[0071] First of all, the robot 4 is used to move the first component 2 closer to the second component 3 until a subregion 18 of the first surface 2a of the first component 2 bears against the second surface 3a. The subregion 18 of the first surface 2a is formed at the lateral edge of the first surface 2, as can be seen in
[0072] The first contact between the first surface 2a and the second surface 3a in the subregion 18 can be detected on the basis of a torque M, which is exerted on the first component 2 by the second component 3 and on the robot 4, more precisely on the longitudinal axis 19 of the robot hand 6 or on the joint 7, by said first component. As can be seen in
[0073] On the basis of the detected torque M, which is a vector quantity, the control device 19 can identify which direction or along which axis of rotation D the first component 2 has to be rotated in order to close the angle R and to place the first component 2 areally on the second component 3. Here, it is not absolutely necessary to know the direction of the torque M. The axis of rotation D during the rotation of the first component 2 is located in the subregion 18 in which the first contact takes place, i.e. the first component 2 is rotated about the already abutting subregion 18 or the corresponding contour at the edge of the first surface 2a.
[0074]
[0075] The areal abutment of the first surface 2a of the first component 2 against the second surface 3a of the second component 3 is also detected with the aid of the torque sensor 20 of the robot 4: The torque M exerted on the first component 2 by the second component 3 in the areally abutting position shown in
[0076] In the example shown, with the components 2, 3 areally abutting against one another, the optical contact bonding is triggered by virtue of the first surface 2a of the first component 2 being pressed against the second surface 3a of the second component 3 at a pressing position 24 which is formed at the circular, peripheral edge of the first surface 2a. The pressing position 24 is illustrated in
[0077] Also visible in
[0078] The direction of extent X of the interference fringes 23 is thus oriented perpendicularly with respect to the longitudinal direction Y of the trench-like depressions 15. This is favorable since a displacement wave, which displaces the air film 21 out of the intermediate space or out of the gap between the two surfaces 2a, 3a, propagates transversely with respect to the interference fringes 23, i.e. in the Y direction, as indicated by an arrow in
[0079] Both the pressing position 24 and the orientation of the first component 2 or of the first surface 2a relative to the second component 3 or to the second surface 3a are defined in dependence on the orientation of the interference fringe pattern 22, more precisely on the direction of extent X of the interference fringes 23 of the interference fringe pattern 22. Here, the orientation of the first component 2, more precisely of the first surface 2a, can be changed by small movements of the first component 2 with the aid of the robot 4 in such a way that the direction of extent X of the interference fringes 23 is oriented substantially perpendicularly with respect to the longitudinal direction Y of the trench-like depressions 15. This makes it possible for the displacement wave, which displaces the air film 21, to not impinge on the longitudinal side of one of the trench-like depressions 15, since in this case the displacement wave might be stopped at the trench-like depression 15. Such an orientation of the first component 2 is also possible if the trench-like depressions 15 are formed in the first component 2 instead of in the second component 3, or if both the first component 2 and the second component 3 comprise trench-like depressions 15.
[0080] Since the displacement wave propagates perpendicularly with respect to the interference fringes 23 of the interference fringe pattern 22, the pressing position 24 is selected at that position at the peripheral edge of the first surface 2a at which the surface 2a has its maximum extent perpendicularly with respect to the direction of extent X of the interference fringes 23. In the example shown in
[0081] The successful optical contact bonding of the two components 2, 3 can also be checked with the aid of the spatially resolving detector 14: if the optical contact bonding was successful, the interference fringe pattern 22 in the captured image should completely disappear. If this is not the case, the two components 2, 3 may possibly be released from one another again, if the robot 4 exerts a sufficiently great force on the components 2, 3. It is also possible for the step of placing the two components 2, 3 onto one another to be interrupted or restarted, e.g. if the torque M cannot be minimized as desired. In this case, it is for example possible for a different subregion 19, which establishes the first contact with the second surface 3a, of the first surface 2a to be selected, as a result of which the axis of rotation D about which the first component 2 is rotated changes.
