Laser spark plug having an improved seal between the combustion chamber window and the casing

Abstract

A casing for a laser spark plug, in particular, of an internal combustion engine of a motor vehicle, or of a stationary engine; the casing including at least one casing part and a combustion chamber window joined to the casing part to form a seal at least regionally; characterized in that at least one sealing element, whose coefficient of thermal expansion at an operating temperature of the laser spark plug is greater than the coefficient of thermal expansion of the casing part at the operating temperature of the laser spark plug, is provided between the casing part and the combustion chamber window.

Claims

1. A casing for a laser spark plug, comprising: a casing part; a combustion chamber window joined to the casing part to form a seal at least regionally; and at least one sealing element, whose coefficient of thermal expansion at an operating temperature of the laser spark plug is greater than the coefficient of thermal expansion of the casing part at the operating temperature of the laser spark plug, is between the casing part and the combustion chamber window.

2. The casing of claim 1, wherein the coefficient of thermal expansion of the combustion chamber window at the operating temperature of the laser spark plug is less than the coefficient of thermal expansion of the casing part at the operating temperature of the laser spark plug.

3. The casing of claim 1, wherein the coefficient of thermal expansion of the combustion chamber window at the operating temperature of the laser spark plug is between approximately 4*10^−6/K and approximately 10*10^−6/K.

4. The casing of claim 1, wherein the coefficient of thermal expansion of the casing part at the operating temperature of the laser spark plug is between approximately 7*10^−6/K and approximately 16*10^−6/K.

5. The casing of claim 1, wherein the coefficient of thermal expansion of the sealing element at the operating temperature of the laser spark plug is between approximately 16*10^−6/K and approximately 20*10^−6/K.

6. The casing of claim 1, wherein the casing part and/or the sealing element is made of steel, and the combustion chamber window is made of sapphire.

7. The casing of claim 1, wherein in a region of contact with the at least one casing part and/or with the combustion chamber window, the sealing element has a coating made of a material, which is different from the base material of the sealing element.

8. The casing of claim 7, wherein the coating has a thickness of approximately 50 μm to approximately 150 μm.

9. The casing of claim 7, wherein the coating is galvanically deposited on the sealing element.

10. The casing of claim 1, wherein the coefficient of thermal expansion of the combustion chamber window at the operating temperature of the laser spark plug is between approximately 4*10^−6/K and approximately 8*10^−6/K.

11. The casing of claim 1, wherein the coefficient of thermal expansion of the casing part at the operating temperature of the laser spark plug is between approximately 7*10^−6/K and approximately 12*10^−6/K.

12. The casing of claim 1, wherein the coefficient of thermal expansion of the sealing element at the operating temperature of the laser spark plug is between approximately 16*10^−6/K and approximately 18*10^−6/K.

13. The casing of claim 1, wherein the casing part and/or the sealing element is made of steel, and the combustion chamber window is made of monocrystalline sapphire.

14. The casing of claim 1, wherein in a region of contact with the casing part and/or with the combustion chamber window, the sealing element has a coating made of a material, which is different from the base material of the sealing element, the base material being made of steel and the coating being made of copper.

15. A laser spark plug, comprising: a casing for the laser spark plug, including a casing part, a combustion chamber window joined to the casing part to form a seal at least regionally, and at least one sealing element, whose coefficient of thermal expansion at an operating temperature of the laser spark plug is greater than the coefficient of thermal expansion of the casing part at the operating temperature of the laser spark plug, is between the casing part and the combustion chamber window; wherein the laser spark plug has an operating temperature of between approximately 200° C. and approximately 1100° C.

16. The laser spark plug of claim 15, wherein the laser spark plug has an operating temperature of between approximately 280° C. and approximately 600° C.

17. The laser spark plug of claim 15, wherein the laser spark plug is of an internal combustion engine of a motor vehicle or of a stationary engine.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) FIG. 1 shows a schematic cross section of a first specific embodiment of the casing according to the present invention.

(2) FIGS. 2a, 2b show different configurations of sealing elements.

(3) FIG. 3 shows a schematic cross section of a further specific embodiment of the casing according to the present invention.

(4) FIG. 4 shows a schematic cross section of a further specific embodiment of the casing according to the present invention.

