Machine arrangement

Abstract

A machine arrangement, comprising at least one carrier, wherein a glass fiber is connected with the machine arrangement. To allow a proper measurement of stresses even at curved surfaces of the machine arrangement, as it is typical in the case of a carrier being attached to bearing rings, the connection between the glass fiber and the machine arrangement is established by a metallic material which metal material is connected by material bonding with the machine arrangement as well as with the glass fiber.

Claims

1. An arrangement comprising a glass fiber connected to a carrier, the carrier being configured to be welded to a machine part, wherein the glass fiber is coated with a first metal, the first metal being materially bonded to the glass fiber, wherein the carrier includes a surface and a groove in the surface and wherein the glass fiber coated with the first metal is located in the groove, and including a brazing material in the groove materially bonded to the carrier and filling the groove to at least a level of the surface and holding the glass fiber coated with the first metal in the groove, and including a metallic material different than the first metal, the metallic material encasing the first metal, wherein the first metal consists essentially of chromium or consists essentially of nickel and wherein the metallic material is an alloy of chromium and nickel, and wherein the metallic material is materially bonded to the first metal and materially bonded to the brazing material.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) The drawings show embodiments of the invention.

(2) FIG. 1 shows in a perspective view a section of a carrier intended to be attached to an outer bearing ring of a roller bearing, on which a glass fiber is fixed,

(3) FIG. 2 shows the cross section A-A according to FIG. 1,

(4) FIG. 3 shows a perspective view of a glass fiber which is fixed to a carrier similar to FIG. 2,

(5) FIG. 4 shows a front view of a glass fiber which is fixed to a carrier, similar to FIG. 3,

(6) FIG. 5 shows a perspective view of a glass fiber which is fixed in a groove of a carrier,

(7) FIG. 6 shows a front view of a glass fiber which is fixed in a groove of a carrier, similar to FIG. 5,

(8) FIG. 7a shows the process of fixing a glass fiber in a groove of a carrier in a first, early state,

(9) FIG. 7b shows the process of fixing a glass fiber in a groove of a carrier in a second, later state,

(10) FIG. 8 shows a side sectioned view of a glass fiber core and a series of metallic coatings, and

(11) FIG. 9 shows a isometric view of a section showing a carrier mounted to an outer ring of a bearing, wherein the carrier supports the mounted optical fiber.

DETAILED DESCRIPTION OF THE INVENTION

(12) In FIG. 1 a machine arrangement 1 is shown being a carrier to be attached to an outer bearing ring of a roller bearing of the machine arrangement. The carrier 1 has an outer spherical surface which is to be monitored with respect to strains which act in the machine part. The survey of those strains is carried out by the fiber Bragg grating (FBG) method which is known as such. Reference is made e. g. to U.S. Pat. No. 6,923,048 B2 where this technology is explained in more detail.

(13) For doing so a glass fiber 2 is securely fixed on the spherical, i.e. cylindrical outer circumference of the carrier 1. The glass fiber 2 has a longitudinal direction L which extends in the circumferential direction of the carrier 1.

(14) Details concerning the fixation of the glass fiber 2 at the carrier 1 can be seen from FIG. 2.

(15) Here, it can be seen that the glass fiber 2 is basically the pure glass elementpossibly covered only by a reflective coating to ensure proper light conduction within the glass fiberwhich is then connected with the carrier 1 by means of metallic material 3.

(16) Here, two different metallic materials are employed:

(17) A first metallic material 3 coats the glass fiber 2 itself. The preferred material is chromium (Cr).

(18) The first metallic material 3 it then connected with a second metallic material 3. This material is preferably an alloy, preferably from chromium (Cr) and nickel (Ni).

(19) Thus, a material bonding is established between the glass fiber 2 and the machine part 1 to be monitored. This means, all strains in the machine part 1 are directly transferred into the glass fiber 2. Thus, the precondition is assured for a precise measurement of physical parameters of the machine part 1.

(20) In FIG. 3 a further embodiment of the invention is shown. Here, the glass fiber 2 is provided with a cladding 3 from a first metallic material being nickel (Ni). This cladding is embedded in a second metallic material 3 being a nickel-chromium-alloy. The second metallic material 3 is fixed on the carrier 1 by means of welding or brazing 4.

(21) In FIG. 4 a similar solution is shown. Here, the glass fiber 2 is again embedded in a cladding of nickel 3. This cladding is covered by a coating 3 of a nickel-chromium-alloy. This coating 3 is fixed with the carrier 1 by means of welding or brazing 4.

(22) In FIG. 5 an alternative is shown. Here the carrier 1 has a groove 5, in which the glass fiber 2 is inserted and securely fixed. For doing so, the glass fiber 2 is cladded with a cover 3 from nickel. Then, the covered glass fiber 2 is fixed on the carrier 1 by a nickel-chromium-alloy 3 which fills up the groove 5.

(23) A similar solution is shown in FIG. 6. Here, the carrier 1 again has a groove 5 in which the glass fiber 2 is inserted. The glass fiber 2 is embedded in a nickel cladding 3. The cladding 3 is embedded by a nickel-chromium-alloy 3. The fixation of the coating of nickel-chromium-alloy 3 is fixed in the groove 5 by means of welding or brazing 4.

