Composite body useful in gas discharge lamp

Abstract

A composite body consisting of two or more formed parts of densely sintered aluminum oxide and a metal such as an envelope for a mercury vapor discharge lamp with a metal halide filling. The parts are connected together with material which comprises at least two of the oxides SiO.sub.2, Al.sub.2 O.sub.3 and B.sub.2 O.sub.3 and at least one of the trivalent oxides La.sub.2 O.sub.3 and Y.sub.2 O.sub.3. This material is applied at a relatively low temperature and is resistant to the gas filling up to approximately 1350.degree. C.

Description

The invention relates to a composite body consisting of two or more formed parts of density sintered aluminium oxide, saphire, one of the metals tantalum, niobium, tungsten, molybdenum or alloys with one of these metals as main component or with iron, nickel or cobalt as main component and/or material consisting of a mixture of metal oxide and a metal (cermet), which parts are joined together gas and vacuum-tight by means of sealing material which results in a joint which is resistant to the action of iodide-, bromide-chloride-vapour and -liquid at temperatures up to approximately 1350.degree. C, aluminium oxide and an oxide or a rare earth metal being present in the material of this joint.

The invention relates in particular to a gas discharge lamp wherein the envelope consists of above-mentioned densely sintered aluminium oxide, which is provided with an electrode feedthrough of molybdenum and as gas filling mercury vapour, doped with a metal chloride, -bromide or -iodide, for example thallium iodide. Densely sintered aluminium is the material which is eminently suitable against the action of metal halides at temperatures up to 1350.degree. C. U.S. Pat. No. 3,234,421 discloses such a gas discharge lamp.

U.S. Pat. No. 3,588,573 discloses a sealing material which consists of a binary or ternary composition of aluminium oxide and one or more oxides of rare earth metals of substantially eutectic composition, which sealing material furnishes a joint which is eminently resistant to the action of metal iodides, bromides and chlorides. A disadvantage of this adhesive material is that it has high melting temperatures so that great mechanical stresses remain in the joint produced.

In practice processing temperatures of not more than 1700.degree. C and, preferably, not more than 1600.degree. C are suitable to obtain composite bodies of the type mentioned in the preamble.

The invention provides such a composite body wherein the joint is formed by material which satisfies this requirement as regards making the joint and which material of the joint is resistant to contact with metal iodide, bromide and chloride vapour at temperatures up to 1350.degree. C.

The composite body according to the invention is characterized in that the material of the joint which is at least partly crystallized comprises at least two of the oxides SiO.sub.2, Al.sub.2 O.sub.3 and B.sub.2 O.sub.3 and at least one of the trivalent oxides La.sub.2 O.sub.3 and Y.sub.2 O.sub.3 in quantities which in mole % have at the utmost the following values: SiO.sub.2 66.6, La.sub.2 O.sub.3 50, B.sub.2 O.sub.3 50, Y.sub.2 O.sub.3 50 and Al.sub.2 O.sub.3 70, the sealing material for obtaining the joint being applied at a temperature of not more than 1700.degree. C and the material of the joint obtained therewith being located in a composition range within a tetrahedron formed by the components Al.sub.2 O.sub.3 -La.sub.2 O.sub.3 -SiO.sub.2 -B.sub.2 O.sub.3, whose limits in the side planes of the tetrahydron are shown in the accompanying FIGS. 1, area a, 2, area a and 3, area a and which are further defined by the cross-sections in FIGS. 8 area a, 9 area a and 10 area a, or in a composition range located within a tetrahedron formed by the components Al.sub.2 O.sub.3 -La.sub.2 O.sub.3 -SiO.sub.2 -Y.sub.2 O.sub.3, whose limits in the side planes of the tetrahedron are shown in the FIGS. 1, area a and 4, area a and are further determined by the cross-sections in FIGS. 5, area a, 6 area a and 7 area a.

A processing temperature of not more than 1600.degree. C can be achieved with compositions with which, when making the joint, one arrives in the following composition range which is located within a tetrahedron, formed by the components Al.sub.2 O.sub.3 -La.sub.2 O.sub.3 -SiO.sub.2 -B.sub.2 O.sub.3, whose limits in the side planes of the tetrahedron are shown in the accompanying FIGS. 1, area b, 2, area b and 3, area a and which are further defined by the cross-sections in FIGS. 8, area b, 9, area b and 10, area b, or in a composition range located within a tetrahedron formed by the components Al.sub.2 O.sub.3 -La.sub.2 O.sub.3 -SiO.sub.2 -Y.sub.2 O.sub.3, whose limits in the side planes of the tetrahedron are shown in the FIGS. 1, area b and 4, area b and which are further determined by the cross-sections in FIGS. 5, area b, 6, area b and 7, area b.