(5) FIG. 5 shows a schematic cross section of a further specific embodiment of the casing according to the present invention.

(6) FIG. 6 shows a schematic of a laser-based ignition system for an internal combustion engine.

DETAILED DESCRIPTION

(7) In FIG. 6, an internal combustion engine is designated, on the whole, by reference numeral 10. It may be used for propelling a motor vehicle not shown. Internal combustion engine 10 usually includes several cylinders, only one of which is denoted in FIG. 5 by the reference numeral 12. A combustion chamber 14 of cylinder 12 is delimited by a piston 16. Fuel reaches combustion chamber 14 directly through an injector 18, which is connected to a fuel pressure reservoir 20 that is also referred to as a rail. Alternatively, the fuel-air mixture may also be formed outside of the combustion chamber, for example, in the intake manifold or, in the case of stationary engines, in front of the turbocharger as well.

(8) The fuel-air mixture 22 present in combustion chamber 14 is ignited by a laser pulse 24, which is radiated into combustion chamber 14, in this instance, onto ignition point ZP, by an ignition device 27 that includes an ignition laser 26. To this end, laser device 26 is supplied with pumping light via a fiber optic device 28 for the optical pumping of laser device 26; the pumping light being provided by a pumping light source 30. Alternatively, pumping light source 30 may also be accommodated directly in the laser spark plug, and consequently, the need for optical waveguide 28 is eliminated. Pumping light source 30 is controlled by a control unit 32, which also controls injector 18.

(9) In an exemplary implementation, ignition laser 26 from FIG. 6 is advantageously integrated in a laser spark plug 100, which may be mounted, for example, in a region of the cylinder head of internal combustion engine 10 in a manner comparable to conventional high-voltage spark plugs.

(10) According to the present invention, laser spark plug 100 includes a casing having the characteristics described below with reference to FIG. 1. FIG. 1 shows a cross section of a portion of casing 110, which includes an end region 110′, which faces the combustion chamber and, in the installed state of laser spark plug 100 or casing 110 in an internal combustion engine 10 (FIG. 6), borders on at least a portion of combustion chamber 14 or extends into it. Ignition laser 26 is situated, for example, in an interior chamber I of a region 110″ of casing 110 facing away from the combustion chamber. In a further specific embodiment, pumping light source 30 may also be situated in laser spark plug 100.

(11) As is apparent from FIG. 1, casing 110 includes at least one first casing part 110a, which is, in this case, substantially sleeve-shaped and accommodates a combustion chamber window 120. Casing 110 further includes a second casing part 110b, which is movable relative to first casing part 110a in an axial direction, thus, horizontally in FIG. 1, using, for example, a screw thread not illustrated. Together with a shoulder 110a′ of first casing part 110a, second casing part 110b delimits a spatial section, which receives combustion chamber window 120 and a substantially disk-shaped or annular sealing element 130a.

(12) In this manner, combustion chamber window 120 is joined to first casing part 110a, that is, to shoulder 110a′, so as to form a seal at least regionally, which means that interior chamber I of casing 110 is shielded from combustion chamber 14.

(13) According to the present invention, a coefficient of thermal expansion of sealing element 130a at the operating temperature of laser spark plug 100 is greater than the coefficient of thermal expansion of casing part 110a at the operating temperature of laser spark plug 100, which means that a normally lower coefficient of thermal expansion of combustion chamber window 120 at the operating temperature of laser spark plug 100 may be at least partially compensated for. Optionally, two sealing elements (not shown in FIG. 1), which are positioned in front of and in back of the combustion chamber window in the axial direction, may also be provided, cf. FIG. 3. Then, the principle of the present invention with regard to the coefficients of thermal expansion of the sealing element is advantageously applicable to at least one of the sealing elements, but, particularly, may be applicable to the two sealing elements as well.

(14) For example, an axial preloading force necessary for the sealing action in the region of sealing element 130a may be applied with the aid of further casing part 110b, e.g., by screwing further casing part 110b suitably far into first casing part 110a (in FIG. 1, from left to right). Accordingly, preloading force F acts upon the “layer construction” made up of combustion chamber window 120 and sealing element 130a.

