The subject matter described herein relates in general to rotating machines and, more particularly, to vibration reduction in rotating machines.
Rotating machines are used for converting one type of energy input into a different type of energy output. Rotating machines are used in various applications, such as rotating vehicle wheels, generating energy from natural resources, and powering everyday appliances. Examples of rotating machines include motors and turbines.
In one respect, the present disclosure is directed to a rotating machine system. The rotating machine system can include a rotating machine. The rotating machine system can include a housing. The housing can include an inner surface. The housing can surround at least a portion of the rotating machine. The inner surface of the housing can be spaced from the rotating machine such that a space is defined therebetween. The rotating machine system can include one or more super elastic wires. The one or more super elastic wires can be positioned in the space and can be operatively connected to the rotating machine and to the inner surface of the housing.
In another respect, the present disclosure is directed to a rotating machine system. The rotating machine system can include a rotating machine. The rotating machine system can include a housing. The housing can include an inner surface. The housing can surround at least a portion of the rotating machine. The inner surface of the housing can be spaced from the rotating machine such that a space is defined therebetween. The rotating machine system can include one or more super elastic wires. The one or more super elastic wires can be positioned in the space and can be operatively connected in tension to the rotating machine and to the inner surface of the housing. The one or more super elastic wires can be stretched to a quasi-zero stiffness regime.
The high speed rotation of a rotating machine can cause the components of the rotating machine to vibrate. Other causes of vibration in rotating machines can include wear and tear on and/or misalignment of the components of the rotating machine, and/or bearing malfunctions, to name a few examples. Over time, vibration in rotating machines can cause mechanical failures within the rotating machine. Accordingly, arrangements described herein relate to vibration isolation for rotating machines.
A rotating machine system can include a rotating machine and a housing. The housing can include an inner surface, and the housing can surround at least a portion of the rotating machine. The inner surface of the housing can be spaced from the rotating machine such that a space is defined therebetween. The rotating machine system can include one or more super elastic wires positioned in the space and operatively connected to the rotating machine and to the inner surface of the housing. The one or more super elastic wires can reduce vibration in the rotating machine system.
Detailed embodiments are disclosed herein; however, it is to be understood that the disclosed embodiments are intended only as examples. Therefore, specific structural and functional details disclosed herein are not to be interpreted as limiting, but merely as a basis for the claims and as a representative basis for teaching one skilled in the art to variously employ the aspects herein in virtually any appropriately detailed structure. Further, the terms and phrases used herein are not intended to be limiting but rather to provide an understandable description of possible implementations. Various embodiments are shown in
It will be appreciated that for simplicity and clarity of illustration, where appropriate, reference numerals have been repeated among the different figures to indicate corresponding or analogous elements. In addition, numerous specific details are set forth in order to provide a thorough understanding of the embodiments described herein. However, it will be understood by those of ordinary skill in the art that the embodiments described herein can be practiced without these specific details.
Referring to
The rotating machine system 10 can include a rotating machine 12, a housing 14, and one or more super elastic wires 16. The various elements of the rotating machine system 10 can be operatively connected to each other (or any combination thereof). As used herein, the term “operatively connected” can include direct or indirect connections, including connections without direct physical contact.
Each of the above noted elements of the rotating machine system 10 will be described in turn below. The rotating machine 12 can be any suitable rotating machine, including a motor, a turbine, or a generator, just to name a few examples. The rotating machine 12 can include one or more stationary components and one or more rotating components. In some arrangements, the rotating machine 12 can include a stator, rotor, and/or central shaft 18. The rotating machine 12 can be configured to rotate at a high rate. The rotating machine 12 can have an axis of rotation 19.
The rotating machine system 10 can include a housing 14. At least a portion of the rotating machine 12 can be located within the housing 14, which can protect the rotating machine 12 or one or more components thereof. The housing 14 can include an inner surface 20 and an outer surface 22. In some arrangements, the housing 14 can be substantially cylindrical in shape, but the housing 14 can be any other suitable shape. In some arrangements, the inner surface 20 can be substantially cylindrical in shape, but other suitable shapes for the inner surface 20 are possible.
