SEALING DEVICE, COMPONENT AND LITHOGRAPHY APPARATUS

The present invention relates to a sealing device for a lithography apparatus, to a component for a lithography apparatus comprising a sealing device of this type, and to a lithography apparatus comprising a sealing device of this type and/or a component of this type.

The content of the priority apphcation DE 10 2019 204 699.1 is incorporated by reference in its entirety.

Microlithography is used for producing microstructured components, for example integrated circuits. The microlithography process is performed using a lithogra phy apparatus, which has an illumination system and a projection system. The image of a mask (reticle) illuminated by means of the illumination system is in this case projected by means of the projection system onto a substrate (for exam ple a silicon wafer) which is coated with a light-sensitive layer (photoresist) and arranged in the image plane of the projection system, in order to transfer the mask structure to the light-sensitive coating of the substrate.

Driven by the desire for ever smaller structures in the production of integrated circuits, currently under development are EUV lithography apparatuses that use light with a wavelength in the range from 0.1 nm to 30 nm, in particular 13.5 nm. In the case of such EUV lithography apparatuses, because of the high ab sorption of light of this wavelength by most materials, reflective optical units, that is to say mirrors, have to be used instead of - as previously - refractive opti cal units, that is to say lens elements.

An EUV lithography apparatus as explained above comprises components having a cooling circuit, for example for cooling the respective component with water, or a purging circuit, for example for purging the respective component with a purge gas, in particular with an inert gas. A component of this type can be a so-called actuation sensor unit, for example, with the aid of which facets of a facet mirror, for example of a field facet mirror or of a pupil facet mirror, can be deflected. In this case, a so-called actuation sensor package is assigned to each facet for the purpose of deflecting the facets. The actuation sensor packages should be sealed in a fluid-tight manner vis-a-vis a main body or frame of the actuation sensor unit.

For seahng purposes, O-rings or sealing mats can be used as seals. In order to maintain the sealing function during operation and over the lifetime, the seal can be clamped onto the respective actuation sensor package by means of prestress or in a manner supported in the pressure direction. A centring of the seal can be ob tained as a result. In this case, it should be taken into consideration that the seal requires a yielding volume for the purpose of pressing it. Said yielding volume can be created by keeping enough space available between an inner contour of the respective seal and the actuation sensor package. However, this space is in turn disadvantageous with regard to a good centring of the seal.

Against this background, it is an object of the present invention to provide an im proved sealing device.

Accordingly, a sealing device for sealing a first component part of a lithography apparatus vis-a-vis a multiphcity of second component parts of the hthography ap paratus is proposed. The seahng device comprises a multiplicity of sealing rings, and a multiphcity of connection locations, wherein the sealing rings are connected to one another with the aid of the connection locations.

By virtue of the fact that the sealing rings are connected to one another with the aid of the connection locations, the mounting of the sealing device is simplified compared to a sealing device without such connection locations.

The sealing device can also be referred to as a seahng mat. Preferably, a multiplic ity of sealing rings is provided which form a two-dimensional pattern or grid. That is to say that the sealing rings are arranged in particular in the shape of a grid or in the shape of a pattern. Preferably, a plurality of connection locations, for exam ple four, are assigned to each seahng ring. The connection locations can also be referred to as contact locations. Preferably, the sealing rings are connected to one another integrally, in particular materially in one piece, with the aid of the con nection locations.“Integrally” means in the present case that the sealing rings to gether form a common component part, namely the sealing device.“Materially in one piece” means here that the sealing device is produced from the same material throughout. Preferably, the sealing device is produced from a plastics material. By way of example, a perfluoro rubber (FFKM) can be used as suitable material. The sealing device can be cut out from a sheet or film of a suitable plastics material with the aid of a laser, for example.

In accordance with one embodiment, the connection locations each comprise a yielding volume for pressing the respective sealing ring between the first compo nent part and one of the second component parts.

By virtue of the fact that the yielding volume is provided, it is possible for the respective seahng ring always to be sufficiently pressed, with the result that leaks during mounting and also over the service life of the lithography apparatus can be prevented or at least significantly reduced. The yielding volume can be provided between an inner contour of the respective sealing ring and a second component part received in the inner contour. However, the yielding volume can also be pro vided directly in or at the respective connection location, for example in the form of a cutout, a groove, a hole or the hke. All that is relevant here is that material of the sealing ring is pressed into the yielding volume during the pressing of the re spective sealing ring. The abovementioned inner contour of the sealing ring can have an arbitrary shape. The inner contour can be circular, oval, triangular, polyg onal or the like. Furthermore, the inner contour - as will be explained below - can also be trefoiled. The yielding volume is provided in particular in or at the sealing device itself.

In accordance with a further embodiment, each sealing ring comprises an inner contour, in each of which a second component part is able to be received at least in sections, and wherein the yielding volume is formed by virtue of the inner contour widening at the connection locations.

The fact that the inner contour“widens” means in the present case that the inner contour, at least in an unpressed state of the respective sealing ring, does not bear against the corresponding second component part and thus stands away from the second component part, in particular. By virtue of the fact that the inner contour widens at the connection locations, a sufficiently large yielding volume for the pressing of the respective seahng ring can be provided at the connection locations.

In accordance with a further embodiment, the inner contour comprises a connec tion radius at the connection locations, wherein the inner contour comprises an intermediate radius in each case between two adjacent connection locations, and wherein the intermediate radius and the connection radius differ from one another in terms of their absolute value in such a way that the inner contour widens at the connection locations and narrows between two adjacent connection locations.

By virtue of the fact that the inner contour narrows between two adjacent connec tion locations, a centring of the seahng rings at the respective intermediate radius is made possible. Thus, with the aid of the widening and the narrowing, it is pos sible simultaneously to ensure a sufficiently large yielding volume for the pressing of the sealing rings and a centring of the sealing rings at the second component parts.