(15) In particular, inner axial dimension 11 of the spatial region containing components 120, 130a has a temperature dependence, which is essentially a function of the thermal expansion coefficient of first casing part 110a. Therefore, when casing 110 is heated up to the operating temperature of laser spark plug 100, inner axial dimension 11 of the spatial region increases relatively steeply, while a longitudinal expansion of combustion chamber window 120 essentially parallel to this, thus, the thermally dependent change in thickness d2, is relatively low, which means that an unwanted reduction in axial preloading force F is generated.

(16) Due to the selection of the present invention of the thermal expansion coefficient for the sealing element 130a also situated in the spatial region, because of its relatively large linear thermal expansion in the axial direction, which is greater than that of first casing part 110a, the sealing element offsets the relatively low linear thermal expansion of combustion chamber window 120 at least partially or compensates for it almost completely, which means that the preloading force F necessary for the sealing action is essentially maintained even in the event of large temperature fluctuations.

(17) That is, the selection of the coefficient of thermal expansion of the material of sealing element 130a according to the present invention allows a comparatively low increase in thickness d2 of combustion chamber window 120 in response to heating it to the operating temperature to be at least partially compensated for by a comparatively large increase in thickness d1 of sealing element 130a, which means that the increase in inner axial dimension 11, which is also comparatively large, is countered with the intention of maintaining preloading force F.

(18) In one advantageous specific embodiment, it is provided that the coefficient of thermal expansion of combustion chamber window 120 at the operating temperature of laser spark plug 100 be less than the coefficient of thermal expansion of casing part 110a and/or 110b at the operating temperature of laser spark plug 100.

(19) In one further advantageous specific embodiment, it is provided that the coefficient of thermal expansion of combustion chamber window 120 at the operating temperature of laser spark plug 100 be between approximately 4*10^−6/K (Kelvin) and approximately 10*10^−6/K, in particular, approximately 8*10^−6/K. These values are attainable, for example, using crystalline sapphire.

(20) In a further advantageous specific embodiment, the coefficient of thermal expansion of casing part 110a and/or 110b at the operating temperature of laser spark plug 100 is between approximately 7*10^−6/K and approximately 16*10^−6/K, in particular, approximately 12*10^−6/K. These values are attainable, for example, using steel of type 1.4913 or similar (turbine steel).

(21) In a further advantageous specific embodiment, the coefficient of thermal expansion of sealing element 130a at the operating temperature of laser spark plug 100 is between approximately 16*10^−6/K and approximately 20*10^−6/K, in particular, approximately 18*10^−6/K. These values are attainable, for example, using steel of type 1.4841 or similar.

(22) In a further advantageous specific embodiment, it is provided that casing part 110a, 110b and/or sealing element 130a be made of steel (which may be of a different type to produce different coefficients of thermal expansion); combustion chamber window 120 being made of sapphire, in particular, monocrystalline sapphire.

(23) In a further advantageous specific embodiment, it is provided that a thickness d1 of sealing element 130a be between approximately 0.4 mm and approximately 3 mm, in particular, approximately 1.0 mm; particularly effective sealing action and particularly efficient compensation for the thermal expansion of the materials of casing part 110a and of combustion chamber window 120 being simultaneously obtained.

(24) In a further advantageous specific embodiment, it is provided that a thickness d2 of combustion chamber window 120 be between approximately 2 mm and approximately 8 mm, in particular, approximately 4 mm; together with casing part 110a and sealing element 130a, particularly efficient balancing of the thermal expansion of the materials and effective optical characteristics for transmitting laser ignition pulses 24 being simultaneously produced (cf. FIG. 6, as well).

(25) In one further advantageous specific embodiment, which is schematically represented in FIG. 2a, sealing element 130a has, in a region of contact with the at least one casing part 110a (FIG. 1) and/or with combustion chamber window 120, a coating 140 (FIG. 2a) made of a material, which is different from the base material of sealing element 130a; base material 130a may be steel; and coating 140 may be made of copper or another ductile material. As an alternative, copper foil may also be used.

(26) In a further advantageous specific embodiment, coating 140 is made of a copper layer of a thickness d3 between approximately 50 μm and approximately 150 μm, which may be, approximately 100 μm. According to tests of the Applicant, such a copper coating may be advantageously provided as a “filler,” that is to say, as an actual sealing material, which may advantageously level out further the surface roughness of the components including the coating (casing part 110a, combustion chamber window 120), in that the material of the sealing element or its coating 140 spreads itself out into these contact surfaces of the components involved, for example, by creep, during the bracing or pressing at specifiable preloading force F.

