Pneumatic vibration isolator utilizing an elastomeric element for isolation and attenuation of horizontal vibration

Information

  • Patent Grant
  • 6619611
  • Patent Number
    6,619,611
  • Date Filed
    Monday, July 2, 2001
    23 years ago
  • Date Issued
    Tuesday, September 16, 2003
    21 years ago
Abstract
A vibration isolator that has an elastomer which couples a support plate to a piston. The elastomer can provide horizontal damping of a payload that is coupled to the support plate. The piston can move within a first housing inner chamber that is in fluid communication with a second housing inner chamber. The chambers are pressurized with air that can flow to dampen vertical movement of the piston. The vibration isolator of the present invention thus provides both vertical and horizontal damping without using any oils.
Description




BACKGROUND OF THE INVENTION




1. Field of the Invention




The present invention relates to a vibration isolator that can dampen payload movement in both vertical and horizontal directions.




2. Background Information




Vibration isolators are used to isolate and damp vibration loads on an adjoining structure that is commonly referred to as a payload. The payload may be a table that is part of a semiconductor wafer fabrication system. The payload may be subjected to shock/vibration loads in both a vertical direction and a horizontal direction. For this reason vibration isolators are designed to dampen energy applied in both the vertical and horizontal directions.




U.S. Pat. No. 3,784,146 issued to Matthews discloses a vibration isolator which contains a piston that is coupled to a support plate by a plurality of cables. The piston is located within an air cylinder that can dampen vertical shock/vibration loads applied by the payload.




The cables allow the support plate to move within an inner cavity of the piston. The piston inner cavity includes a damping fluid that dampens shock/vibration loads applied in the horizontal direction.




It has been found that the damping oil will sometimes leak, thereby requiring a repair or replacement of the vibration isolator. Leaking fluid may therefore reduce the effective life of the isolator. Additionally, having to seal and charge a vibration isolator with damping fluid increases the cost of mass producing the isolator.




BRIEF SUMMARY OF THE INVENTION




One embodiment of the present invention includes a vibration isolator that has an elastomer, which couples a support plate to a piston. The piston can move within an inner chamber of an isolator housing.











BRIEF DESCRIPTION OF THE DRAWINGS





FIG. 1

is a cross-sectional view of an embodiment of a vibration isolator of the present invention;





FIG. 2

is a cross-sectional view of an alternate embodiment of the vibration isolator.











DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT




The applicants disclose a vibration isolator that has an elastomer, which couples a support plate to a piston. The elastomer can provide horizontal damping of a payload that is coupled to the support plate. The vibration isolator does not require the cables and damping fluid typically found in isolators of the prior art. The piston can move within a first housing inner chamber that is in communication with a second housing inner chamber. The chambers are pressurized with air that can flow to dampen vertical movement of the piston. The vibration isolator of the present invention thus provides both vertical and horizontal damping without using any oil. Additionally, the elastomer provides high damping, short settling time, and a “soft” stop of payload motion.




Referring to the drawings more particularly by reference numbers,

FIG. 1

shows an embodiment of a vibration isolator


10


of the present invention. The isolator


10


includes a support plate


12


that is coupled to a payload


14


. The payload


14


may be any structure that is to be isolated such as an optical bench or the base of an x-y table. The payload


14


may move in a vertical direction or a horizontal direction as indicated by the arrows.




The support plate


12


is coupled to a piston


16


by an elastomer


18


. The piston


16


is coupled to an isolator housing


20


by a diaphragm


22


. The elastomer


18


is constructed to be smaller than an inner cavity


24


of the piston


16


to allow elastomer deflection when the payload


14


moves in a horizontal direction.




The elastomer


18


is typically constructed from a rubber or other damping material that will dissipate energy transmitted from the payload


14


into the support plate


12


. Elastomeric materials may have a higher damping coefficient and a faster settling time than oil damping fluid. Additionally, the elastomer


18


has a higher shear stiffness that will provide a “soft” stop for the payload. The elastomer


18


is also stiff enough to withstand shock loads applied in the vertical direction.




It is desirable to provide an elastomer


18


that does not buckle under certain vertical loads. To increase the buckling load the elastomer


18


may have a conical shape. The narrow portion of the elastomer


18


may be attached to the top surface of the piston inner cavity


24


. This allows the elastomer


18


to sit deeper into the inner cavity


24


and improves the stability of the system. Although a conical shape is shown and described, it is to be understood that the elastomer


18


may have other shapes such as cylindrical, rectangular or square. These shapes are not an exhaustive list of the elastomer profiles. To decrease stiffness the elastomer


18


may also have an inner cavity


26


. The elastomer


18


shown in

FIG. 1

also described in U.S. Pat. No. 6,398,407 Apr. 22, 2003, which is hereby incorporated by reference. Although an embodiment showing the narrow portion of the elastomer


18


attached to the piston


16


is shown and described, the wider portion of the elastomer


18


may be attached to the piston


16


.