In accordance with one preferred embodiment of the seahng device, the latter com prises a multiplicity of sealing rings, a multiplicity of connection locations, wherein the sealing rings are connected to one another with the aid of the connection loca tions, wherein each sealing ring comprises an inner contour, in each of which a second component part is able to be received at least in sections, wherein the inner contour comprises a connection radius at the connection locations, wherein the in ner contour comprises an intermediate radius in each case between two adjacent connection locations, and wherein the intermediate radius and the connection ra dius differ from one another in terms of their absolute value in such a way that the inner contour widens at the connection locations and narrows between two adja cent connection locations.

The inner contour is composed of a plurality of radii, in particular. That is to say that the inner contour is preferably not circular. The inner contour can also have any other geometry, as mentioned above. In the region of the connection locations, the inner contour has a widening or broadening and, in the region between the connection locations, the inner contour has a narrowing, constriction or restriction. This results in a trefoiled or trefoil-like geometry of the inner contour, deviating from the circular shape. The inner contour can therefore be referred to as“tre- foiled” or“trefoil-like”. The sealing device is positioned in particular between a sealing surface of the first component part and a seahng surface of the second com ponent part and effects fluid-tight sealing vis-a-vis them.

The fact that the second component part is“able to be received” in the inner con tour should be understood in the present case to mean that a respective sealing ring can be put onto the second component part, or vice versa. In this case, the second component part preferably has a circular-cylindrical base section, at which the sealing ring is centred with the aid of the intermediate radius.

Preferably, as mentioned above, four connection locations are provided. Accord ingly, the inner contour also has four times the connection radius and four times the intermediate radius. Accordingly, there are, in particular, also four pairs of adjacent connection locations, between each of which a connection radius is pro vided. The radii transition into one another, such that the inner contour has no shoulders, but rather a curved shape.

The fact that the intermediate radius and the connection radius“differ” from one another should be understood to mean, in particular, that the intermediate radius is greater than the connection radius, or vice versa. A centre point of the connection radius can be offset relative to a centre point of the intermediate radius in such a way that the condition that the inner contour widens at the connection locations and narrows between two adjacent connection locations is met both if the connec tion radius is greater than the intermediate radius and if the connection radius is less than the intermediate radius.

In accordance with a further embodiment, the intermediate radius is greater than the connection radius.

By way of example, the connection radius is approximately 5 mm. The intermedi ate radius can be approximately 11 to 12 mm. In accordance with a further embodiment, the inner contour comprises a first in ^¬ termediate radius and a second intermediate radius, wherein the first intermedi ^¬ ate radius and the second intermediate radius are equal in magnitude or have dif ^¬ ferent magnitudes.

Preferably, the first intermediate radius is greater than the second intermediate radius. Alternatively, the first intermediate radius can also be less than the second intermediate radius. With the aid of the different intermediate radii, it is possible, if the connection locations are positioned in a manner spaced apart from one an ^¬ other at different azimuth angles in an azimuth direction or circumferential direc ^¬ tion, to take account of the fact that a shortening of the sealing ring by the factor of azimuth angle/360 ^o is to be produced between two connection locations in order, during the mounting of the sealing device, to prevent the connection locations from moving azimuthally, which could otherwise lead to warpage of the sealing device. For the case where the azimuth angles are equal in magnitude, the first interme ^¬ diate radius and the second intermediate radius are preferably also equal in mag ^¬ nitude. Preferably, the connection locations are constructed in each case symmet ^¬ rically with respect to a line of symmetry assigned to the respective connection location. The azimuth angles are measured between the lines of symmetry of the connection locations. A respective centre point of the connection radius lies on the line of symmetry of that connection location to which the connection radius is as ^¬ signed.

In accordance with a further embodiment, the second intermediate radius has a bigger magnitude than the first intermediate radius.

Alternatively, the second intermediate radius can also have a smaller magnitude than the first intermediate radius.

In accordance with a further embodiment, two adjacent connection locations be ^¬ tween which the first intermediate radius is provided and two adjacent connection locations between which the second intermediate radius is provided are arranged in a manner spaced apart at the same distance or at different distances from one another. Preferably, the connection locations are positioned in a manner spaced apart from one another non-uniformly as viewed in the circumferential direction. That is to say that different azimuth angles are provided between the connection locations. In this case, the first intermediate radius is positioned between a pair of connection locations between which a smaller azimuth angle is provided. The second interme diate radius is provided between a pair of connection locations between which a larger azimuth angle is provided. For the case where the azimuth angles are equal in magnitude, the connection locations are also arranged in a manner spaced apart at an equal distance from one another.

In accordance with a further embodiment, a centre point of the intermediate radius is arranged offset relative to a centre point of the connection radius.

Preferably, the sealing ring comprises a first plane of symmetry and a second plane of symmetry, with respect to which the sealing ring is constructed symmetrically. The planes of symmetry are positioned perpendicularly to one another, in particu lar. The centre point of the intermediate radius is positioned eccentrically. The centre point of the connection radius is also positioned eccentrically. As mentioned above, the centre point of the connection radius lies on the respective line of sym metry of the connection location.

In accordance with a further embodiment, a centre point of the first intermediate radius is arranged offset relative to the centre point of the connection radius in an x-direction and a ydirection of the sealing ring, wherein a centre point of the sec ond intermediate radius is arranged offset relative to the centre point of the con nection radius in the x-direction and in the ydirection of the sealing ring.

In particular, a coordinate system having a first spatial direction or x-direction, a second spatial direction or ydirection and a third spatial direction or z- direction is assigned to the sealing ring. The spatial directions are positioned perpendicularly to one another. The first plane of symmetry is spanned by the ydirection and the z-direction, in particular. The second plane of symmetry is spanned by the x-direc tion and the z-direction, in particular. The inner contour runs in particular as two- dimensional geometry in the x-direction and the ydirection. The centre point of the first intermediate radius is positioned offset relative to the centre point of the connection radius in the x- direction and the y direction in particular in such a way that the inner contour experiences a constriction in the region of the first interme diate radius, even though the first intermediate radius is greater than the connec tion radius. In particular, the centre point of the second intermediate radius is positioned offset relative to the centre point of the connection radius in the x-direc- tion and in the ydirection in such a way that the inner contour experiences a con striction in the region of the second intermediate radius, even though the second intermediate radius is preferably greater than the connection radius.