(27) In a further advantageous specific embodiment, the flatness of coating 140 is, advantageously, approximately 2 μm or better.

(28) According to a further advantageous specific embodiment, coating 140, in particular, copper coating, may be advantageously applied to sealing element 130a galvanically or by similar coating methods.

(29) Providing a coating 140 of the type mentioned above to regions of casing parts 110a, 110b, in particular, to their front-side end regions, which come into contact with elements 120, 130a, is also conceivable and may be accomplished with the aid of similar or identical manufacturing processes.

(30) In the case of a galvanic coating, care must be taken that copper coating 140 have an effective bond with the base material, for example, steel of type 1.4841.

(31) In a further advantageous specific embodiment, it is provided that in a region of contact with the at least one casing part 110a and/or with combustion chamber window 120, sealing element 130a have a lapped surface may have a maximum average surface roughness Rzmax of less than or equal to approximately 6, through which further increased sealing action is attained.

(32) The surfaces of contact of casing parts 110a, 110b with combustion chamber window 120 and with sealing element 130a may also be advantageously lapped or, e.g., precision-turned so as to have turning grooves substantially concentric with respect to the longitudinal axis of the component in question. Grinding may also be considered. It further may be the case for the contact surfaces of casing parts 110a, 110b to also have a maximum average surface roughness Rzmax of less than or equal to approximately 6.

(33) In a further advantageous specific embodiment, the at least one casing part 110a is pressed against combustion chamber window 120 at a specifiable preloading force F. The specifiable preloading force F of, e.g., approximately 5 kN (kilonewtons) to approximately 15 kN advantageously allows particularly effective sealing action between the casing part 110a in question and combustion chamber window 120 or sealing element 130a. In addition, the use of a specified, and thus, known preloading force F may allow a prediction to be made regarding the imperviousness attained and the approximate service life of casing 110 and laser spark plug 100 (FIG. 6) to be expected.

(34) In one further advantageous specific embodiment, two or more sealing elements 130a, 130a′, cf. FIG. 2b, whose coefficients of thermal expansion at the operating temperature of laser spark plug 100 are different from one another, are provided between casing part 110a and combustion chamber window 120, which means that further degrees of freedom are given to compensate for the thermal linear expansion.

(35) An operating temperature of laser spark plug 100 is, for example, between approximately 200° C. and approximately 1100° C., in particular, between approximately 280° C. and approximately 600° C.

(36) According to a further advantageous specific embodiment, the values of the coefficients of thermal expansion of the components and/or their ratios to one another, specified according to the present invention, may not only apply to the operating temperature of laser spark plug 100, but also to room temperature (e.g., approximately 20° C.), as well as, optionally, to the temperature range between room temperature and the operating temperature of the laser spark plug, which may be, at least between approximately 20° C. and approximately 400° C.

(37) FIG. 3 shows a cross section of a further specific embodiment of the casing according to the present invention. As is apparent from FIG. 3, casing parts 110a, 110b are each substantially sleeve-shaped and matched to one another in such a manner, that they are insertable into each other over a certain overlap length 1 and are coaxially alignable with each other. In this case, casing parts 110a, 110b may be joined with the aid of a screw thread G, which is situated at least partially in overlap region 1.

(38) Casing 110 may also be advantageously attached to a cylinder head of internal combustion engine 10 (FIG. 6) via a screw connection; a corresponding external thread GA (FIG. 3) is provided on the casing part 110b facing the combustion chamber.

(39) The part 110′ of casing 110 facing the combustion chamber is essentially formed by casing part 110b, while a part 110″ of casing 110 facing away from the combustion chamber is essentially formed by casing part 110a. In turn, e.g., components of laser device 26 from FIG. 6, in particular, a laser-active solid body, etc., may be situated in casing part 110a.

(40) As is apparent from FIG. 3, combustion chamber window 120 is situated in an interior section of second casing part 110b. In particular, combustion chamber window 120 rests against an approximately annular step 110b′ of the inner radius of second casing part 110b, which means that a substantially annular contact surface or sealing surface is accordingly produced on the surface of combustion chamber window 120 facing combustion chamber 14.

