The disclosure relates generally to accelerometers, and more particularly, to an insulated accelerometer assembly for a vibrating component in a high voltage environment.
Large industrial machines such as dynamoelectric machines (e.g., generators and motors) vibrate during operation such that monitoring of the vibrations is desired. For example, it is advantageous to monitor vibrations in a generator stator end winding. Because of the high voltage environment, this vibration monitoring is traditionally accomplished using fiber-optic based devices. These fiber-optic devices may use a variety of fiber-optic technologies such fiber bragg grating, intensity based, Fabry-Perot interferometers, etc. and typically measures in 1 or 2 axes. A significant number of sensors, e.g., a minimum of 6, per generator end are needed to gather an accurate representation of the stator end winding vibration. The need for so many expensive fiber-optic sensors leads to costly systems.
Electrical accelerometers, such as Piezoelectric or Micro Electro-Mechanical system (MEMs), are well-known systems to detect motion, and are significantly less expensive than fiber-optic based accelerometers. Accelerometers output signals indicative of the force/motion and are operatively connected to vibrating components for receipt of the signals. Use of electrical accelerometers in high voltage areas such as a generator end winding, however, presents a number of challenges because the sensors can offer a path to ground for the high voltage that can result in harmful scenarios. For example, these accelerometers may present a path for voltage discharge, voltage tracking and/or coronas that may potentially damage end winding components. Devices have been created to provide protection for the accelerometer so they can be used in a high voltage environment, but they require highly complex structural configurations.
A first aspect of the disclosure provides an insulated accelerometer assembly for a vibrated component in a high voltage environment, the assembly comprising: an accelerometer; a high dielectric strength potting compound encapsulating the accelerometer; a structurally supporting insulator layer surrounding at least a portion of the high dielectric strength potting compound; and a conductive layer over at least a portion of the structurally supporting insulator layer.
A second aspect of the disclosure provides a dynamoelectric machine comprising: a rotor; a stator including a plurality of stator end windings; an insulated accelerometer assembly coupled to at least one of the plurality of stator end windings, the assembly including: an accelerometer; a high dielectric strength potting compound encapsulating the accelerometer; a structurally supporting insulator layer surrounding at least a portion of the high dielectric strength potting compound; and a conductive layer over at least a portion of the glass epoxy layer.
The illustrative aspects of the present disclosure are designed to solve the problems herein described and/or other problems not discussed.
These and other features of this disclosure will be more readily understood from the following detailed description of the various aspects of the disclosure taken in conjunction with the accompanying drawings that depict various embodiments of the disclosure, in which:
It is noted that the drawings of the disclosure are not to scale. The drawings are intended to depict only typical aspects of the disclosure, and therefore should not be considered as limiting the scope of the disclosure. In the drawings, like numbering represents like elements between the drawings.
As indicated above, the disclosure provides an insulated accelerometer assembly for a vibrated component in a high voltage environment. A related dynamoelectric machine is also provided.
Referring to the drawings, and in particular the perspective view of
Turning to
In the example shown on the left of
With continuing reference to the perspective view of
High dielectric strength potting compound 132 may include any material, examples described herein, with a dielectric strength that can withstand 60,000 Volts repeatedly without a breakdown. In one embodiment, potting compound 132 may include, for example, a low to medium viscosity glycidyl ether epoxy resin and a low temperature cure amine hardener. In addition, the potting compound can contain a reactive epoxy diluent to reduce the viscosity of the resin. An example of a liquid, glycidyl ether epoxy resins is a Bisphenol A diglycidyl ether epoxy resins made by Dow Chemical (DER 332, epoxide equivalent weight 172-176, viscosity at 25° C. 4,000-6,000 centipoise (cps)). Mono-, di- and trifunctional epoxy diluents can be used to reduce the viscosity of the potting compound. Example monofunctional epoxy diluents may include: Araldite DY-A (2-ethylhexyl glycidyl ether, epoxide equivalent weight 202-235, viscosity at 25° C. 1-4 cps; example difunctional epoxy diluents may include: Araldite DY 026 (1,4-butanediol diglycidyl ether), epoxide equivalent weight 108-118, viscosity at 25° C.<15 cps; and example trifunctional epoxy diluents may include: Araldite DY-T (trimethylpropane triglycidyl ether), epoxide equivalent weight 111-143, viscosity at 25° C. 100-300 cps. The Araldite brand epoxy diluents are available from Huntsman Corp.; other diluents from other manufacturers may also be employed. Epoxy resins or the epoxy resins containing an epoxy diluent to reduce viscosity are cured with a hardener that will cure below approximately 120° C. One hardener example includes an amine with amino-hydrogen, NH, reactive groups. For example, a hardener may include an aliphatic amine, amidoamine, polyamide based amines and cycloaliphatic amines. An example hardener may include: Aradur 21 (trimethyl hexamethylene diamine), NH equivalent weight 40, viscosity at 25° C.<10 cps. The Aradur brand hardeners are available from Huntsman Corp.; other hardeners from other manufacturers may also be employed. The hardeners with NH functionality are compatible with each other and can be used in combinations to optimize properties such as the reactivity and viscosity of the potting compound.