It should be noted that when making a joint between two parts one of which consists at least of densely sintered aluminium oxide a starting composition of the sealing material may be chosen which comprises less Al.sub.2 O.sub.3 then corresponds with the areas defined in the Figures. When making the joint a reaction occurs between the aluminium oxide and the sealing material wherein Al.sub.2 O.sub.3 dissolves in last-mentioned material. Then the material in the joint obtains a higher Al.sub.2 O.sub.3 content. In the ultimate product the composition of the material of the joint must be within the areas described above. The geometry of the feedthrough plays an important part herein. Besides the action of metal chlorides, -bromides or iodides the SiO.sub.2 -free materials of the joint are also resistant to the action of sodium vapour. In accordance with a further elaboration of the invention the La.sub.2 O.sub.3 and/or Y.sub.2 O.sub.3 may have been wholly or partly replaced in the material of the joint by one or more of the oxides of the lanthanides and of scandium.

Furthermore the material of the joint may contain to a total of not more than 20 mole % one or more of the oxides TiO.sub.2, ZrO.sub.2 and HfO.sub.2. These additions influence the crystallization behaviour of the starting material and, consequently, the quality of the joint.

The materials of the joints in accordance with the areas defined above are all vitreous-crystalline or poly-crystalline. Vitreous-crystalline means that one or more crystalline phases are present, finely dispersed in a vitreous phase.

The manner of applying the sealing material for producing the composite body according to the invention is, for example, the customary manner wherein the formed parts are pressed and kept together, the sealing material is applied on the seam in the form of a suspension or a ring of glass wire or of sintered glass which may be either crystallized or vitreous, and the whole assembly being heated to the required temperature, the material then flowing into the seams. It is also possible to enamel the surfaces to be connected with the sealing material.

Another method is that wherein the seams between said parts are filled with the sealing material in the vitreous state, the whole assembly being heated to a temperature above the softening temperature of the sealing material whereinafter the joint is effected under pressure. The vitreous joint obtained can be reinforced by crystallization at a slightly higher temperature than the transformation temperature. The glass-ceramic joint is sufficiently strong at temperatures up to 1350.degree. C-1450.degree. C above which flow of the material occurs.

Of the materials of the joint in accordance with last-mentioned preferred range which must be applied at a normal pressure at temperatures below 1600.degree. C wherein the material flows the transformation temperature (the temperature at which the viscosity amounts to 10.sup.13.6 poises) is as a rule between 850.degree. and 900.degree. C. When a pressure of, for example, 8 atm. is used, the joint can be made at approximately 950.degree.-1050.degree. C and devitrification of the joint can be effected at 1050.degree.-1150.degree. C. Herebelow some embodiments are given with reference to diagrammatic drawings to explain the invention.

EXAMPLE 1

As starting material for the joint to be made for obtaining the composite body according to the invention a plurality of compositions were melted to glass from which either glass wire or glass powder was produced. The glasses were melted, starting from lanthanum oxide having a purity over 99.995%, yttrium oxide, aluminium oxide 99.8% sand having a purity of 99.9%, optionally titanium dioxide, boron trioxide, hafnium oxide, zirconium sand ZrSiO.sub.4. The melting temperatures varied from 1500.degree. to 1900.degree. C. The Tables 1 to 6 list a number of the melted compositions.