(41) In contrast, a second surface of combustion chamber window 120 facing interior chamber I of casing 110 also has, for instance, a substantially annular sealing surface, which is defined by a contact surface between combustion chamber window 120 and a front-side end region of sleeve-shaped, first casing part 110a.

(42) According to a specific embodiment, both of the above-mentioned sealing surfaces may advantageously have sealing elements 130a, 130b, for example, elements taking the form of sealing disks. In the variant of the present invention shown in FIG. 3, the principle of the present invention, which is described above with reference to FIG. 1 and concerns the selection of the coefficient of thermal expansion of the material for the sealing element, may be applied to both the two sealing elements 130a, 130b and only one of the two.

(43) All in all, the configuration illustrated in FIG. 3 produces reliable and stable sealing of interior chamber I of casing 110 from combustion chamber 14 of internal combustion engine 10; for example, laser device 26 (FIG. 5) being able to be situated in the interior chamber of the housing. The sealing is optimal when the principle of the present invention regarding the selection of the coefficient of thermal expansion of the material for the sealing element is applied to both sealing elements 130a, 130b, since this provides the maximum potential for offsetting the relatively low linear thermal expansion of combustion chamber window 120, using sealing elements 130a, 130b.

(44) In this case, the preloading force F for joining at least one, which may be both, of the casing parts 110a, 110b to combustion chamber window 120 is generated by screwing inner sleeve 110a into outer sleeve 110b with the aid of thread G. This means that in each instance, essentially the same preloading force is generated for the two sealing elements 130a, 130b, that is, the relevant sealing surfaces between components 110a, 130a, 120 and 110b, 130b, 120.

(45) According to a further, particularly advantageous specific embodiment, specifiable preloading force F is at least approximately 5 kN, which may be, approximately 15 kN, by which particularly reliable sealing of interior chamber I with respect to combustion chamber 14 is provided.

(46) In a further advantageous specific embodiment, it is proposed that the connection between the at least one casing part 110a and combustion chamber window 120 have a helium-tightness of at least approximately 10.sup.−6 mbar×1/sec.

(47) In a further specific embodiment, at least one of the casing parts 110a, 110b, but which may be both, have a tensile strength of at least approximately 1000 N per mm.sup.2, which may be accomplished, for example, by selecting an appropriate type of steel, for example, ST 1.4913, as a material. It is particularly advantageous for steels having a high high-temperature strength and creep rupture strength to be used.

(48) In a further advantageous specific embodiment, a maximum average surface roughness R.sub.zmax≦approximately 6 is provided for regions of parts 110a, 110b, which are pressed against combustion chamber window 120 or sealing disks 130a, 130b. Sealing disks 130a, 130b themselves may also be manufactured, in turn, to have a comparable maximum average surface roughness.

(49) According to a further specific embodiment, sealing element 130a, 130b may have a substantially disk-shaped or annular geometry with a parallelism between a base and a top surface of ≦approximately 10 μm, in particular, approximately 5 μm.

(50) It is advantageous for the exact geometry of casing parts 110a, 110b in the region of combustion chamber window 120 to be selected in such a manner, that combustion chamber window 120 or sealing elements 130a, 130b may lie flat on corresponding shoulders 110a′ (FIG. 1) and 110b′ (FIG. 3), and thus, their surface normals are each parallel to optical axis OA (FIG. 3) of laser spark plug 100 and casing 110. For this, one must ensure that an outer diameter of sealing elements 130a, 130b or of combustion chamber window 120 is somewhat smaller than the inner diameter of the region of casing part 110b receiving these components. In particular, any existing inner radii caused by machining (e.g., due to a non-disappearing outer radius of a corner of a cutting tool that removes chips) must be taken into account, so that the outer edges of components 120, 130a, 130b do not come to rest on corresponding inner radii of casing part 110b, but on the end faces in region 110b′ manufactured to be as flat as possible.