High dielectric strength potting compound 132 may extend partially along lead 134, i.e., lead 134 is partially encapsulated by compound 132. High dielectric strength potting compound 132 may have any thickness necessary to insulate accelerometer 130, which depends on the size and shape of accelerometer 130. In one example, the compound can be approximately 0.6 centimeters on the sides, 3.8 cm on one end and 2.5 on the other end; however, the thickness may vary drastically depending on the accelerometer used. During formation, a vacuum can be used in the process to remove any air bubbles in high dielectric strength potting compound 132.
A structurally supporting insulator layer 138 surrounds at least a portion of high dielectric strength potting compound 132. Layer 138 may provide additional insulating capabilities and some structural support. In one embodiment, structurally supporting insulator layer 138 includes a glass epoxy layer 140 that may include any glass fabric with high temperature epoxy resin such as but not limited to that generally known as “G-11.” Such glass epoxy layer is available from a large number of suppliers such as Plastics International of Eden Prairie, Minn., USA and Polymer Plastics Company of Carson City, Nev., USA. Glass epoxy layer 140 may have a thickness ranging from approximately 0.0158 centimeters to 0.635 cm ( 1/16 inch to ¼ inch) and may preferably be approximately 0.317 cm (⅛ inch). In one embodiment, glass epoxy layer 140 may extend beyond an end 142 of high dielectric strength potting compound 132, creating an overhang 144. Overhang 144 provides additional protection to lead 134 to further prevent a direct current path to lead 134 (increases distance that must be traveled).
Assembly 120 may also include a conductive layer 146 over at least a portion of structurally supporting insulator layer 138. Conductive layer 146 may provide corona and partial discharge protection. In one embodiment, conductive layer 146 may include at least one conductive silicon carbide coating 148. The coating can be, for example, a polyester or epoxy resin based material having a grit in the range of 300 to 800. In the enlarged view in
Referring to
Referring to
Turning to
With continuing reference to the perspective view of
In contrast to the first embodiment, in this embodiment, structurally supporting insulator layer 138 may include a mica layer 240 surrounding at least a portion of high dielectric strength potting compound 232. In one embodiment, mica layer 240 may include a number of mica layer(s) 240. In any event, mica layer(s) 240 may provide additional insulating capabilities and some structural support. Mica layer(s) 240 may include any form of mica, e.g., a silicate mineral with a layered structure, found as minute scales in granite and other rocks, or as crystals. In one embodiment, mica layer(s) 240 may take the form of a tape, having adhesive on one or both sides so the layer can readily adhere to potting compound 232, lead 234 and each other. One example includes MICA 77956 manufactured by Vonn Roll; however, other mica layers from other manufacturers may also be employed. Mica layer 240 can be supported by glass cloth, films, or impregnated with a high property resin to obtain the needed electrical properties. Mica layer(s) 240 may have a thickness ranging from approximately 0.1-0.2 millimeters (mm) in thickness, and, in one example, approximately 10-20 layers of the tape may be applied to create a final thickness ranging from 1 mm-4 mm.
Assembly 220 may also include a conductive layer 246 over at least a portion of structurally supporting insulator layer 138, e.g., mica layer(s) 240. Conductive layer 246 may provide corona and partial discharge protection. As in the first embodiment, conductive layer 246 may include at least one conductive silicon carbide coating 248. In the enlarged view in
Referring to
Assemblies 120, 220 as described herein provide a significantly lower cost solution compared to fiber optics for monitoring vibration in a high voltage environment such as a stator end winding. The lower cost allows for more instrumentation to be placed on a generator.