In accordance with a further embodiment, centre points of two first intermediate radii are arranged in a manner spaced apart from one another by a first distance in the ydirection, wherein centre points of two second intermediate radii are ar ranged in a manner spaced apart from one another by a second distance in the x- direction, and wherein the first distance and the second distance are equal in mag nitude or have different magnitudes.

In particular, the centre points of the two first intermediate radii are positioned in the first plane of symmetry and outside the second plane of symmetry. Preferably, the centre points are positioned mirror-symmetrically with respect to the second plane of symmetry. In particular, the centre points of the two second intermediate radii are positioned in the second plane of symmetry and outside the first plane of symmetry. Preferably, the centre points of the second intermediate radii are posi tioned mirror-symmetrically with respect to the first plane of symmetry. For the case where the azimuth angles are equal in magnitude, the first distance and the second distance are preferably equal in magnitude.

In accordance with a further embodiment, the first intermediate radii and the sec ond intermediate radii are arranged alternating along the inner contour.

This means that seen along the inner contour, each first intermediate radius is arranged between two second intermediate radii and vice versa. The two first in termediate radii are arranged vis-a-vis or with a peripheral angle of 180°. The same can be valid for the second intermediate radii. In accordance with a further embodiment, the inner contour comprises a transition radius, wherein the intermediate radius transitions into the connection radius with the aid of the transition radius.

This ensures a continuously variable transition from the intermediate radius to the transition radius. Preferably, the transition radius is less than the intermedi ^¬ ate radius and the connection radius.

In accordance with a further embodiment, two yielding volumes are provided per connection location, wherein a connection web of the connection location is pro ^¬ vided between the two yielding volumes, and wherein the connection web connects adjacent sealing rings to one another.

In particular, the connection web connects the sealing rings to one another inte ^¬ grally, in particular materially in one piece.

In accordance with a further embodiment, the yielding volume is a groove which completely penetrates through a wall thickness of the seahng device or which ex ^¬ tends only to a defined depth into the wall thickness.

For the case where the groove penetrates through the wall thickness only to the defined depth, the groove can be rectangular or rounded in cross section. If the groove does not completely penetrate through the wall thickness, said groove can also extend through the connection web. The groove can comprise sidewalls run ^¬ ning parallel to one another. The sidewalls can also be positioned obliquely with respect to one another, such that the groove is wedge-shaped.

In accordance with a further embodiment, the yielding volume comprises a multi ^¬ plicity of holes which completely penetrate through a wall thickness of the seahng device or which extend only to a defined depth into the wall thickness.

The holes can all have the same diameter or different diameters. The holes can be arranged in a manner spaced apart from one another uniformly or non-uniformly. The holes can be arranged in one row or a plurahty of rows. Furthermore, a component for a lithography apparatus is proposed. The compo nent comprises a first component part, a multiplicity of second component parts which are received at least in sections in the first component part, and a sealing device of this type.

By way of example, the component can be part of a beam shaping and illumination system or of a projection system of the lithography apparatus. The component can be a so-called Actuation Sensor Unit (ASU), for example, with the aid of which facets of a facet mirror, for example of a field facet mirror or of a pupil facet mirror, can be deflected. Such a facet mirror having deflectable facets can be part of the beam shaping and illumination system, for example. The first component part can be for example a main body or frame of the component. The first component part can comprise a cooling system for cooling the component, in particular the second component parts. The cooling system can be formed with the aid of cooling chan nels provided in the first component part. The second component part can be an Actuation Sensor Package (ASP), for example, which is suitable for deflecting a facet of a facet mirror as mentioned above. The second component parts can have a circular-cylindrical geometry at least in sections. With the aid of the sealing de vice, the second component parts are sealed vis-a-vis the first component part in order to seal the cooling system with respect to surroundings of the component.

In accordance with one embodiment, the sealing rings are pressed in each case between the first component part and one of the second component parts in such a way that a respective yielding volume of the sealing device is at least partly filled with material of the respective seahng ring.

During the pressing of the sealing ring, the latter is pressed at least partly into the yielding volume. A permanent safeguard against leaks is achieved as a result.

In accordance with one preferred embodiment, the component comprises a first component part, a multiplicity of second component parts which are received in the first component part at least in sections, a sealing device as explained above, wherein the inner contour, for the purpose of centring the respective sealing ring at one of the second component parts, bears against the second component part with the intermediate radius, and wherein the inner contour, for the purpose of providing a yielding volume between the inner contour and the second component part, stands away from the second component part at the connection radius.

The fact that the inner contour“stands away” from the second component part at the connection radius for the purpose of providing the yielding volume should be understood to mean, in particular, that the inner contour does not make contact with the second component part in the region of the connection radius. That is to say that the inner contour and the second component part are free of contact or do not touch at the connection radius.

Furthermore, a lithography apparatus is proposed. The lithography apparatus con comitantly comprises a sealing device as explained above and/or a component as explained above.

The lithography apparatus can be an EUV lithography apparatus or a DUV li thography apparatus. EUV stands for“extreme ultraviolet” and denotes a wave length of the working hght of between 0.1 nm and 30 nm. DUV stands for“deep ultraviolet” and denotes a wavelength of the working light of between 30 nm and 250 nm.

“A(n); one” in the present case should not necessarily be understood as restrictive to exactly one element. Rather, a plurahty of elements, such as, for example, two, three or more, can also be provided. Any other numeral used here, too, should not be understood to the effect that there is a restriction to exactly the stated number of elements. Rather, numerical deviations upwards and downwards are possible, unless indicated to the contrary.

The embodiments and features described for the sealing device are correspond ingly applicable to the proposed component and respectively to the proposed li thography apparatus, and vice versa.

Further possible implementations of the invention also comprise not explicitly mentioned combinations of features or embodiments that are described above or below with respect to the illustrative embodiments. In this case, a person skihed in the art will also add individual aspects as improvements or supplementations to the respective basic form of the invention.