[0082] The component part which is formed during the optical contact bonding of the two components 2, 3 and which, in the example shown, is a mirror or a substrate for a mirror can be unloaded with the aid of the robot 4. Here, the robot 4, more precisely the robot hand 6, can grip or hold the two components 2, 3. However, it is also possible for the robot 4 to grip the assembled component part only on the first component 2, if the connection formed during the optical contact bonding is stable enough.
[0083]
[0084] With the aid of the joints 7a, 7b, . . . , it is possible to also implement a controlled rotational or tilting movement of the first component 2 in addition to a translational movement of the first component 2 by virtue of the linear units 25a, 25b, . . . being deflected to different extents. The linear units 25a, 25b, . . . or the clamping devices 26a, 26b, . . . mounted thereon may possibly be precisely positioned with the aid of piezo actuators.
[0085] In order to measure the torque M exerted on the first component 2 by the second component 3, a respective torque sensor 20a, 20b, . . . (force-torque sensor) is mounted on a respective joint 7a, 7b, . . . of the robot 4, of which only two torque sensors 20a,b are illustrated in
[0086] The optical contact bonding of the two components 2, 3 which is described further above can be followed, for example, by a tempering step, in which a permanent connection between the two components 2, 3 is established; however, this is not absolutely necessary.
[0087]
[0088] During the fully automated optical contact bonding, the machine stations A to E are passed through successively. The first machine station A is an input station, at which the two components are introduced via an air lock into the interior space of the housing 13. It is for example possible to use a conveyor belt to transport the components into the interior space. The input station A of the apparatus 1 comprises an ultrafine cleaning installation, at which the surfaces of the components are clean. The ultrafine cleaning installation is configured to blow off particles deposited on the surfaces with the aid of compressed air. However, the ultrafine cleaning installation may also clean the surfaces in a different manner. The ultrafine cleaning of a respective component at the input station A can be effected without said component needing to be held by the handling device 27.
[0089] After the ultrafine cleaning has concluded, the respective component is transported with the aid of the handling device 27 to the second machine station B, at which an inspection device for automated pre-inspection of the respective component, more precisely of that surface of the component which is connected to the surface of the other component during the optical contact bonding process, is arranged. The inspection device may, for example, comprise a camera or the like, in order to inspect the respective surface. If it is determined during the inspection that the cleanliness of the surface is not sufficient for the subsequent optical contact bonding process, the component can be transported back to the ultrafine cleaning device at the input station A by the handling device 27 and the ultrafine cleaning can be repeated.
[0090] If the surface of the respective component has a sufficient surface quality, said component is transported by the handling device 27 to the third machine station C, at which an optical contact bonding module 28 for the optical contact bonding of the two components to one another is arranged, said module being described in more detail further below. During the optical contact bonding, a component part is formed from the two components, said component part being transported with the handling device 27 to a fourth machine station D, at which a further inspection device for post-inspection of the component part is arranged. For this purpose, the further inspection device may, for example, comprise a microscope which checks whether defects, e.g. inclusions in the form of air bubbles, were formed along a for example planar contact surface at which the two components 2, 3 were connected to one another during the optical contact bonding. The defects are quantified and qualified by the further inspection device with regard to number, position, size and possibly defect type. The information obtained during the inspection is stored by the further inspection device in a database which can be accessed by a machine operator located outside of the housing 13.
[0091] The component part assembled during the optical contact bonding is transported by the handling device 27 from the fourth machine station D to a fifth machine station E, which is an output station at which the component part is deposited and transported via an air lock out of the interior space of the housing 13.
[0092]
[0093] The optical contact bonding module 28 also comprises a robot 4 which, like the robot 4 shown in
[0094] As can be seen in
[0095] As can also be seen in
[0096] As has been described further above in conjunction with
[0097] As has been described further above in conjunction with
[0098] There are various possibilities for the implementation of the optical contact bonding process, of which four possibilities are indicated in highly schematic form in
[0099]
[0100] In the optical contact bonding process shown in
[0101] As has been described further above, the conclusion of the optical contact bonding process, in which the two components 2, 3 are completely connected to one another at a contact surface, can be detected on the basis of the disappearance of the interference fringe pattern 22, since in this case the air film between the two surfaces 2a, 3a has been completely displaced. If the interference fringe pattern 22 does not disappear, the optical contact bonding process can be terminated or the two components 2, 3 can be separated from one another again by the application of a counterforce.