Table 1______________________________________Composition wt % Composition mole %No. Al.sub.2 O.sub.3 La.sub.2 O.sub.3 SiO.sub.2 Al.sub.2 O.sub.3 La.sub.2 O.sub.3 SiO.sub.2______________________________________1 22.5 51.0 26.5 27.0 19.1 53.92 25 51 24 30.6 19.5 49.93 21 53 24 26.8 21.2 52.04 27.3 51.1 21.6 34.1 20.0 45.95 15 60 25 19.7 24.6 55.76 19.1 52.3 28.6 22.7 19.5 57.87 38.6 41.2 20.2 45 15 408 38.0 48.6 13.4 50 20 309 20.9 66.8 12.3 33.3 33.3 33.410 10 60 30 12.5 23.6 63.911 29.1 37.4 33.5 29.8 12.0 58.212 26.9 33.5 39.6 25.6 10.2 64.213 23.9 34.0 42.1 22.6 10.2 67.214 15.5 38.5 46.0 14.8 11.5 74.715 20 60 20 27.5 25.8 46.716 10.8 78.0 11.2 20 45 35______________________________________ Table 2______________________________________Composition wt % Composition mole %No. Al.sub.2 O.sub.3 Y.sub.2 O.sub.3 SiO.sub.2 Al.sub.2 O.sub.3 Y.sub.2 O.sub.3 SiO.sub.2______________________________________17 28.0 30.9 41.1 25.0 12.5 62.518 24.8 31.4 43.8 21.9 12.5 65.619 31.6 39.4 29.0 32.0 18 5020 35.8 38.6 25.6 37 18 4521 25.3 41.2 33.5 25.1 18.5 56.422 15.6 46.6 37.8 15.5 20.9 63.623 21.3 47.2 31.5 22.2 22.2 55.624 16.6 54.8 28.6 18.5 27.5 54.025 16.7 65.8 17.5 22 39 3926 15.0 27.6 57.4 12 10 78______________________________________ Table 3__________________________________________________________________________Composition in mole % Composition in wt %No. Al.sub.2 O.sub.3 La.sub.2 O.sub.3 B.sub.2 O.sub.3 SiO.sub.2 HfO.sub.2 Al.sub.2 O.sub.3 La.sub.2 O.sub.3 B20.sub.3 SiO.sub.2 HfO.sub.2__________________________________________________________________________27 30 36 34 17.9 68.3 13.828 14 50 36 7.1 80.5 12.429 10 50 40 5.1 81.0 13.930 31.4 27.2 28.4 13 21.7 59.6 13.4 5.331 37.5 23.5 24 15 27.3 54.4 11.9 6.432 47 17 21 15 37.9 43.5 11.5 7.133 42 22.5 22.5 13 27.0 45.9 9.9 17.234 45 20 20 15 29.4 41.5 8.9 20.235 22 37.5 25.5 15 11.5 62.9 9.2 16.4__________________________________________________________________________ Table 4______________________________________Composition in mole % Composition in wt %No. Al.sub.2 O.sub.3 La.sub.2 O.sub.3 Y.sub.2 O.sub.3 SiO.sub.2 Al.sub.2 O.sub.3 La.sub.2 O.sub.3 Y.sub.2 O.sub.3 SiO.sub.2______________________________________36 30 15 5 50 25.3 40.5 9.3 24.937 12 39.8 13.2 35 6.3 67.3 15.5 10.938 30 10 10 50 26.4 28.1 19.5 26.039 12 26.5 26.5 35 6.8 48.1 33.4 11.740 30 5 15 50 27.6 14.7 30.6 27.141 12 13.2 39.8 35 7.4 25.9 54.1 12.642 19.5 22.5 2.9 55.1 15 55 5 25______________________________________ Table 5______________________________________Composition in mole % Composition in wt %No. Al.sub.2 O.sub.3 La.sub.2 O.sub.3 SiO.sub.2 B.sub.2 O.sub.3 Al.sub.2 O.sub.3 La.sub.2 O.sub.3 SiO.sub.2 B.sub.2 O.sub.3______________________________________43 20 20 50 10 16.6 53.2 24.5 5.744 51.3 22.5 16.2 10 36.8 51.5 6.8 4.945 5.0 23.4 61.6 10 4.1 60.8 29.5 5.646 17.8 17.8 44.4 20 15.5 49.7 22.9 11.947 33.2 29.2 17.6 20 22.0 62.0 6.9 9.148 6.4 22.0 51.6 20 5.3 58.2 25.2 11.349 14.8 14.8 37.1 33.3 13.9 44.3 20.5 21.350 27.7 24.3 14.7 33.3 20.3 56.8 6.3 16.651 8.3 25.4 33.0 33.3 6.3 61.6 14.8 17.3______________________________________ Table 6__________________________________________________________________________Composition in mole % Composition in wt %No Al.sub.2 O.sub.3 La.sub.2 O.sub.3 SiO.sub.2 ZrO.sub.2 HfO.sub.2 TiO.sub.2 Sc.sub.2 O.sub.3 Al.sub.2 O.sub.3 La.sub.2 O.sub.3 SiO.sub.2 ZrO.sub.2 HfO.sub.2 TiO.sub.2 Sc.sub.2__________________________________________________________________________ O.sub.352 16.6 11.9 66.5 5.0 16.6 38.1 39.2 6.153 25.7 18.1 51.2 5.0 21.0 48.6 25.3 5.154 15.7 11.3 63.0 10.0 15.9 36.6 35.3 12.255 30.7 18.0 41.3 10.0 24.6 46.2 19.5 9.756 16.6 11.9 66.5 5.0 15.9 36.5 37.7 9.957 27.0 20.5 47.5 5.0 20.7 50.1 21.4 7.858 26.8 10.8 52.4 10.0 23.7 30.6 27.4 18.359 17.4 11.3 61.3 10.0 15.8 32.7 32.8 18.760 17.5 11.2 61.3 10.0 18.0 36.8 37.1 8.161 5.0 23.4 61.6 10.0 4.0 60.4 29.3 6.362 20.0 20.0 40.0 20.0 16.2 51.9 19.2 12.763 14.4 28.6 37.0 20.0 10.1 63.8 15.2 10.964 25.1 56.4 18.5 30.1 39.8 30.165 37.0 45.0 18.0 42.5 30.4 27.166 18.5 54.0 27.5 21.1 36.3 42.6__________________________________________________________________________