The inner surface 20 can surround at least a portion of the rotating machine 12. The housing 14 can be spaced from the rotating machine 12 such that there is a space 24 between the rotating machine 12 and the inner surface 20. The space 24 can include an upper region 26 and a lower region 28. The terms “upper” and “lower” are used for convenience to indicate the relative location of the region in the operative position of the rotating machine system 10. The space 24 can be substantially constant in one or more directions. For example, the space 24 can be substantially constant in the axial direction A, a circumferential direction C, and/or a radial direction R. The axial direction A can be a direction that is coaxial with and/or substantially parallel to the axis of rotation 19, which can be represented by point A in a direction into and/or out of the page. The circumferential direction C can be the direction about the axis of rotation 19. The radial direction R can be any direction extending substantially radially outward from the axial direction A toward the inner surface 20.
The rotating machine 12 can include one or more super elastic wires 16. The super elastic wire(s) 16 can be positioned in the space 24 between the rotating machine 12 and the inner surface 20. The super elastic wire(s) 16 can be operatively connected to the rotating machine 12 and to the inner surface 20.
The super elastic wire(s) 16 can be operatively connected to the rotating machine 12 and to the inner surface 20 in any suitable manner. For example, the super elastic wire(s) 16 can be operatively connected to the rotating machine 12 and/or to the inner surface 20 by one or more fasteners, one or more adhesives, one or more forms of mechanical engagement, and/or any combination thereof.
Referring to
Also shown in
In other examples, the super elastic wire(s) 16 can be operatively connected to the rotating machine 12 and to the inner surface 20 directly. For example, the super elastic wire(s) 16 can be operatively connected to the rotating machine 12 and to the inner surface 20 by one or more screws, one or more nails, one or more adhesives, and/or one or more forms of mechanical engagement, or any combination thereof. As a result, the super elastic wire(s) 16 can directly contact the inner surface 20.
The super elastic wire(s) 16 can be positioned in the space 24 and operatively connected to the rotating machine 12 and to the inner surface 20 in any suitable arrangement. In one or more arrangements, such as is shown in
In other arrangements, such as is shown in
As described above in connection with
In some examples, such as is shown in
In other examples, such as is shown in
The super elastic wire(s) 16 can be operatively connected to the rotating machine 12 and to the inner surface 20 such that the super elastic wire(s) 16 form a row 38 substantially in the circumferential direction C about the rotating machine 12. The row 38 of super elastic wire(s) 16 can be substantially perpendicular relative to the axial direction A of the rotating machine 12.
In some arrangements, the rotating machine system 10 can include a plurality of rows 38 of super elastic wires 16, as shown in
In some arrangements, the super elastic wire(s) 16 can be operatively connected to the rotating machine 12 and to the inner surface 20 such that the super elastic wire(s) 16 are stretched in tension. As such, the rotating machine 12 can be suspended within the housing 14 by the super elastic wire(s) 16. The tension of the super elastic wire(s) 16 can be varied in any suitable manner. In some examples, the super elastic wire(s) 16 can be pre-stretched before they are operatively connected to the rotating machine 12 and to the inner surface 20. In other examples, the super elastic wire(s) 16 can be operatively connected to the rotating machine 12 and to the inner surface 20 before being stretched. In some examples, the super elastic wire(s) 16 can be stretched, for example, by adjusting the fasteners 30 and//or by manual stretching.
In arrangements including a plurality of super elastic wires 16, each of the plurality of super elastic wires 16 can have a predetermined stiffness. In some examples, each of the plurality of super elastic wires 16 can have substantially the same predetermined stiffness. In other examples, the predetermined stiffness of one or more of the plurality of super elastic wires 16 can be different from the other super elastic wires 16. In some examples, the predetermined stiffness of each of the plurality of super elastic wires 16 can vary based on one or more characteristics of the rotating machine 12. For example, the predetermined stiffness of each of the plurality of super elastic wires 16 can vary to account for the load caused by the weight of the rotating machine 12. In this example, the super elastic wires 16 in a lower region 28 of the space 24 can have a higher predetermined stiffness compared to the super elastic wires 16 in an upper region 26 of the space 24.
The super elastic wire(s) 16 can be made of any suitable super elastic material. One example of a super elastic wire is AdrenaLine™, which is available from Miga Motor Company, Silverton, Oreg. Another example of a super elastic wire is Furukawa Ni—Ti Alloy, which is available from Furukawa Techno Material Co., Ltd., Kanagawa, Japan. In other examples, the super elastic material can be shape memory alloy.