Further advantageous configurations and aspects of the invention are the subject matter of the dependent claims and also of the exemplary embodiments of the in vention described below. In the text that follows, the invention is explained in more detail on the basis of preferred embodiments and with reference to the ac companying figures.

Fig. 1A shows a schematic view of one embodiment of an EUV lithography appa ratus;

Fig. IB shows a schematic view of one embodiment of a DUV lithography appa ratus;

Fig. 2 shows a schematic view of one embodiment of a component for the lithogra phy apparatus in accordance with Fig. 1A or Fig. IB;

Fig. 3 shows a schematic sectional view of the component in accordance with the sectional line III-III in Fig. 2;

Fig. 4 shows the detail view IV in accordance with Fig. 3;

Fig. 5 shows a further schematic sectional view of the component in accordance with the sectional line V-V in Fig. 2;

Fig. 6 shows the detail view VI in accordance with Fig. 5;

Fig. 7 shows a schematic view of one embodiment of a sealing device for the com ponent in accordance with Fig. 2;

Fig. 8 shows the detail view IIX in accordance with Fig. 7;

Fig. 9 shows the detail view IX in accordance with Fig. 7 ; Fig. 10 shows a schematic sectional view of the sealing device in accordance with the sectional line X-X in Fig. 9;

Fig. 11 shows a schematic sectional view of a further embodiment of a seahng de ^¬ vice for the component in accordance with Fig. 2;

Fig. 12 shows a schematic detail view of a further embodiment of a seahng device for the component in accordance with Fig. 2;

Fig. 13 shows a schematic detail view of a further embodiment of a seahng device for the component in accordance with Fig. 2; and

Fig. 14 shows a schematic detail view of a further embodiment of a seahng device for the component in accordance with Fig. 2.

Identical elements or elements having an identical function have been provided with the same reference signs in the figures, unless indicated to the contrary. It should also be noted that the illustrations in the figures are not necessarily true to scale.

Fig. 1A shows a schematic view of an EUV lithography apparatus 100A, which comprises a beam shaping and illumination system 102 and a projection system 104. In this case, EUV stands for“extreme ultraviolet” and denotes a wavelength of the working hght of between 0.1 nm and 30 nm. The beam shaping and illumi ^¬ nation system 102 and the projection system 104 are respectively provided in a vacuum housing (not shown), each vacuum housing being evacuated with the aid of an evacuation device (not shown). The vacuum housings are surrounded by a machine room (not shown), in which drive devices for mechanically moving or set ^¬ ting optical elements are provided. Moreover, electrical controllers and the like can also be provided in this machine room.

The EUV lithography apparatus 100A comprises an EUV light source 106A. A plasma source (or a synchrotron), which emits radiation 108A in the EUV range (extreme ultraviolet range), that is to say for example in the wavelength range of 5 nm to 20 nm, can for example be provided as the EUV hght source 106A. In the beam shaping and illumination system 102, the EUV radiation 108A is focused and the desired operating wavelength is filtered out from the EUV radiation 108A. The EUV radiation 108A generated by the EUV light source 106A has a relatively low transmissivity through air, for which reason the beam guiding spaces in the beam shaping and illumination system 102 and in the projection system 104 are evacuated.

The beam shaping and illumination system 102 illustrated in Fig. 1A has five mirrors 110, 112, 114, 116, 118. After passing through the beam shaping and illu ^¬ mination system 102, the EUV radiation 108A is guided onto a photomask (called a reticle) 120. The photomask 120 is likewise embodied as a reflective optical ele ^¬ ment and can be arranged outside the systems 102, 104. Furthermore, the EUV radiation 108A can be directed onto the photomask 120 by means of a mirror 122. The photomask 120 has a structure which is imaged onto a wafer 124 or the like in a reduced fashion by means of the projection system 104.

The projection system 104 (also referred to as projection lens) has six mirrors Ml to M6 for imaging the photomask 120 onto the wafer 124. In this case, individual mirrors Ml to M6 of the projection system 104 can be arranged symmetrically in relation to an optical axis 126 of the projection system 104. It should be noted that the number of mirrors Ml to M6 of the EUV lithography apparatus 100 A is not restricted to the number represented. A greater or lesser number of mirrors Ml to M6 can also be provided. Furthermore, the mirrors Ml to M6 are generally curved on their front face for beam shaping.

Fig. IB shows a schematic view of a DUV lithography apparatus 100B, which comprises a beam shaping and illumination system 102 and a projection system 104. In this case, DUV stands for“deep ultraviolet” and denotes a wavelength of the working light of between 30 nm and 250 nm. As has already been described with reference to Figure 1A, the beam shaping and illumination system 102 and the projection system 104 can be arranged in a vacuum housing and/or sur ^¬ rounded by a machine room with corresponding drive devices. The DUV lithography apparatus 100B has a DUV light source 106B. By way of example, an ArF excimer laser that emits radiation 108B in the DUV range at 193 nm, for example, can be provided as the DUV light source 106B.

The beam shaping and illumination system 102 illustrated in Fig. IB guides the DUV radiation 108B onto a photomask 120. The photomask 120 is embodied as a transmissive optical element and can be arranged outside the systems 102, 104. The photomask 120 has a structure which is imaged onto a wafer 124 or the like in a reduced fashion by means of the projection system 104.

The projection system 104 has a plurality of lens elements 128 and/or mirrors 130 for imaging the photomask 120 onto the wafer 124. In this case, individual lens elements 128 and/or mirrors 130 of the projection system 104 can be ar ^¬ ranged symmetrically in relation to an optical axis 126 of the projection system 104. It should be noted that the number of lens elements 128 and mirrors 130 of the DUV hthography apparatus 100B is not restricted to the number repre ^¬ sented. A greater or lesser number of lens elements 128 and/or mirrors 130 can also be provided. Furthermore, the mirrors 130 are generally curved on their front face for beam shaping.