FIG. 2

shows an alternate embodiment of the vibration isolator


10


′ wherein the elastomer


18


′ has a laminated construction. The laminated elastomer


18


′ may have a plurality of metal plates


28


that separate a number of damping layers


30


. The damping layers


30


are constructed from a damping material such as rubber. The laminated structure has higher load capacity and vertical stiffness, as well as high rotational (tilt) stiffness, which improves the stability of the system, whereas the isolation in the horizontal direction remains good due to low stiffness of elastomeric layers in the horizontal (shear) direction.




Referring to

FIG. 1

, the piston


16


can move within a first inner chamber


30


of the isolator housing


20


. The first inner chamber


30


is in communication with a second inner chamber


32


of the housing


30


through an orifice


34


. The inner chambers


30


and


34


are pressurized with air at a pressure greater than atmospheric pressure through a leveling port


36


.




Vertical movement of the payload


14


will move the piston


16


within the first inner chamber


30


. The piston movement will induce air flow between the first


30


and second


32


chambers through the valve


34


. The air flow absorbs and dampens energy transferred from the payload


14


. The vibration isolator


10


of the present invention is thus able to dampen energy in both the vertical and horizontal directions.




While certain exemplary embodiments have been described and shown in the accompanying drawings, it is to be understood that such embodiments are merely illustrative of and not restrictive on the broad invention, and that this invention not be limited to the specific constructions and arrangements shown and described, since various other modifications may occur to those ordinarily skilled in the art.