(51) Casing 110 of the present invention may be obtained, for example, using the following manufacturing method: in a first step, casing parts 110a, 110b are pressed or preloaded against combustion chamber window 120 and sealing element 130a, 130b, which may be, at a specifiable preloading force F (FIG. 3). In this context, components 110a, 120, 130a, 130b are selected so as to satisfy the above-described principle of the present invention regarding the different coefficients of thermal expansion. During the pressing, casing parts 110a, 110b are interconnected in an advantageous manner, in particular, by screwing and/or welding and/or clamping or comparable techniques.

(52) Optionally, after casing parts 110a, 110b have been joined to one another, a tempering step may still be carried out, which is used, inter alia, to allow a surface coating 140, e.g., of sealing elements 130a, 130b to set; the surface coating improving sealing action; the material creeping, in particular, into the surface indentations defined by the non-disappearing surface roughness of the components 110a, 110b, 120, 130a, 130b in question.

(53) In a further advantageous specific embodiment, the screwing is carried out, using a specifiable torque profile; in particular, the torque profile may specify different tightening torques for different screw depths; for at least one screw depth, waiting times also being provided before the screwing operation is continued.

(54) Generally, in the case of the screwing variant, the contact force F provided by the present invention (FIG. 3) may therefore be applied by screwing first casing part 110a together with second casing part 110b in a defined manner, thus, with a predetermined torque. For example, a torque wrench or a comparable tool may be used for this.

(55) According to a specific embodiment of the present invention, the torque profile may provide, for example, that a tightening torque for the screwing operation be increased in steps, for example, from an initial value of 0 Nm (newton meter) to a final value of approximately 20 Nm. According to a further specific embodiment, a torque profile advantageously provides that certain screw depths 1 (FIG. 3) of casing parts 110a, 110b with respect to one another be reached using torque values of approximately 12 Nm and approximately 17 Nm; a final torque of approximately 20 Nm being used for ultimately producing contact force F proposed by the present invention. It is particularly advantageous for waiting times between the individual screwing stages to be from approximately 3 minutes to approximately 5 minutes long, in order to allow setting processes of the components to be screwed to set in, which further improve the sealing action.

(56) In a further specific embodiment of the present invention, screw thread G (FIG. 1) has an M 16×2 thread.

(57) Combustion chamber window 120 (FIG. 1) may be made of crystalline, in particular, monocrystalline sapphire having a high rigidity and good transmission characteristics at a laser wavelength used. In particular, combustion chamber window 120 may be formed and positioned in such a manner, that the C-axis (also zero-degree axis) of the crystal structure extends along optical axis OA of casing 110 (FIG. 3) and of laser device 26 (FIG. 6).

(58) According to one specific embodiment, an outer diameter of combustion chamber window 120 may be approximately 12.7 mm.

(59) The optically active surfaces of combustion chamber window 120 may be industrially polished, for example, of the type scratch/dig: 60/40. The edges of combustion chamber window 120 may be advantageously brushed or provided with a chamfer of, e.g., approximately 0.3 mm. In particular, the optically active surfaces of combustion chamber window 120 may be plane-parallel.

(60) According to a specific embodiment, an outer diameter of sealing elements 130a, 130b is, for example, approximately 12.3 mm, thus, approximately 0.4 mm less than the outer diameter of combustion chamber window 120. In this manner, sealing elements 130a, 130b advantageously do not rest on the manufacturing chamfer in region 110b′ (FIG. 3) of plug casing 110.

(61) It is advantageous for an inner diameter of sealing elements 130a, 130b, through which laser beam 24 (FIG. 1, 6) may be emitted, to be approximately 8 mm, at least approximately 6 mm.

(62) FIG. 4 shows a cross section of a further specific embodiment of a casing 110 according to the present invention. A first casing part 110c is formed, again, to be substantially sleeve-shaped and is coaxially situated, along its entire length, and thus, completely, in a second casing part 110d, which is also approximately sleeve-shaped. Combustion chamber window 120 is surrounded, in turn, by disk-shaped sealing elements 130a, 130b, which produce, together with the corresponding end faces of casing parts 110c, 110d, the sealing action rendered possible by the present invention.

(63) According to the present invention, a coefficient of thermal expansion of at least one of the sealing elements 130a, 130b at the operating temperature of laser spark plug 100 is greater than the coefficient of thermal expansion of casing part 110d and 110c at the operating temperature of laser spark plug 100, which means that, in turn, the lower coefficient of thermal expansion of the combustion chamber window 120 presently made of monocrystalline sapphire, at the operating temperature of laser spark plug 100, may be at least partially compensated for.