An air gap between the last lens element 128 and the wafer 124 can be replaced by a liquid medium 132 which has a refractive index of > 1. The liquid medium 132 can be high -purity water, for example. Such a construction is also referred to as immersion lithography and has an increased photolithographic resolution. The medium 132 can also be referred to as an immersion liquid.

Fig. 2 shows a plan view of a component 200 for an EUV lithography apparatus 100A as explained above. By way of example, the component 200 can be part of the beam shaping and illumination system 102 or of the projection system 104 of the EUV lithography apparatus 100A. However, the component 200 can also be part of a DUV lithography apparatus 100B as explained above.

The component 200 can be a so-called Actuation Sensor Unit (ASU), for example, with the aid of which facets of a facet mirror, for example of a field facet mirror or of a pupil facet mirror, can be deflected. Such a facet mirror having deflectable facets can be part of the beam shaping and illumination system 102, for example.

The component 200 comprises a first component part 202. The first component part 202 can be for example a main body or frame of the component 200. The first component part 202 can be produced from metal, preferably from copper, high- grade steel or aluminium. Preferably, the first component part 202 is actively cooled.“Actively cooled” should be understood in the present case to mean that a fluid, for example water, is guided through the first component part 202 in order to absorb heat there and transport it away. For this purpose, the first component part 202 can comprise a cooling system 204, in particular a cooling circuit, which is illustrated highly schematically in Fig. 2. The cooling system 204 can be formed with the aid of cooling channels provided in the first component part 202.

The component 200 comprises a multiplicity of second component parts 206, only one of which, however, is provided with a reference sign in Fig. 2. The second component part 206 can be an Actuation Sensor Package (ASP), for example, which is suitable for deflecting a facet of a facet mirror as mentioned above. In this case, a second component part 206 of this type is assigned to each facet. Pref erably, a multiplicity of second component parts 206 are provided. By way of ex ample, hundreds of second component parts 206 can be provided. As shown in Fig. 2, the second component parts 206 are arranged in the shape of a grid or in the shape of a pattern. The second component parts 206 can have a circular-cylin drical geometry.

The second component parts 206 are received in the first component part 202 at least in sections and are sealed vis-a-vis said first component part. The second component parts 206 can be cooled with the aid of the cooling system 204. The first component part 202 has receiving sections, for example holes or recesses, in which the second component parts 206 are received in sections.

Fig. 3 shows a schematic section view through two second component parts 206 in accordance with the sectional line III-III in Fig. 2. Fig. 4 shows the detail view IV in accordance with Fig. 3. Reference is made below to Figs 3 and 4 simultane ously. As already mentioned, the first component part 202 comprises receiving sections 208, in which the second component parts 206 are received. The receiving sec tions 208 can be embodied as holes in the first component part 202. The first com ponent part 202 furthermore comprises one sealing surface 210 or a plurality of sealing surfaces 210. In particular, a sealing surface 210 of this type is assigned to each second component part 206. The seahng surfaces 210 each extend circu larly around the corresponding second component part 206. As shown in Fig. 3, the second component parts 206 each project above the sealing surface 210 as signed thereto.

Each second component part 206 comprises a main body 212 having a cylindrical base section 214 and a flange section 216 extending around the base section 214. The base section 214 can be constructed rotationally symmetrically with respect to a centre axis or axis of symmetry 218. The flange section 216 is not constructed rotationally symmetrically with respect to the axis of symmetry 218.

The flange section 216 can be polygonal. As viewed along the sectional line III- III, a distance Al between flange sections 216 of two adjacent second component parts 206 is only a few hundred pm. By way of example, the distance Al can be 200 pm. The base section 214 is received in the receiving section 208 and projects beyond the corresponding sealing surface 210. The flange section 216 comprises in each case a sealing surface 220 respectively facing a corresponding seahng sur face 210 of the first component part 202.

A ring body 222 is placed onto the main body 212. The ring body 222 is closed off with a ceramic plate towards the top in the orientation in Fig. 3. The ceramic plate can be soldered into the ring body 222. The ring body 222 can be welded to the main body 212. Each second component part 206 comprises a sensor system and an actuator. The actuator can comprise a plurahty of coils.

The second component parts 206, in particular the sealing surfaces 220, are sealed vis-a-vis the first component part 202, in particular the seahng surfaces 210, with the aid of a sealing device 300. For this purpose, the sealing device 300 is positioned and pressed between the sealing surfaces 210, 220. A yielding vol ume 226 for the pressing of the sealing device 300 is provided in each case be tween the sealing device 300 and the base sections 214. The yielding volume 226 can be referred to as a compensation volume.

Fig. 5 shows a schematic sectional view through two second component parts 206 in accordance with the sectional line V-V in Fig. 2. Fig. 6 shows the detail view VI in accordance with Fig. 5. Reference is made below to Figs 5 and 6 simultane ously.

As viewed along the sectional line V-V, the first component part 202 extends out over the sealing surfaces 210 with a bearing section 224. The second component parts 206 bear on the bearing sections 224 in such a way that the sealing sur faces 210, 220 are positioned at a defined distance away from one another. The distance Al is significantly larger when viewed along the sectional line V-V than when viewed along the sectional line III-III.

The comparison of Figs 3 and 4 with Figs 5 and 6 shows that very little structural space is present along the sectional line III-III. There is a very small overlap be tween the sealing surfaces 220 of the second component parts 206 and the sealing device 300. A decentration of the sealing device 300 in relation to the respective axis of symmetry 218 can easily lead to leakage for this reason. Furthermore, be tween adjacent second component parts 206, there is also only a very small or al most no yielding volume 226 for the pressing of the sealing device 300. Therefore, leaks can occur between two adjacent second component parts 206.