Claims
  • 1. A vibration isolator, comprising:a housing which has a first inner chamber; a piston that can move within said first inner chamber of said housing; a diaphragm coupled to said piston and said housing; a support plate; and, an elastomer that is attached to and contiguous with said support plate and attached to said piston.
  • 2. The vibration isolator of claim 1, wherein said elastomer has a conical shape.
  • 3. The vibration isolator of claim 1, wherein said elastomer has an inner cavity.
  • 4. The vibration isolator of claim 1, wherein said elastomer includes a plurality of plates and a plurality of damping layers.
  • 5. The vibration isolator of claim 1, further comprising a valve that provides fluid communication between a second inner chamber and said first inner chamber.
  • 6. The vibration isolator of claim 5, wherein said first and second inner chambers contain a pressurized air.
  • 7. The vibration isolator of claim 1, wherein said elastomer can be deflected within an inner cavity of said piston.
  • 8. A vibration isolator, comprising:a housing which has a first inner chamber; a piston that can move within said first inner chamber of said housing; a diaphragm coupled to said piston and said housing; a support plate; and, coupling means for attaching said support plate directly to said piston.
  • 9. The vibration isolator of claim 8, wherein said coupling means includes an elastomer.
  • 10. The vibration isolator of claim 9, wherein said elastomer has a conical shape.
  • 11. The vibration isolator of claim 9, wherein said elastomer has an inner cavity.
  • 12. The vibration isolator of claim 9, wherein said elastomer includes a plurality of plates, and a plurality of damping layers.
  • 13. The vibration isolator of claim 9, wherein said elastomer can be deflected within an inner cavity of said piston.
  • 14. The vibration isolator of claim 8, further comprising an orifice that provides fluid communication between a second inner chamber and said first inner chamber.
  • 15. The vibration isolator of claim 14, wherein said first and second inner chambers contain a pressurized air.
  • 16. A method for damping a payload coupled to a support plate of a vibration isolator, comprising:moving the payload in a horizontal direction, which movement deflects an elastomer that is attached to and contiguous with a support plate and attached to a piston, the piston being coupled to a housing by a diaphragm.
  • 17. The method of claim 16, further comprising moving the payload in a vertical direction wherein the piston moves within a first inner housing chamber to induce flow of air into a second inner housing chamber.
  • 18. A vibration isolator, comprising:a housing which has a first inner chamber; a piston that has an inner cavity and can move within said first inner chamber of said housing; a support plate; and, an elastomer that is attached to and contiguous with said support plate and attached to said inner cavity of said piston.
  • 19. The vibration isolator of claim 18, wherein said elastomer has a conical shape.
  • 20. The vibration isolator of claim 18, wherein said elastomer has an inner cavity.
  • 21. The vibration isolator of claim 18, wherein said elastomer includes a plurality of plates and a plurality of damping layers.
  • 22. The vibration isolator of claim 18, further comprising a valve that provides fluid communication between a second inner chamber and said second inner chamber.
  • 23. The vibration isolator of claim 22, wherein said first and second inner chambers contain a pressurized air.
  • 24. A vibration isolator, comprising:a housing which has a first inner chamber; a piston that has an inner cavity and can move within said first inner chamber of said housing; a support plate; and, coupling means for attaching said support plate directly to inner cavity of said piston.
  • 25. The vibration isolator of claim 24, wherein said coupling means includes an elastomer.
  • 26. The vibration isolator of claim 25, wherein said elastomer has a conical shape.
  • 27. The vibration isolator of claim 25, wherein said elastomer has an inner cavity.
  • 28. The vibration isolator of claim 25, wherein said elastomer includes a plurality of plates, and a plurality of damping layers.
  • 29. The vibration isolator of claim 24, further comprising an orifice that provides fluid communication between a second inner chamber and said second inner chamber.