By means of the above-mentioned sealing materials joints were made between tungsten and densely sintered aluminium oxide, molybdenum and densely sintered aluminium oxide, tantalum and densely sintered aluminium oxide, niobium and densely sintered aluminium oxide and two components of densely sintered aluminium together. For the assemblies 1 to 8 inclusive, 15, 17 to 24 inclusive, 27 to 35 inclusive, 36, 38, 40, 42 and 43 to 66 inclusive the temperature to which the weld must be heated must be between 1500.degree. and 1600.degree. C, for the assemblies 9 to 14 inclusive, 16, 25, 26 and 37, 39 and 41 between 1600.degree. and 1700.degree. C.

Some compositions crystallize rather quickly and spontaneous. Most compositions crystallize after a thermal treatment for some hours at a temperature which is 300.degree. to 400.degree. C below the temperature of application.

In the composite bodies obtained the following compositions were determined, for example with energy dispersive technics such as "Microprobe" and "EDAX". The average composition in the joint was determined herewith.

Table 1a______________________________________Composition in mole % Composition in mole %No. Al.sub.2 O.sub.3 La.sub.2 O.sub.3 SiO.sub.2 No. Al.sub.2 O.sub.3 La.sub.2 O.sub.3 SiO.sub.2______________________________________1 30.0 18.3 51.7 9 36.6 31.7 31.72 33.8 18.7 47.5 10 17.4 22.4 60.23 29.2 20.5 50.3 11 45.6 9.3 45.14 37.4 19.1 43.5 12 48.4 7.1 44.55 21.8 24.0 54.2 13 46.8 7.0 46.26 25.2 19.3 55.5 14 44.3 7.5 48.27 50.6 13.4 36.0 15 32.7 24.0 43.38 52.7 18.9 28.4 16 22.3 43.7 34.0______________________________________ Table2a______________________________________Composition in mole % Composition in mole %No. Al.sub.2 O.sub.3 Y.sub.2 O.sub.3 SiO.sub.2 No. Al.sub.2 O.sub.3 Y.sub.2 O.sub.3 SiO.sub.2______________________________________17 27.6 12.1 60.3 22 17.9 20.3 61.818 24.2 12.1 63.7 23 25.3 21.3 53.419 33.1 17.7 49.2 24 23.2 25.8 51.020 38.2 17.6 44.2 25 24.3 37.8 37.921 26.8 18.1 55.1 26 27.1 8.3 64.6______________________________________ Table 3a______________________________________Composition in mole %No. Al.sub.2 O.sub.3 La.sub.2 O.sub.3 B.sub.2 O.sub.3 SiO.sub.2 HfO.sub.2______________________________________27 36 33 3128 19 47 3429 22 43 3530 33 26.6 27.7 12.731 39 23 23.4 14.632 50 16 20 1433 45 21.5 21.5 -- 1234 49 18.5 18.5 -- 1435 25 36.5 24.5 -- 14______________________________________ Table 4a______________________________________Composition in mole %No. Al.sub.2 O.sub.3 La.sub.2 O.sub.3 Y.sub.2 O.sub.3 SiO.sub.2______________________________________36 34.8 13.9 4.7 46.637 20.2 36.2 12.0 31.638 34.9 9.3 9.3 46.539 20.4 24.0 24.0 31.640 36.2 4.6 13.7 45.541 24.8 11.3 34.0 29.942 25.2 20.9 2.7 51.2______________________________________ Table 5a__________________________________________________________________________Composition in mole % Composition in mole %No. Al.sub.2 O.sub.3 La.sub.2 O.sub.3 SiO.sub.2 B.sub.2 O.sub.3 No. Al.sub.2 O.sub.3 La.sub.2 O.sub.3 SiO.sub.2 B.sub.2 O.sub.3__________________________________________________________________________43 24.6 18.8 