Along the sectional line V-V, by contrast, the ridge-shaped bearing section 224 is provided between two adjacent second component parts 206, the flange sections 216 of the second component parts 206 being supported on said bearing section. The sealing device 300 extends between the bearing section 224 and the base sec tions 214 of the main body 212 of the respective second component part 206. Sig nificantly more structural space is present between adjacent second component parts 206 in comparison with a view along the sectional line III-III. There is a significantly larger overlap between the sealing surfaces 220 of the second com ponent parts 206 and the sealing device 300. Therefore, a decentration of the sealing device 300 is rather noncritical here with regard to leaks. The yielding volume 226 for the pressing of the sealing device 300 is also significantly larger as viewed along the sectional line V-V.

If an internal diameter of the seahng device 300 is then increased in order to en large the yielding volume 226, the centring of the sealing device 300 is no longer ensured, however. The lack of centring of the sealing device 300 can have the ef fect that in the view along the sectional hne IITIII the sealing device 300 bears against one of two adjacent second component parts 206 and is spaced apart by double the distance from the other of the two second component parts 206. Leaks can occur on account of the small overlap between the sealing surface 220 and the sealing device 300. No overlap at all between the sealing surface 220 and the sealing device 300 occurs in the worst case. This must be avoided.

The small structural space between the second component parts 206 does not per mit the sealing device 300 to be separated into individual sealing rings, for exam ple into O-rings. Furthermore, individual sealing rings cannot be prevented from tilting away on account of the small structural space. Therefore, the sealing de vice 300, as shown in Fig. 7, is produced as a sealing mat, which is cut out from a suitable plastics material with the aid of a laser, for example. By way of example, a perfluoro rubber (FFKM) can be used as suitable material.

As shown in Fig. 7, the sealing device 300 comprises a multiplicity of sealing rings 302 connected to one another, only one of which, however, is provided with a reference sign in Fig. 7. By virtue of the fact that the sealing rings 302 are con nected to one another, the sealing rings 302 are prevented from tilting away.

Fig. 8 shows the detail view IIX in accordance with Fig. 7. The sealing rings 302 are connected to one another at connection locations 304, only two of which are provided with a reference sign in Fig. 8. The sealing device 300 is thus an inte gral component part, in particular one which is materially in one piece.“Integral” should be understood to mean in the present case that the sealing device 300 forms a single component part, which is not constructed from mutually separate component parts. That is to say that the sealing rings 302 are fixedly connected to one another, wherein the totahty of all the sealing rings 302 forms the sealing device 300.“Materially in one piece” should be understood in the present case to mean that the sealing device 300 is an integral component part produced from the same material throughout.

The seahng rings 302 each have an external diameter DA, which is constant and which is flattened only in the region of the connection locations 304. For the case where the sealing rings 302 are embodied such that they each also have a con ^¬ stant internal diameter chosen in such a way that a centring on the respective base section 214 of the second component parts 206 is effected, the problem arises that, as viewed along the sectional line III-III in Fig. 2, almost no yielding vol ^¬ ume 226 for the pressing of the sealing device 300 is present. Consequently, the sealing device 300 cannot be pressed sufficiently between adjacent second compo ^¬ nent parts 206.

This can have the consequence that either the sealing device 300 is damaged, which can lead to leaks, or a required installation position of the respective sec ^¬ ond component part 206 cannot be attained. This last can lead to position errors in a height direction (z- error) of the component 200. In order to obtain a sufficient yielding volume 226, the internal diameter of the seahng rings 302 can be in ^¬ creased, such that a sufficiently large yielding volume 226 is kept available be ^¬ tween the second component parts 206 and the sealing device 300. However, this has the disadvantage that a sufficient centring at the base sections 214 of the second component parts 206 is not ensured. The sealing rings 302 then do not bear circumferentially against the base sections 214, which can lead to leaks over time or directly in the course of mounting.

In order then to obtain a sufficiently large yielding volume 226 and a good cen ^¬ tring at the same time, the seahng rings 302 each comprise an inner contour 306 which is not circular, but rather, as will be explained below, is trefoiled. That is to say that the sealing rings 302 have a varying internal diameter rather than a constant internal diameter. Reference is made below to just one sealing ring 302. A theoretical internal diameter DI of the sealing ring 302 is illustrated by a dashed line in Fig. 8. The internal diameter DI corresponds to an external diame ^¬ ter of the base section 214 of the second component parts 206. Each sealing ring 302 comprises a first plane of symmetry El and a second plane of symmetry E2. The planes of symmetry El, E2 are positioned perpendicularly to one another and intersect one another. The sealing ring 302 is constructed symmetrically, in particular mirror-symmetrically, both with respect to the first plane of symmetry El and with respect to the second plane of symmetry E2. The diameters DA, DI have their centre point on a line of intersection of the two planes of symmetry El, E2. A coordinate system having a first spatial direction or x- direction x, a second spatial direction or y direction y and a third spatial di ^¬ rection or z-direction z is assigned to the seahng ring 302. The directions x, y, z are positioned perpendicularly to one another.

Furthermore, an azimuth direction or circumferential direction U is also assigned to the sealing ring 302. The circumferential direction U can be oriented in the clockwise or anticlockwise direction. The circumferential direction U is oriented in the anticlockwise direction in Fig. 8. The circumferential direction U runs along the inner contour 306.

The connection locations 304 are arranged mirror-symmetrically both with re ^¬ spect to the first plane of symmetry El and with respect to the second plane of symmetry E2. A respective azimuth angle a, 6 is provided between two adjacent connection locations 304. The azimuth angle a can be referred to as first azimuth angle. The azimuth angle 6 can be referred to as second azimuth angle. The azi ^¬ muth angle 6 is greater than the azimuth angle a. By way of example, the azi ^¬ muth angle a is approximately 71° and the azimuth angle 6 is approximately 108°. The azimuth angle a is provided in each case between two connection loca ^¬ tions 304 arranged mirror-symmetrically with respect to the first plane of sym ^¬ metry El. The azimuth angle 6 is provided in each case between two connection locations 304 arranged mirror-symmetrically with respect to the second plane of symmetry E2.