  • 30. The vibration isolator of claim 29, wherein said first and second inner chambers contain a pressurized air.
  • 31. A method for damping a payload coupled to a support plate of a vibration isolator, comprising:moving the payload in a horizontal direction, which movement deflects an elastomer that is attached to and contiguous with a support plate and attached to an inner cavity of a piston.
  • 32. The method of claim 31, further comprising moving the payload in a vertical direction wherein the piston moves within a first inner housing chamber to induce flow of air into a second inner housing chamber.
US Referenced Citations (184)
Number Name Date Kind
1143165 Begusch Jun 1915 A
1306906 Jaques, Sr. Jun 1919 A
2367139 Ress Jan 1945 A
3357268 Richter Dec 1967 A
3442475 Rivin May 1969 A
3460786 Rivin Aug 1969 A
3478608 Met Nov 1969 A
3533012 Johnson et al. Oct 1970 A
3565515 De Mey, II Feb 1971 A
3577791 Vanden Broek May 1971 A
3578278 Pickering May 1971 A
3601476 MacKenzie Aug 1971 A
3620558 MacMillan Nov 1971 A
3667525 Spieth Jun 1972 A
3751025 Beery et al. Aug 1973 A
3917201 Roll Nov 1975 A
3945246 Wadensten Mar 1976 A
4030811 Khoe et al. Jun 1977 A
4065203 Goell et al. Dec 1977 A
4079404 Comerford et al. Mar 1978 A
4088396 Edelstein May 1978 A
4119363 Camlibel et al. Oct 1978 A
4144504 Leggett et al. Mar 1979 A
4164363 Hsu Aug 1979 A
4167744 Nyul Sep 1979 A
4199222 Ikushima et al. Apr 1980 A
4237474 Ladany Dec 1980 A
4268113 Noel, Jr. May 1981 A
4295152 Khoe et al. Oct 1981 A
4296998 Dufft Oct 1981 A
4316678 F'Geppert Feb 1982 A
4332469 Wendland Jun 1982 A
4350867 Kinoshita et al. Sep 1982 A
4355323 Kock Oct 1982 A
4357072 Goodfellow et al. Nov 1982 A
4387956 Cline Jun 1983 A
4403243 Hakamada Sep 1983 A
4435037 Abramson et al. Mar 1984 A
4469399 Cowen et al. Sep 1984 A
4469929 Rosen et al. Sep 1984 A
4479698 Landis et al. Oct 1984 A
4500165 Scholl et al. Feb 1985 A
4506108 Kersch et al. Mar 1985 A
4523802 Sakaguchi et al. Jun 1985 A
4523810 Goss et al. Jun 1985 A
4525659 Imahashi et al. Jun 1985 A
4550410 Chenausky et al. Oct 1985 A
4615031 Eales et al. Sep 1986 A
4623220 Grabbe et al. Nov 1986 A
4647147 Pikulski et al. Mar 1987 A
4647331 Koury, Jr. et al. Mar 1987 A
4657429 Morris Apr 1987 A
4664732 Campbell et al. May 1987 A
4673244 Miles Jun 1987 A
4673245 Kling et al. Jun 1987 A
4677290 Mitch Jun 1987 A
4678271 Beaulieu Jul 1987 A
4679908 Goodwin Jul 1987 A
4701013 Jurczyszyn et al. Oct 1987 A
4702556 Ishii et al. Oct 1987 A
4708429 Clark et al. Nov 1987 A
4714315 Krause Dec 1987 A
4720163 Goodwin et al. Jan 1988 A
4746195 Auracher et al. May 1988 A
4747657 Chaoui et al. May 1988 A
4748632 Preston May 1988 A
4759600 Caron et al. Jul 1988 A
4763979 Heywang Aug 1988 A
4767174 Carenco et al. Aug 1988 A
4768759 Bellamy et al. Sep 1988 A
4773730 Sedlmayr Sep 1988 A
4779946 Pimpinella et al. Oct 1988 A
4779959 Saunders Oct 1988 A
4782223 Suzuki Nov 1988 A
4787691 Lorenzo et al. Nov 1988 A
4800262 Lentine Jan 1989 A
4807750 Ryder et al. Feb 1989 A
4823220 Milster et al. Apr 1989 A
4837768 Schmid Jun 1989 A
4842397 Eisler Jun 1989 A
4850261 Greene Jul 1989 A
4850671 Finzel Jul 1989 A
4854667 Ebata et al. Aug 1989 A
4913527 Jessop Apr 1990 A
4914867 Saito et al. Apr 1990 A
4915482 Collins et al. Apr 1990 A
4916635 Singer et al. Apr 1990 A
4938564 Romero Jul 1990 A
4966474 Geiger Oct 1990 A
4978910 Knox et al. Dec 1990 A
4988159 Turner et al. Jan 1991 A
4988165 Ishii et al. Jan 1991 A
5000415 Sandercock Mar 1991 A
5044719 Nakamura Sep 1991 A
5058124 Cameron et al. Oct 1991 A
5062012 Maeda et al. Oct 1991 A
5068749 Patel Nov 1991 A
5077747 Hemmer et al. Dec 1991 A
5132824 Patel et al. Jul 1992 A
5138496 Pong Aug 1992 A
5140470 Luecke Aug 1992 A
5146532 Hodge Sep 1992 A
5150236 Patel Sep 1992 A
5172160 Van Eijk et al. Dec 1992 A
5179618 Anton Jan 1993 A
5183350 Kramer Feb 1993 A
5189725 Bensel, III et al. Feb 1993 A
5191587 Hanson et al. Mar 1993 A
5194993 Bedzyk Mar 1993 A
5214735 Henneberger et al. May 1993 A
5218258 Shirasu et al. Jun 1993 A
5218610 Dixon Jun 1993 A
5219051 Davis Jun 1993 A
5251863 Gossman et al. Oct 1993 A
5285995 Gonzalez et al. Feb 1994 A
5289559 Wilson Feb 1994 A
5300755 Nishitani et al. Apr 1994 A
5311278 Rosencher May 1994 A
5319435 Melle et al. Jun 1994 A
5321539 Hirabayashi et al. Jun 1994 A
5327061 Gullapalli Jul 1994 A
5337383 DeAngelis et al. Aug 1994 A
5367140 Jonaneh et al. Nov 1994 A
5410145 Coroy Apr 1995 A
5428225 Silva et al. Jun 1995 A
5428635 Zhiglinsky et al. Jun 1995 A
5434944 Kerry et al. Jul 1995 A