A super elastic material is a material that exhibits two primary properties under certain conditions: superelasticity and quasi-zero stiffness. These properties are depicted in the stress-strain curve 70 shown in
While the super elastic material is described herein as being a wire, it will be understood that the super elastic material is not limited to being a wire. In other examples, the super elastic material can take the form of cables, tubes, and/or other structures, just to name a few examples. Additionally or alternatively, the super elastic material may include an insulated coating.
It will be appreciated that the arrangements described herein can provide numerous benefits, including one or more of the benefits mentioned herein. For example, the arrangements described herein can reduce vibrations within a rotating machine and stabilize the rotating machine within the housing. The arrangements described herein can also improve the rate of wear of the rotating machine and the operability of the rotating machine. Moreover, the arrangements described herein can also reduce the occurrence of mechanical failures within the rotating machine.
The terms “a” and “an,” as used herein, are defined as one or more than one. The term “plurality,” as used herein, is defined as two or more than two. The term “another,” as used herein, is defined as at least a second or more. The terms “including” and/or “having,” as used herein, are defined as comprising (i.e., open language). The phrase “at least one of . . . and . . . ,” as used herein refers to and encompasses any and all possible combinations of one or more of the associated listed items. As an example, the phrase “at least one of A, B, and C” includes A only, B only, C only, or any combination thereof (e.g. AB, AC, BC, or ABC). As used herein, the term “substantially” or “about” includes exactly the term it modifies and slight variations therefrom. Thus, the term “substantially parallel” means exactly parallel and slight variations therefrom. “Slight variations therefrom” can include within 15 degrees/percent/units or less, within 14 degrees/percent/units or less, within 13 degrees/percent/units or less, within 12 degrees/percent/units or less, within 11 degrees/percent/units or less, within 10 degrees/percent/units or less, within 9 degrees/percent/units or less, within 8 degrees/percent/units or less, within 7 degrees/percent/units or less, within 6 degrees/percent/units or less, within 5 degrees/percent/units or less, within 4 degrees/percent/units or less, within 3 degrees/percent/units or less, within 2 degrees/percent/units or less, or within 1 degree/percent/unit or less. In some examples, “substantially” can include being within normal manufacturing tolerances.
Aspects herein can be embodied in other forms without departing from the spirit or essential attributes thereof. Accordingly, reference should be made to the following claims, rather than to the foregoing specification, as indicating the scope of the invention.
This application claims the benefit of U.S. Provisional Application No. 63/128,519, filed on Dec. 21, 2020, which is incorporated herein by reference in its entirety.
Number | Name | Date | Kind |
---|---|---|---|
82276 | Bellerille | Sep 1868 | A |
1826597 | Brecht | Oct 1931 | A |
2121835 | Sproul | Jun 1938 | A |
2655935 | Kinzbach | Oct 1953 | A |
2991655 | Jorgensen | Jul 1961 | A |
3394631 | Thompson | Jul 1968 | A |
3430942 | MacGlashan | Mar 1969 | A |
3559512 | Aggarwal | Feb 1971 | A |
3574347 | Hughes | Apr 1971 | A |
