THERMOCOUPLE SYSTEM HAVING A TERMINAL END REGION
20170350767 · 2017-12-07
Assignee
Inventors
- Gilbert Braun (Herzogenrath, DE)
- Andreas Böttcher (Mettmann, DE)
- Olga Deiss (Düsseldorf, DE)
- Thomas Grieb (Krefeld, DE)
- Ljiljana Hanf (Mülheim an der Ruhr, DE)
- Jens Kleinfeld (Mülheim an der Ruhr, DE)
- Tobias Krieger (Oberhausen, DE)
- Fabian Sander (Mülheim, DE)
Cpc classification
G01K1/14
PHYSICS
G01K7/08
PHYSICS
International classification
G01K7/08
PHYSICS
G01K13/02
PHYSICS
Abstract
A thermocouple system, has a metal feedthrough having a cylindrical portion having an axis of symmetry and a terminal end region arranged thereon, which completely closes the cylindrical portion, and which has at least two passageways, the opening cross-section of which is smaller than the cross-sectional surface vertical to the axis of symmetry through the cylindrical portion. Through one passageway, a thermocouple is guided, and in the region of the passageway, the thermocouple is connected to the end region in a fluid-tight manner by way of a seal.
Claims
1. A thermocouple system comprising: a metal leadthrough with a cylindrical section with a symmetry axis and also a terminal end region, arranged thereon, which completely closes off the cylindrical section and has at least two passages, the opening cross section of which is smaller than the cross-sectional area perpendicularly to the symmetry axis through the cylindrical section, wherein a thermocouple is guided through a passage and in the region of the passage the thermocouple is connected to the terminal region in a fluid-tight manner by means of a seal.
2. The thermocouple system as claimed in claim 1, wherein the terminal region is at least partially of conical design.
3. The thermocouple system as claimed in claim 1, wherein the terminal region is at least partially of stepped design and at least two passages are introduced into different steps of the step-formed terminal region.
4. The thermocouple system as claimed in claim 1, wherein the seal is a solder which is preferably a soft solder or a hard solder.
5. The thermocouple system as claimed in claim 1, wherein all passages which are not provided with a thermocouple are also sealed in a fluid-tight manner.
6. The thermocouple system as claimed in claim 1, wherein the opening cross sections of the passages are at least 1.0 mm but at most 7.0 mm in diameter.
7. The thermocouple system as claimed in claim 1, wherein the passages are designed as holes which extend parallel to the symmetry axis of the cylindrical section.
8. The thermocouple system as claimed in claim 1, wherein the passages in the longitudinal direction through the material of the terminal region have a length of at least 1.0 mm and at most 10.0 mm.
9. The thermocouple system as claimed in claim 1, wherein tube sections are attached on the outer wall of the terminal region, which tube sections are in alignment with the passages and are fixed on the outer wall.
10. The thermocouple system as claimed in claim 1, wherein the fluid-tight seal between thermocouple and passage is of pressure-tight design up to 30 bar.
11. A gas turbine comprising: at least one thermocouple system as claimed in claim 1, wherein the thermocouple system is integrated into the outer casing of the gas turbine.
12. The thermocouple system as claimed in claim 2, wherein the openings of at least two passages on the conically formed outer wall of the terminal region have in the main different distances to the symmetry axis of the cylindrical section.
13. The thermocouple system as claimed in claim 4, wherein the seal is a soft solder or a hard solder.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0031] In this case, in the drawing:
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DETAILED DESCRIPTION OF INVENTION
[0038]
[0039] It is furthermore to be seen that provision is made for a symmetry axis S of the cylindrical section 10, which represents the rotational symmetry axis. The individual passages 12 in the terminal end region 11 are arranged in this case in a number or rings around this symmetry axis S, wherein the individual rings have a different number of passages 12. The individual passages 12 of a ring in each case are in the main equidistant to the respective adjacent passage 12, wherein advantageously the individual rings are also in the main equidistant to the respectively next adjacent ring.
[0040] The thermocouple system 1 can now be guided in its entirety through a suitable opening (not shown in the present case) on an outer casing of a working machine, wherein the cylindrical section 10 of the leadthrough 2 is suitably clamped in the outer casing. In this case, the cylindrical section 10 can for example be inserted into a suitable Swagelok socket and clamped therein. If it were now to be necessary to exchange the thermocouple 20, only the seal 15 would be removed in order to be able to withdraw the thermocouple 20 as a whole from the leadthrough 2. In this respect, the entire leadthrough 2 is no longer to be removed or destroyed but it is sufficient to manipulate just one part, i.e. a specific passage 12.
[0041] The embodiment shown in
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[0045]
[0046] Further embodiments are gathered from the dependent claims.