5434945 Burek et al. Jul 1995 A
5446519 Makinouchi Aug 1995 A
5460357 Stewart Oct 1995 A
5463647 Pan Oct 1995 A
5469265 Measures et al. Nov 1995 A
5499261 Welch et al. Mar 1996 A
5502598 Kimura et al. Mar 1996 A
5528718 Ray et al. Jun 1996 A
5530547 Arnold Jun 1996 A
5530785 Sakamoto et al. Jun 1996 A
5544725 Handke et al. Aug 1996 A
5553186 Allen Sep 1996 A
5558189 Beck Sep 1996 A
5563972 Krausse et al. Oct 1996 A
5564537 Shoureshi Oct 1996 A
5570444 Janssen et al. Oct 1996 A
5581077 Chirovsky et al. Dec 1996 A
5598500 Crespel et al. Jan 1997 A
5603387 Beard et al. Feb 1997 A
5617501 Miller et al. Apr 1997 A
5619609 Pan et al. Apr 1997 A
5638267 Singhose et al. Jun 1997 A
5638482 Winterhoff et al. Jun 1997 A
5653317 Wakui Aug 1997 A
5655045 Morlion et al. Aug 1997 A
5660255 Schubert et al. Aug 1997 A
5668906 Yamamura et al. Sep 1997 A
5673350 Song et al. Sep 1997 A
5689607 Vincent et al. Nov 1997 A
5717804 Pan et al. Feb 1998 A
5725066 Beard et al. Mar 1998 A
5737132 Luecke et al. Apr 1998 A
5745633 Giebel et al. Apr 1998 A
5748821 Schempp et al. May 1998 A
5751877 Ishizaka et al. May 1998 A
5757561 Sechrist et al. May 1998 A
5758004 Alarcon et al. May 1998 A
5761360 Grois et al. Jun 1998 A
5765800 Watanabe et al. Jun 1998 A
5774614 Gilliland et al. Jun 1998 A
5793920 Wilkins et al. Aug 1998 A
5793921 Wilkins et al. Aug 1998 A
5794912 Whittaker et al. Aug 1998 A
5812958 Mayama Sep 1998 A
5823307 Schubert et al. Oct 1998 A
5825558 Farmiga et al. Oct 1998 A
5852519 Do et al. Dec 1998 A
5880894 Blakley Mar 1999 A
5909324 Bryant et al. Jun 1999 A
5930057 Sechrist et al. Jul 1999 A
5941920 Schubert Aug 1999 A
5946023 Blanding Aug 1999 A
5963695 Joyce Oct 1999 A
6016230 Nunnally et al. Jan 2000 A
6022005 Gran et al. Feb 2000 A
6198580 Dallakian Mar 2001 B1
6209841 Houghton, Jr. et al. Apr 2001 B1
Foreign Referenced Citations (7)
Number Date Country
2199423 Mar 1996 CA
2 124 402 Jul 1982 GB
2 131 971 Jun 1984 GB
03021894 Jan 1991 JP
08088167 Sep 1994 JP
09330875 Jun 1996 JP
10144601 Nov 1996 JP
Non-Patent Literature Citations (14)
Entry
J. M. Kahn, C. A. Burrus, and G. Raybon, High-Stability 1.5 um External-Cavity Semiconductor Lasers for Phase-Lock Applications, Photonics Technology Letters, vol. 1. No. 7, Jul. 1989.
P. Zorabedian and W. R. Trutna, Jr., “Interference-filter-tuned, alignment-stabilized, semiconductor external-cavity laser”, 1988, Optical Society of America.
A. Schremer and C. L. Tang, “Single-Frequency tunable external-cavity semiconductor laser using an electro-optic birefringent modulator”, Appl. Phys. Lett., vol. 55, No. 1, Jul. 3, 1989.
M. W. Maeda, J. S. Patel, D. A. Smith, Chinlon Lin, M. A. Saifi, and A. Von Lehman, “An Electronically Tunable Fiber Laser with a Liquid-Crystal Etalon Filter as the Wavelength-Tuning Element”, IEEE Photonics Technology Letters, vol. 2, No. 11, Nov. 1990.
Katsuhiko Hirabayashi, Hiroyuki Tsuda, and Takashi Kurokawa, “Tunable Liquid-Crystal Fabry-Perol Interferometer Filter for Wavelength-Division Multiplexing Communication Systems”, Journal of Lightwave Technology, vol. 11, No. 12, Dec. 1993.
Stephen R. Mallinson, “Wavelength-selective filters for single-mode fiber WDM systems using Fabry-Perot interferometers”, Applied Optics, vol. 26, No. 3, Feb. 1, 1987.
W. Gunning, J. Pasko, J. Tracy, “A liquid crystal tunable spectral filter: visible and infrared operation”, SPIE vol. 268 Imaging Spectroscopy (1981).
Hiroyuki Tsuda, Katsuhiko Hirabayashi, Yuichi Tohmori, and Takashi Kurokawa, “Tunable Light Source Using a Liquid-Crystal Fabry-Perot Interferometer”, IEEE Photonics Technology Letters, vol. 3. No. 6. Jun. 1991.
John R. Andrews, “Low Voltage Wavelength Tuning of an External Cavity Diode Laser Using a Nematic Liquid Crystal-Containing Birefringent Filert”, IEEE Photonics Technology Letters. vol. 2, No. 5, May 1990.
N. A. Olsson and J. P. Van Der Ziel, “Performance Characteristics of 1.5-um External Cavity Semiconductor Lasers for Coherent Optical Communication”, Journal Of Lightwave Technology, vol. LT-5. No. 4, Apr. 1987.
Hecht Optics Second Edition, Eugene Hecht, reprinted 1990, reference text pp. 303 # 368.
Rivin, Eugene I., “Vibration isolation of precision equipment”, Precision Engineering, 1995, pp. 41-56, vol. 17.
“Marsh Mellow Springs Vibration Isolation Design Manual”, 1998, Firestone Industrial Products Company.
Rivin, Eugene I., “Shaped Elastomeric Components for Vibration Control Devices”, Sound and Vibration, Jul. 1999, pp. 18-23, vol. 33, No. 7.