3608883 | Russold | Sep 1971 | A |
3743266 | Sturman et al. | Jul 1973 | A |
3836195 | Teeri | Sep 1974 | A |
3856242 | Cook | Dec 1974 | A |
3858665 | Winkler | Jan 1975 | A |
3873079 | Kuus | Mar 1975 | A |
3980016 | Taylor | Sep 1976 | A |
4168101 | DiGrande | Sep 1979 | A |
4215841 | Herring, Jr. | Aug 1980 | A |
4351556 | Worringer | Sep 1982 | A |
4457213 | Morgan | Jul 1984 | A |
4522447 | Snyder et al. | Jun 1985 | A |
4530491 | Bucksbee et al. | Jul 1985 | A |
4612429 | Milianowicz | Sep 1986 | A |
4824338 | Eickmann | Apr 1989 | A |
4799654 | Eickmann | Jun 1989 | A |
4898426 | Schulz et al. | Feb 1990 | A |
5178357 | Platus | Jan 1993 | A |
5222709 | Culley, Jr. et al. | Jun 1993 | A |
5263694 | Smith et al. | Nov 1993 | A |
5310157 | Platus | May 1994 | A |
5390903 | Fidziukiewicz | Feb 1995 | A |
5482351 | Young et al. | Jan 1996 | A |
5662376 | Breuer et al. | Sep 1997 | A |
5669594 | Platus | Sep 1997 | A |
5669598 | Ticey et al. | Sep 1997 | A |
5747140 | Heerklotz | May 1998 | A |
5842312 | Krumme et al. | Dec 1998 | A |
6025080 | Soroushian | Feb 2000 | A |
6142563 | Townsend et al. | Nov 2000 | A |
6290037 | Williams | Sep 2001 | B1 |
6354556 | Ritchie et al. | Mar 2002 | B1 |
6796408 | Sherwin | Sep 2004 | B2 |
6896324 | Kull et al. | May 2005 | B1 |
6935693 | Janscha | Aug 2005 | B2 |
6939097 | Carr et al. | Sep 2005 | B2 |
7100990 | Kimura et al. | Sep 2006 | B2 |
7152839 | Mullinix et al. | Dec 2006 | B2 |
7411331 | Dubowski et al. | Aug 2008 | B2 |
7506937 | Bequet | Mar 2009 | B2 |
7661764 | Ali et al. | Feb 2010 | B2 |
7703281 | Kosaka et al. | Apr 2010 | B2 |
7717520 | Boren et al. | May 2010 | B2 |
7822522 | Wereley et al. | Oct 2010 | B2 |
7971939 | Fujita et al. | Jul 2011 | B2 |
8166626 | Sereni et al. | May 2012 | B2 |
8185988 | Wieland | May 2012 | B2 |
8328962 | Schussler | Dec 2012 | B2 |
8366082 | Evans | Feb 2013 | B2 |
8585026 | Dittmar | Nov 2013 | B2 |
8793821 | Fowkes et al. | Aug 2014 | B2 |
8899393 | Kraner et al. | Dec 2014 | B2 |
8919751 | Kneidel | Dec 2014 | B2 |
9154024 | Jore et al. | Oct 2015 | B2 |
9194452 | Hawkins et al. | Nov 2015 | B2 |
9327847 | Platus | May 2016 | B2 |
9370982 | Siuissa | Jun 2016 | B2 |
9394950 | Henry et al. | Jul 2016 | B1 |
9399320 | Johnson et al. | Jul 2016 | B2 |
9408428 | Gaudet | Aug 2016 | B2 |
9447839 | Dunning | Sep 2016 | B2 |
9731828 | Lichota | Aug 2017 | B2 |
9791014 | McKnight et al. | Oct 2017 | B1 |
9920793 | Churchill et al. | Mar 2018 | B1 |
9994136 | Nakada | Jun 2018 | B2 |
10233991 | Churchill et al. | Mar 2019 | B2 |
10357955 | Ziolek | Jul 2019 | B2 |
10371229 | Gandhi et al. | Aug 2019 | B2 |
10479246 | Meingast et al. | Nov 2019 | B2 |
10677310 | Gandhi et al. | Jun 2020 | B2 |
11021998 | Ganiger | Jun 2021 | B2 |
20040145230 | Snyder et al. | Jul 2004 | A1 |
20040245830 | Scheck et al. | Dec 2004 | A1 |
20060101803 | White | May 2006 | A1 |
20060101807 | Wood | May 2006 | A1 |
20070138720 | Evans | Jun 2007 | A1 |
20070236071 | Fujita et al. | Oct 2007 | A1 |
20080181763 | Webster | Jul 2008 | A1 |
20090025833 | Schussler | Jan 2009 | A1 |
20090126288 | Fanucci | May 2009 | A1 |
20100001568 | Trybus et al. | Jan 2010 | A1 |
20100283887 | Topliss et al. | Nov 2010 | A1 |
20120018577 | Quiroz-Hernandez | Jan 2012 | A1 |
20140265468 | Greenhill et al. | Sep 2014 | A1 |
20150130220 | Preisler et al. | May 2015 | A1 |
20150298580 | Kanai | Oct 2015 | A1 |
20150346507 | Howarth | Dec 2015 | A1 |
20160009156 | Leonard et al. | Jan 2016 | A1 |
20160032997 | Seepersad et al. | Feb 2016 | A1 |