(64) In contrast to the specific embodiment shown in FIG. 3, casing 110 in FIG. 4 does not have a screw connection between casing parts 110c, 110d. Rather, a continuous material connection of casing parts 110c, 110d is produced by welding, in particular, laser welding, in this case, in the region of arrow S. It may advantageously be a circumferential welded seam, which produces a particularly rigid connection of components 110c, 110d. In this case, contact force F between casing parts 110c, 110d and combustion chamber window 120 is advantageously generated by initially pressing or bracing sleeves 110c, 110d against each other prior to welding, namely, with contact force F. Only then is the continuous material connection produced in region S by laser welding. In this manner, it is advantageously ensured that contact force F proposed by the present invention is also maintained for the future, that is, after external contact force F ceases to be applied. During the manufacture of casing 110, contact force F may be generated, for example, using a press known per se. After the laser welding, a process of tempering may be carried out again, as well as a slow cool-off to room temperature.

(65) FIG. 5 shows a cross-sectional view of a further specific embodiment of a casing 110 according to the present invention. In contrast to the specific embodiments described above with reference to FIGS. 3, 4, in this case, casing 110 has a so-called sealing configuration screwed in on the side of the combustion chamber, where a first casing part 110e (“front cap”) is screwed from combustion chamber 14 or combustion-chamber side end 110′ into second casing part 110f. Preloading force F and, therefore, the sealing action, is produced in a manner comparable to the specific embodiments described above.

(66) Analogously to the specific embodiment shown in FIG. 1, only one sealing element 130c is illustrated in the configuration shown in FIG. 5. The explanations above apply to the coefficients of thermal expansion of components 110e, 110f, 120, 130c.

(67) As an option, a further sealing element (not shown) may also be provided between combustion chamber window 120 and the step-change in inner diameter of casing part 110f situated to the left of it.

(68) Casing part 110e advantageously includes a driving profile, which is not shown in further detail in FIG. 5 and allows casing part 110e to be screwed into second casing part 110f in a simple manner.

(69) In a further advantageous specific embodiment, the dimensioning specification explained below in further detail is provided for the axial dimensions of the components of combustion chamber window 120 and sealing element 130a or sealing elements 130a, 130b. As already described above, the axial dimension of combustion chamber window 120 is designated in FIG. 1 by double arrow d2 and, in this case, is also referred to as the thickness of combustion chamber window 120. The axial dimension of sealing element 130a is denoted in FIG. 1 by double arrow d1, and analogously to the thickness of combustion chamber window 120, it is also referred to as thickness d1 of sealing element 130a. In the present specific embodiment, the following dimensioning specification is advantageously provided:

(70) $\frac{l_{\mathrm{window}}}{l_{\mathrm{sealing}\mathrm{element}}}=\frac{{\alpha }_{\mathrm{casing}}-{\alpha }_{\mathrm{sealing}\mathrm{element}}}{{\alpha }_{\mathrm{window}}-{\alpha }_{\mathrm{casing}}},$
where l.sub.window refers to thickness d2 of combustion chamber window 120 as shown in FIG. 1, l.sub.sealing element refers to thickness d1 of sealing element 130a as shown in FIG. 1, and variables α.sub.casing, α.sub.sealing element, α.sub.window denote the coefficients of thermal expansion of the components: casing 110a, 110b (FIG. 1), sealing element 130a, and combustion chamber window 120.

(71) In specific embodiments that only contain one sealing element 130a (FIG. 1), 130c (FIG. 5) next to combustion chamber window 120, the thickness l.sub.sealing element indicated in the above formula corresponds to thickness d1 of the only sealing element 130a. In specific embodiments, in which two sealing elements 130a, 130b are provided in the region of combustion chamber window 120, cf., e.g., FIG. 3, the variable l.sub.sealing element of the above formula corresponds to the sum of the individual thicknesses of the two sealing elements 130a, 130b, since in this case, in a layout of their thermal expansion coefficients according to the present invention, the two sealing elements 130a, 130b interact to compensate for the relatively low thermal expansion of combustion chamber window 120 or adapt it to the relatively high thermal expansion of casing parts 110a, 110b.