The sealing ring 302 comprises a connection radius R304 at the connection loca ^¬ tions 304. The inner contour 306 thus has the connection radius R304 in the re ^¬ gion of the connection locations 304. That is to say that four connection radii R304 are provided, only one of which, however, is shown in Fig. 8. A respective centre point MR304- 1 to MR304-4 of the connection radius R304 lies outside the planes of symmetry El, E2. Four centre points MR304- 1 to MR304-4 are pro vided, which he on hnes of symmetry LI to L3 of the connection locations 304. Each connection location 304 is assigned a line of symmetry LI to L3, wherein only three lines of symmetry LI to L3 are shown in Fig. 8. The connection loca tions 304 are constructed in each case symmetrically with respect to the lines of symmetry LI to L3. In other words, the lines of symmetry LI to L3 run centrally through the connection locations 304. The azimuth angles a, 6 are plotted be tween the lines of symmetry LI to L3.

The centre points MR304- 1 to MR304-4 are positioned mirror-symmetrically with respect to the planes of symmetry E l, E2. The centre points MR304- 1, MR304-4 and the centre points MR304-2, MR304-3 are positioned in a manner spaced apart by a distance A2 from one another in the y- direction y. The centre points MR304- 1, MR304-2 and the centre points MR304-3, MR304-4 are positioned in a manner spaced apart by a distance A3 from one another in the x-direction x. The distance A2 is greater than the distance A3. The respective connection radius R304 extends over an azimuth angle g in the circumferential direction U. The az imuth angle g is 20°, for example. For the case where the azimuth angles a, 6 are each 90°, the distances A2, A3 are equal in magnitude. The connection radius R304 is less than half the internal diameter DI.

The inner contour 306 has a respective first intermediate radius Rl l, R12 be tween two connection locations 304 which are adjacent in the x-direction x. The inner contour 306 comprises two first intermediate radii Rll, R12. The first in termediate radii Rl l, R12 are situated respectively at the top and bottom in the orientation in Fig. 8. The first intermediate radii Rll, R12 are each greater than the connection radius R304. It thus holds true that: Rll, R12 > R304.

A respective centre point MR11, MR12 of the first intermediate radii Rl l, R12 is situated on the first plane of symmetry El and is offset respectively upwards and downwards in relation to the second plane of symmetry E2 in the orientation in Fig. 8. As viewed in the ydirection y, the centre points MR11, MR12 of the first intermediate radii Rl l, R12 are positioned in a manner spaced apart by a dis tance A4 from one another. In this case, the centre point MR 11 is assigned to the first intermediate radius Rl l. The centre point MR12 is assigned to the first in termediate radius R12.

The inner contour 306 comprises a respective second intermediate radius R21, R22 between two connection locations 304 which are adjacent in the ydirection y. The inner contour 306 comprises two second intermediate radii R21, R22. The second intermediate radii R21, R22 are situated respectively on the left and right in the orientation in Fig. 8. The second intermediate radii R21, R22 are in each case greater than the connection radius R304 and less than the first intermediate radii Rl l, R12. It thus holds true that: Rl l, R12 > R21, R22 > R304. However, other suitable size relationships can also be chosen. The intermediate radii Rll, R12, R21, R22 are greater than half the internal diameter DI.

A respective centre point MR21, MR22 of the second intermediate radii R21, R22 is situated on the second plane of symmetry E2 and is offset respectively towards the left and right in relation to the first plane of symmetry E 1 in the orientation in Fig. 8. As viewed in the x-direction x, the centre points MR21, MR22 of the sec ond intermediate radii R21, R22 are positioned in a manner spaced apart by a distance A5 from one another. In this case, the centre point MR21 is assigned to the second intermediate radius R21. The centre point MR22 is assigned to the second intermediate radius R22. The distance A4 is greater than the distance A5. For the case where the azimuth angles a, 6 are each 90° and thus equal in magni tude, the distances A4, A5 are equal in magnitude. Accordingly, the intermediate radii Rl l, R12, R21, R22 can also be equal in magnitude.

The inner contour 306 furthermore comprises optional transition radii RU, with the aid of which the intermediate radii Rl l, R12, R21, R22 transition into the re spective connection radius R304. In each case two transition radii RU are pro vided per connection location 304. The transition radii RU are preferably identi cal, but can also be embodied individually. The transition radii RU provide for a continuously variable transition from the respective connection radius R304 into the intermediate radii Rl l, R12, R21, R22. The prestress of the sealing ring 302 on the base section 214 of the respective sec ond component part 206 is proportional to the azimuth angle a, 6. Given an azi muth angle a of 71°, by way of example, a shortening of the sealing ring 302 be tween the corresponding connection locations 304 by a/360° or 71°/360° is neces sary. Given different distances or different azimuth angles a, 6, mutually differ ent first intermediate radii Rl l, R12 and second intermediate radii R21, R22 are chosen, as mentioned above. It is thereby possible to prevent the connection loca tions 304 from moving azimuthally during mounting and the sealing device 300 from warping as a result.

By virtue of the fact that the inner contour 306 has the connection radius R304 in the region of the connection locations 304, said connection radius being chosen such that it is less than the external diameter of the base section 214 of the sec ond component parts 206 and thus the internal diameter DI, a sufficiently large yielding volume 226 for the pressing of the sealing ring 302 can be provided at the connection locations 304.

In the region between the connection locations 304 at which the intermediate ra dii Rl l, R12, R21, R22 are provided, by contrast, the inner contour 306 experi ences a constriction or narrowing, such that the inner contour 306 bears against the base section 214 and can be centred there. Consequently, between the connec tion locations 304, the inner contour 306 bears against the base section 214 with a prestress. The narrowing of the inner contour 306 between the connection loca tions 304 and the widening of said inner contour at the connection locations 304 result in the inner contour 306 having the trefoiled or trefoil 4 ike design men tioned above.

Fig. 9 shows the detail view IV in accordance with Fig. 7. Fig. 7 shows a connec tion location 304 between two sealing rings 302 in detail. A respective yielding volume 308 is provided at the connection location 304 on both sides, said yielding volume, like the yielding volume 226, enabling the sealing rings 302 to be pressed. The yielding volume 308 can be referred to as a compensating volume. Unlike the yielding volume 226, however, the yielding volumes 308 are provided directly at the sealing device 300. A connection web 310 is provided between the yielding volumes 308, said connection web connecting adjacent sealing rings 302 to one another integrally. The connection location 304 itself has a width B304 at the connection web 310. The width B304 can be two millimetres, for example.