20160068085 | Mindel et al. | Mar 2016 | A1 |
20170009601 | Szwedowicz | Jan 2017 | A1 |
20170158104 | Le et al. | Jun 2017 | A1 |
20180195570 | Churchill et al. | Jul 2018 | A1 |
20180195571 | Churchill et al. | Jul 2018 | A1 |
20180312086 | Meigast et al. | Nov 2018 | A1 |
20190186588 | Gandhi et al. | Jun 2019 | A1 |
20190186589 | Gandhi et al. | Jun 2019 | A1 |
20210107623 | Barrett | Apr 2021 | A1 |
Number | Date | Country |
---|---|---|
202811955 | Mar 2013 | CN |
104062461 | Sep 2014 | CN |
204774820 | Nov 2015 | CN |
103147511 | Apr 2016 | CN |
108240415 | Jul 2018 | CN |
108757799 | Nov 2018 | CN |
109540493 | Mar 2019 | CN |
109932805 | Jun 2019 | CN |
102010003594 | Oct 2011 | DE |
H0614980 | Feb 1994 | JP |
2011201378 | Oct 2011 | JP |
2014180009 | Nov 2014 | WO |
Entry |
---|
Williams et al., “Dynamic modelling of a shape memory alloy adaptive tuned vibration absorber,” Journal of Sound and Vibration 280, Dec. 4, 2003, pp. 211-234 (24 pages). |
Araki et al., “Integrated mechanical and material design of quasi-zero stiffness vibration isolator with superelastic Cu—Al—Mn shape memory alloy bars,” Journal of Sound and Vibration, Dec. 2015, pp. 1-19 (34 pages). |
Casciati et al., “Performance of a base isolator with shape memory alloy bars,” Earthquake Engineering and Engineering Vibration, vol. 6, No. 4, Dec. 2007, pp. 401-408 (8 pages). |
Morsch et al., “Design of a Generic Zero Stiffness Compliant Joint,” Proceedings of the ASME 2010 International Design Engineering Technical Conferences & Computers and Information in Engineering Conference, Aug. 15-18, 2010, pp. 1-9 (10 pages). |
Miga Motor Company, “Miga Adrenaline—A Space Age Wire,” retrieved from the Internet: <https://migamotors.com/index.php?main_page=product_info&cPath=1&products_id=37>, [retrieved Mar. 26, 2021] (1 page). |
Furukawa Techno Material, “Shape Memory Alloys & Super-elastic Alloys,” retrieved from the Internet: <https://www.furukawa-ftm.com/english/nt-e/product.htm>, [retrieved Mar. 26, 2021] (3 pages). |
Le et al., “A vibration isolation system in low frequency excitation region using negative stiffness structure for vehicle seat,” Journal of Sound and Vibration, vol. 330, Issue 26, Dec. 19, 2011, pp. 6311-6335 (25 pages). |
Lee et al., “A multi-stage high-speed railroad vibration isolation system with “negative” stiffness,” Journal of Sound and Vibration, vol. 331, Issue 4, Feb. 13, 2012, pp. 914-921 (8 pages). |
Lee et al., “Position control of seat suspension with minimum stiffness,” Journal of Sound and Vibration, vol. 292, Issues 1-2, Apr. 25, 2006, pp. 435-442 (8 pages). |
Carrella et al., “Demonstrator to show the effects of negative stiffness on the natural frequency of a simple oscillator,” Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science, Jul. 14, 2008, pp. 1189-1192 (4 pages). |
Le et al., “Experimental investigation of a vibration isolation system using negative stiffness structure,” International Journal of Mechanical Sciences, vol. 70, May 2013, pp. 99-112 (14 pages). |
Shan et al., “Rigidity-tuning conductive elastomer,” Smart Materials and Structures, 2015, pp. 1-9 (10 pages). |
Correa et al., “Mechanical design of negative stiffness honeycomb materials,” Integrating Materials and Manufacturing Innovation, 2015, pp. 1-11 (11 pages). |
Ferguson-Pell, “Seat Cushion Selection,” JRRD Clinical Supplement No. 2: Choosing a Wheelchair System, 1990, pp. 49-73 (25 pages). |
Number | Date | Country | |
---|---|---|---|
20220196109 A1 | Jun 2022 | US |
Number | Date | Country | |
---|---|---|---|
63128519 | Dec 2020 | US |