47.1 9.5 48 9.9 21.3 49.6 19.244 53.1 21.8 15.4 9.7 49 20.7 13.9 34.5 30.945 16.2 20.6 54.3 8.9 50 31.1 23.1 14.0 31.846 21.5 17.0 42.4 19.1 51 12.6 24.2 31.5 31.747 35.1 28.4 17.1 19.4__________________________________________________________________________ Table 6a______________________________________Composition in mole %No. Al.sub.2 O.sub.3 LaO.sub.3 SiO.sub.2 ZrO.sub.2 HfO.sub.2 TiO.sub.2 Sc.sub.2 O.sub.3______________________________________52 21.6 11.2 62.5 4.753 28.1 17.5 49.6 4.854 19.7 10.8 60.0 9.555 32.4 17.6 40.3 9.756 21.6 11.2 62.5 4.757 31.0 19.4 44.9 4.758 29.6 10.4 50.5 9.559 21.1 10.8 58.6 9.560 21.3 10.7 58.5 9.561 17.3 20.3 53.6 8.862 28.2 17.9 35.9 18.063 21.6 26.2 33.9 18.364 29.5 53.2 17.365 40.3 42.6 17.166 21.2 52.2 26.6______________________________________ By way of example, the compositions 1 and 4 soften as glass at 850.degree.-900.degree. C, the glass crystallizes between 1050.degree. and 1150.degree. C and the crystallized material in the joint softens between 1500.degree. and 1600.degree. C and becomes liquid (viscosity < 100 poises).

EXAMPLE 2

A discharge vessel for a high pressure mercury vapour discharge lamp with halide addition has on both sides a construction as shown in FIG. 11 or in FIG. 12. The lamp which is known in itself inter alia from U.K. patent specification No. 1,374,063 will not be further described here.

In FIG. 11 the discharge vessel consists of a tube 1 of densely sintered aluminium oxide and a disc 2 also of densely sintered aluminium oxide. In the disc 2 a molybdenum pin 3 is sealed vacuum-tight by means of sealing material 4 which has one of the compositions 1 or 4 of the Table of example 1. Within the discharge vessel a tungsten spiral 5 which serves as electrode is spot welded to the pin 3. Disc 2 is connected vacuum-tight to the tube 1 by means of sealing material 6 of the composition 1, 12 or 24 of the Table. FIG. 12 shows another construction of a discharge vessel consisting of densely sintered aluminium oxide 11. The electrode assembly here consists of an aluminium oxide-molybdenum cermet 12 in which a molybdenum can 13 is sintered vacuum-tight. Inside the discharge space the can 13 supports a tunsten electrode 14. The cermet disc 12 is joined vacuum-tight by means of the sealing material 15 of the composition 5 of Table 1 to the end portion 16 of the discharge vessel 11.

The joints 4 and 6 of FIG. 11 were made by means of rings of sintered glass. The joint was made by heating the assembly to 1600.degree. C in argon and by cooling it slowly thereafter in which the glass crystallized.

The joint 15 was made by first covering the part 16 with an enamel coat of the composition 1, 12 or 24 of Table 1 and 2 respectively and by pressing the assembly 12-13-14 on it at a temperature between 940.degree. and 1000.degree. C under a pressure of 8 atm. Thereafter the assembly was heated for 15 minutes at 1100.degree. C which caused the sealing material to devitrify. In the different joints thus obtained approximately the compositions 1, 4, 5, 12 and 24 of Table 1a and 2a respectively were determined.