The yielding volumes 308 can be embodied as flattened portions of the respective external diameter DA of the sealing rings 302. That is to say that the external di ameters DA of adjacent sealing rings 302 do not transition into one another. By way of example, the yielding volumes 308 are embodied in each case as a cutout or groove extending completely through a wall thickness W300 (Fig. 10) of the sealing device 300. In this case, the groove-type yielding volumes 308 can have a width B308. The width B308 can be for example 0.1 to 0.3, in particular 0.2, mil limetre. The wall thickness W300 can be 1 to 3, in particular 2, millimetres.

Fig. 11 shows a development of the connection location 304 explained with refer ence to Figs 9 and 10. In contrast to Figs 9 and 10, the yielding volumes 308 do not extend completely through the wall thickness W300, but rather only to a depth T308. The depth T308 can be 1 millimetre, for example.

Fig. 12 shows once again the detail view IV in accordance with Fig. 7, but a de velopment of the connection location 304 shown in Figs 9 and 10 is illustrated in Fig. 12. In this case, the yielding volumes 308 are not embodied as cutouts or grooves. Rather, the yielding volumes 308 comprise a multiplicity of holes 312, 314, 316 positioned next to one another, only three of which, however, are pro vided with a reference sign in Fig. 12. The number of holes 312, 314, 316 is arbi trary. By way of example, it is possible to provide six holes 312, 314, 316 of this type per yielding volume 308.

The holes 312, 314, 316 can be circular and have a diameter D308 in each case. However, the holes 312, 314, 316 can also have any other geometry. By way of ex ample, the holes 312, 314, 316 can also be oval or polygonal. The diameter D308 can be 0.2 millimetre, for example. The holes 312, 314, 316 can all have the same diameter D308 or mutually different diameters D308. The holes 312, 314, 316 can be arranged in one row, as shown in Fig. 12. Alternatively, the holes 312,

314, 316 can also be arranged in a plurality of rows. The holes 312, 314, 316 can be positioned in a manner spaced apart from one another uniformly or non-uni- formly. The connection location 304 itself, as shown in Fig. 12, along the width B304, that is to say at the connection web 310, can be free of holes 312, 314, 316 or hole- free or holeless. The holes 312, 314, 316 can extend through the entire wall thick ness W300 or only to the depth T308 explained above.

Fig. 13 shows once again the detail view IV in accordance with Fig. 7, but a de velopment of the connection location 304 shown in Fig. 12 is illustrated in

Fig. 13. In this case the yielding volumes 308 each comprise a plurality of rows 318, 320 of holes, which in turn have a multiphcity of holes 312, 314, 316 as ex plained above. The number of rows 318, 320 of holes is arbitrary. The holes 312, 314, 316 can be arranged in two rows, as shown in Fig. 13. However, the holes 312, 314, 316 can also be arranged in three rows or in four rows. The individual holes 312, 314, 316 of the rows 318, 320 of holes can be positioned next to one an other, as shown in Fig. 13. However, the holes 312, 314, 316 can also be arranged offset with respect to one another.

Fig. 14 shows once again the detail view IV in accordance with Fig. 7, but a de velopment of the connection location 304 shown in Fig. 12 is illustrated in

Fig. 14. In this embodiment of the connection location 304, the entire connection web 310 is provided with holes 312, 314, 316, such that only a single continuous yielding volume 308 formed from holes 312, 314, 316 is provided.

All configurations of the yielding volumes 308 explained above reliably enable pressing of the respective sealing ring 302 in the region of the connection loca tions 304. As a result, leaks directly in the course of mounting and over time can be reliably prevented. At the same time, as explained above, a centring of the sealing rings 302 on the base sections 214 of the second component parts 206 is always ensured on account of the trefoiled geometry of the inner contour 306.

Although the present invention has been described on the basis of illustrative embodiments, it is modifiable in diverse ways. LIST OF REFERENCE SIGNS

100A EUV lithography apparatus

100B DUV lithography apparatus

102 Beam shaping and illumination system

104 Projection system

106A EUV light source

106B DUV hght source

108A EUV radiation

108B DUV radiation

110 Mirror

112 Mirror

114 Mirror

116 Mirror

118 Mirror

120 Photomask

122 Mirror

124 Wafer

126 Optical axis

128 Lens element

130 Mirror

132 Medium

200 Component

202 Component part

204 Cooling system

206 Component part

208 Receiving portion

210 Sealing surface

212 Main body

214 Base section

216 Flange section

218 Axis of symmetry

220 Sealing surface

222 Ring body

224 Bearing portion 226 Yielding volume

300 Sealing device

302 Sealing ring

304 Connection location

306 Inner contour

308 Yielding volume

310 Connection web

312 Hole

314 Hole

316 Hole

318 Row of holes

320 Row of holes

Al Distance

A2 Distance

A3 Distance

A4 Distance

A5 Distance

B304 Width

DA External diameter

DI Internal diameter

D308 Diameter

El Plane of symmetry

E2 Plane of symmetry

LI Line of symmetry

L2 Line of symmetry

L3 Line of symmetry

MR11 Centre point

MR 12 Centre point

MR21 Centre point

MR22 Centre point

MR304- 1 Centre point

MR304-2 Centre point

MR304-3 Centre point

MR304-4 Centre point Ml Mirror

M2 Mirror

M3 Mirror

M4 Mirror

M5 Mirror

M6 Mirror

RU Transition radius Rl l Intermediate radius R12 Intermediate radius R21 Intermediate radius

R22 Intermediate radius R304 Connection radius T308 Depth

U Circumferential direction W300 Wall thickness x x- direction

y y- direction

z- direction a Azimuth angle

6 Azimuth angle

Y Azimuth angle