(24) In FIG. 7a and FIG. 7b a process is depicted by which a fixation as shown in FIG. 6 can be realized. Here, a container 7 is arranged at the carrier 1 when the embedded glass fiber 2 (coated again by a nickel layer 3 and a layer form a nickel-chromium-alloy 3) is arranged in a groove 5 in the carrier 1. The container 7 is filled with braze paste 6. This is shown in FIG. 7a.

(25) Heating elements 8 being inductive heaters are arranged near the container 7. Due to the heat produced by the inductive heaters 8 the braze paste 6 melts and forms the brazing 4 which is shown in FIG. 7b. Afterwards, the container 7 is removed.

(26) The proposed connection technology can be used to fix a glass fiber 2 firmly between two points on the carrier 1 to use the fiber Bragg grating (FBG) method for measurement of specific data.

(27) For the cladding of the glass fiber 2 itself, pure materialspecifically nickel (Ni) or chromium (Cr)is preferred. This gives a very dense and defect free coating.

(28) For the outer coating a selection can be made from suitable alloys between nickel (Ni) and chromium (Cr) with or without additional elements such as B, Fe, Mn, Si, Ti, which can be selected to obtain a harder or more ductile coating and/or to reduce the melting temperature for the coating or later brazing or welding to be applied.

(29) Beside pure nickel also nickel can be used which is alloyed with a maximum of 2 weight-% titan (Ti), 1 weight-% silizium (Si) or a nickel-alloy with a maximum of 3.5 weight-% boron (B), 4.5 weight-% silizium (Si), between 5 and 7 weight-% chromium (Cr) and about 4 weight-% ferrum (Fe).

(30) For the outer coating 3 pure chromium (Cr) can be employed but also chromium alloyed with a maximum of 20 to 60 weight-% nickel (Ni). The outer coating has preferably between 0.2 to 0.5 mm wall thickness in order to enable microlaser welding or brazing,

(31) Here, a nickel-chromium-alloy is preferred with 20 to 80 weight-% nickel (Ni) and a balance of chromium (Cr). Also, an alloy has been found suitable with 20 to 70 weight-% nickel (Ni), 1 to 5 weight-% mangan (Mn), a maximum of 1 weight-% silizium (Si) and a balance of chromium (Cr). Also the addition of copper (Cu) can be beneficial.

(32) In FIG. 8 a glass fiber with core 82, suitably working up to 1000 degrees Centigrade, comprising an in-core Bragg grating 83 has been prepared to be vacuum brazed to a stainless steel carrier. The glass fiber 82 typically comprises a copper coating 84 which outside the attachment area 89 is protected by a thin layer of electroplated Ni 86 during activation. A thin chemical Ni layer 87 is then added to make the bare fiber part electrically conducting and finally an electroplated Ni-layer 88, about 20 micrometers thick is added. The length 89 along which the glass fiber 82 is to be mounted to a carrier will be bare before the Ni layers 87, 88 are added and will comprise one or more in-core Bragg gratings 83.

(33) In FIG. 9 a carrier 91, suitably of 430 stainless steel, is mounted on an outer ring 99 of a bearing. This is of course one of many different location on a bearing that the carrier can be mounted. The carrier described can suitably be mounted on any hardened steel, especially hardened bearing steel. The carrier 91 can suitably be in the range of 25 millimeter long in the direction of a mounted optical fiber 92, 5 millimeter wide and 1 millimeter thick. It is important that the carrier 91 is thin so that the optical fiber 92 is as close as possible to the part it is supposed to measure as the optical fiber is on one side and the machine part on the other side. The carrier 91 suitable comprises a groove with a diameter/depth in the range of 0.3 millimeter for a nickel coated optical fiber 92. A prepared optical fiber 92, suitably of the kind according to FIG. 8, is put in the groove and a filling material 94 is added between the nickel coated fibers and the stainless steel carrier 91. The filling material can suitably be brazing alloy Cusin-1 ABA paste. The optical fiber 92 is then embedded into the carrier 91 by brazing, suitably vacuum brazing. After the optical fiber 92 has been embedded into or onto the carrier 91, the carrier 91 is then attached to a machine part which is to be measured as to for example temperature and/or strain. The attachment of the carrier 91 to, as in this example, an outer bearing ring, is according to this embodiment done by pulse arc welding, such as micro TIG welding in an Argon atmosphere to form welds 98. The optical fiber 92 will then have a stiff connection with the machine part it is meant to measure.

REFERENCE NUMERALS

(34) 1 Machine arrangement (carrier) 2 Glass fiber 3 Metallic material 3 First metallic material 3 Second metallic material 4 Welding/Brazing 5 Groove 6 Braze paste 7 Container 8 Heating element (induction heating element) 82 Glass fiber with core, suitably working up to 1000 degrees C. 83 In-core Bragg grating 84 Copper, Cu, coating of fiber 86 Thin electroplated Ni to protect the Cu during activation 87 Thin chemical Ni layer to make the bare fiber part electrically conducting 88 Final electroplated Ni-layer, about 20 micrometers thick 89 Carrier mounting area 91 Carrier, suitably 430 stainless steel 92 Optical fiber, suitable working up to a 1000 degrees C. 94 Filling material, suitably brazing alloy Cusin-1 ABA paste 98 Pulse Arc welding, micro TIG (Tungsten Inert Gas) in Argon atmosphere L Longitudinal axis