In accordance with one form of the invention a composite body is manufactured by coating at least one of the parts to be joined with a layer of sealing glass at the surface at which the joint is to be made. The parts at the locations where they are to be joined are heated in contact with one another to a temperature up to approximately 100.degree. C above the softening temperature of the sealing glass and then a pressure is applied to the joint while parts in the sealing glass and the joint is heated at a temperature of 150.degree. C to 250.degree. C above the sealing glass softening temperature until the sealing glass crystalizes.

Claims

1. A composite body comprising two parts formed of a material selected from the group consisting of (1) densely sintered aluminum oxide, (2) sapphire, (3) one of the metals tantalum, niobium, tungsten, molybdenum, (4) an alloy having as the main component a metal selected from the group consisting of tantalum, niobium, tungsten, iron, nickel and cobalt and (5) a material consisting of a mixture of a metal oxide and a metal, said parts being joined together in gas and vacuum-tight relationship by means of sealing material which results in a joint which is resistant to the action of iodide, bromide and chloride vapours and liquid at temperatures up to approximately 1350.degree. C, said sealing material including aluminum oxide and an oxide of a rare earth metal, wherein said joint comprises at least two of the oxides SiO.sub.2, Al.sub.2 O.sub.3 and B.sub.2 O.sub.3 and at least one of the trivalent oxides La.sub.2 O.sub.3 and Y.sub.2 O.sub.3 in quantities which in mole % have at the utmost the following value: SiO.sub.2 66.6, La.sub.2 O.sub.3 50, B.sub.2 O.sub.3 50, Y.sub.2 O.sub.3 50 and Al.sub.2 O.sub.3 70, the sealing material for obtaining the joint being applied at a temperature of not more than 1700.degree. C and the material of the joint obtained therewith being located in a composition range within a tetrahedron formed by the components Al.sub.2 O.sub.3 -La.sub.2 O.sub.3 -SiO.sub.2 -B.sub.2 O.sub.3, whose limits in the side planes of the tetrahedron are shown in the accompanying FIGS. 1, area a, 2, area a and 3, area a and which are further defined by the cross-sections in FIG. 8, area a, FIGS. 9, area a and FIG. 10, area a, or in a composition range located within a tetrahedron formed by the components Al.sub.2 O.sub.3 -La.sub.2 O.sub.3 -SiO.sub.2 -Y.sub.2 O.sub.3, whose limits in the side planes of the tetrahedron are shown in the FIGS. 1, area a and 4, area a, 6 area a and 7, area a.

2. A composite body as claimed in claim 1, wherein said sealing material is applied at a temperature of not more than 1600.degree. C and the material of the joint obtained therewith is located in a composition range within a tetrahedron, formed by the components Al.sub.2 O.sub.3 -La.sub.2 O.sub.3 -SiO.sub.2 -B.sub.2 O.sub.3, whose limits in the side planes of the tetrahedron are shown in the accompanying FIGS. 1, area b, 2, area b and 3, area a and which are further defined by the cross-sections in FIGS. 8, area b, 9, area b and 10, area b, or in a composition range located within a tetrahyedron formed by the components Al.sub.2 O.sub.3 -La.sub.2 O.sub.3 -SiO.sub.2 -Y.sub.2 O.sub.3 whose limits in the side planes of the tetrahedron are shown in the accompanying FIGS. 5, area b, 6, area b and 7, area b.

3. A composite body as claimed in claim 1, wherein said sealing material having La.sub.2 O.sub.3, Y.sub.2 O.sub.3, or mixtures thereof is wholly or partly replaced by one or more oxides of the lanthanides and of scandium.

4. A composite body as claimed in claim 1 wherein a total of not more than 20 mole % of one or more of the oxides TiO.sub.2, ZrO.sub.2 and HfO.sub.2 is present in the material of the joint.

5. A method of producing a composite body of the type claimed in claim 1, which comprises: coating at least one of said parts with a layer of sealing glass at the surface at which the joint is to be made, heating said parts in contact with one another to a temperature to approximately 100.degree. C above the softening temperature of the sealing glass, applying a pressure to the joint thereafter while said parts and said sealing glass and said joint is heated at a temperature of 150.degree. to 250.degree. C above the sealing glass softening point until said sealing glass crystallizes.

6. Apparatus as described in claim 1 wherein said two parts are made of densely sintered aluminum oxide and are a discharge tube and a closure member for said discharge tube, said apparatus further including an electrode feedthrough of molybdenum, a gas filling consisting of mercury vapour doped with a metal chloride, -bromide or -iodide, said aluminum oxide parts being joined together and to said molybdenum by means of said sealing material.