The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the disclosure. As used herein, the singular forms “a”, “an” and “the” are intended to include the plural forms as well, unless the context clearly indicates otherwise. It will be further understood that the terms “comprises” and/or “comprising,” when used in this specification, specify the presence of stated features, integers, steps, operations, elements, and/or components, but do not preclude the presence or addition of one or more other features, integers, steps, operations, elements, components, and/or groups thereof. Where the term “approximately” or “about” is used, any value plus/minus 10% may be possible.
The corresponding structures, materials, acts, and equivalents of all means or step plus function elements in the claims below are intended to include any structure, material, or act for performing the function in combination with other claimed elements as specifically claimed. The description of the present disclosure has been presented for purposes of illustration and description, but is not intended to be exhaustive or limited to the disclosure in the form disclosed. Many modifications and variations will be apparent to those of ordinary skill in the art without departing from the scope and spirit of the disclosure. The embodiment was chosen and described in order to best explain the principles of the disclosure and the practical application, and to enable others of ordinary skill in the art to understand the disclosure for various embodiments with various modifications as are suited to the particular use contemplated.
Number | Name | Date | Kind |
---|---|---|---|
3042744 | Shoor | Jul 1962 | A |
4246161 | Smith et al. | Jan 1981 | A |
4417476 | Knowlton | Nov 1983 | A |
4477887 | Berni | Oct 1984 | A |
4513749 | Kino et al. | Apr 1985 | A |
4734976 | Matson | Apr 1988 | A |
4818909 | Balke | Apr 1989 | A |
5130600 | Tomita | Jul 1992 | A |
5146776 | Twerdochlib et al. | Sep 1992 | A |
5469745 | Twerdochlib | Nov 1995 | A |
5473941 | Judd | Dec 1995 | A |
5684718 | Jenkins et al. | Nov 1997 | A |
7276839 | Monahan | Oct 2007 | B1 |
7372279 | Thompson | May 2008 | B2 |
7533572 | Twerdochlib | May 2009 | B2 |
8051712 | Younsi | Nov 2011 | B2 |
8076909 | Diatzikis et al. | Dec 2011 | B2 |
8186223 | Dawson et al. | May 2012 | B2 |
8379225 | Koste et al. | Feb 2013 | B2 |
8422008 | Xia et al. | Apr 2013 | B2 |
8489363 | Piccirillo et al. | Jul 2013 | B2 |
8514409 | Koste et al. | Aug 2013 | B2 |
8520986 | Dailey | Aug 2013 | B2 |
20050052811 | Shrier | Mar 2005 | A1 |
20070247613 | Cloutier et al. | Oct 2007 | A1 |
20090284121 | Lenz | Nov 2009 | A1 |
20100223995 | Watanabe | Sep 2010 | A1 |
20110227872 | Huska | Sep 2011 | A1 |
20110242546 | Koste et al. | Oct 2011 | A1 |
20120086947 | Bazzone | Apr 2012 | A1 |
20120274258 | Andarawis et al. | Nov 2012 | A1 |
20140013843 | Buck et al. | Jan 2014 | A1 |
20150013791 | Banowetz et al. | Jan 2015 | A1 |
Number | Date | Country |
---|---|---|
102324268 | Jan 2012 | CN |
104101610 | Oct 2014 | CN |
0627616 | Dec 1994 | EP |
2244081 | Oct 2010 | EP |
2473903 | Mar 2011 | GB |
2479263 | Oct 2011 | GB |
2009079659 | Jun 2009 | WO |
Entry |
---|
SSA-100 High Sensitivity Fiber Bragg Grating Accelerometer, Aniber Company Limited, http://anibertech.com/SSA-100%20Accelerometer.html, date unknown, 3 pages. |
Turbo—condition monitoring solutions, VibroSystM, http://vibrosystm.com/energy/turbo-complete-monitoring-solutions/, date unknown, 2 pages. |
Micron Optics Accelerometer os7100, Micron Optics, Inc, 2009, 3 pages. |
Iris Power Endwinding Vibration Accelerometer (EVAII) Kit for Hydrogen-Cooled Generators, IRIS Power, Ver 1—Apr. 2015, date unknown, 2 pages. |
Iris Power EVTracll, Continuous On-Line Stator Endwinding Vibration Monitor, IRIS Power, Ver 4—Apr. 2015, date unknown, 4 pages. |
Extended European Search Report and Opinion issued in connection with corresponding EP Application No. 16185117.5 dated Oct. 24, 2016. |
Number | Date | Country | |
---|---|---|---|
20170059608 A1 | Mar 2017 | US |