WO1997027408A1 - Tuned mass damper with tunable damping and antifriction rolling mass - Google Patents

Tuned mass damper with tunable damping and antifriction rolling mass Download PDF

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Publication number
WO1997027408A1
WO1997027408A1 PCT/US1996/018224 US9618224W WO9727408A1 WO 1997027408 A1 WO1997027408 A1 WO 1997027408A1 US 9618224 W US9618224 W US 9618224W WO 9727408 A1 WO9727408 A1 WO 9727408A1
Authority
WO
WIPO (PCT)
Prior art keywords
mass
ofthe
container
damper
interior
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
PCT/US1996/018224
Other languages
English (en)
French (fr)
Inventor
David A. Osterberg
Toren S. Davis
Conor D. Johnson
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Honeywell Inc
Original Assignee
Honeywell Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Honeywell Inc filed Critical Honeywell Inc
Priority to EP96939697A priority Critical patent/EP0871826B1/en
Priority to JP9526826A priority patent/JP2000504087A/ja
Priority to DE69611624T priority patent/DE69611624T2/de
Publication of WO1997027408A1 publication Critical patent/WO1997027408A1/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F7/00Vibration-dampers; Shock-absorbers
    • F16F7/10Vibration-dampers; Shock-absorbers using inertia effect
    • F16F7/104Vibration-dampers; Shock-absorbers using inertia effect the inertia member being resiliently mounted
    • F16F7/112Vibration-dampers; Shock-absorbers using inertia effect the inertia member being resiliently mounted on fluid springs
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F7/00Vibration-dampers; Shock-absorbers
    • F16F7/10Vibration-dampers; Shock-absorbers using inertia effect
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F7/00Vibration-dampers; Shock-absorbers
    • F16F7/10Vibration-dampers; Shock-absorbers using inertia effect
    • F16F7/104Vibration-dampers; Shock-absorbers using inertia effect the inertia member being resiliently mounted
    • F16F7/116Vibration-dampers; Shock-absorbers using inertia effect the inertia member being resiliently mounted on metal springs
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F2230/00Purpose; Design features
    • F16F2230/0052Physically guiding or influencing

Definitions

  • the present invention relates to tuned mass damping devices and more particularly to such dampers which may find use in reducing the periodic motion of elongated structures such as booms.
  • the invention may have particular utility with booms mounted on satellites to hold measuring equipment the accuracy of which may be reduced due to the sway of the boom resulting from disturbances such as thermal distortion shock caused by, for example, transient thermal distortions of solar panels.
  • the present invention overcomes the problems in the prior art by providing a damper with a mass which is constrained to move in the desired direction. By making the mass cylindrical and positioning it within a housing closely adjacent the mass, motion in the fluid container in only the desired direction is permitted.
  • the fluid may be varied to make the vibration tunable and, in fact, the present invention provides for tunable damping without having to change the fluid.
  • the tuning of the damping is accomplished by providing a pair of bellows with changeable internal springs therein to change the volumetric stiffness of the bellows and thus provide different characteristics to the fluid expansion and contraction in the chambers surrounding the mass.
  • FIG. 1 shows an example of the basic tuned damper of the present invention
  • FIG. 2 shows a second embodiment of the present invention inco ⁇ orating both the fine tuning of damping and reduction of friction with motion ofthe mass.
  • a damper 8 comprising a hollow moveable mass 10, slideably mounted in a cylindrical container 12 having a first end piece 14 fastened to cylinder 12 by conventional means, such as bolts, not shown and sealed to prevent fluid loss by a grommet 16.
  • a second end piece 18 is fastened at a second end in a recess 20 of cylinder 12 by conventional means such as bolts, also not shown.
  • the cylinder 12 and end pieces 14 and 18 form a chamber 22 within which mass 10 may move back and forth.
  • a spring 30 of predetermined stiffness is fastened at one end thereof to a protrusion 32 of end piece 14 and at the other end thereof to a recess 34 in mass 10 so that mass 10 will be positioned by spring 30 until subjected to a force allowing mass 10 to oscillate, only horizontally, back and forth in chamber 22 at a frequency determined by the size of mass 10 and stiffness of spring 30.
  • the first end piece 14 has a filling port 36 therethrough which allows the introduction of a damping fluid, shown by arrow 38, into the chamber 22. After filling, port 36 is sealed in conventional manner.
  • a thermal expansion bellows 40 is connected at one end thereof to a protrusion 42 in end piece 18 and at the other end thereof to a sealing member 44.
  • End piece 18 has a small opening 48 therethrough connecting the interior of bellows 40 to chamber 22. This allows transfer of fluid from chamber 22 to the interior of bellows 40 to accommodate expansion and contraction of the fluid under modest temperature variations.
  • the damper may be used to compensate for unwanted vibrations of, for example, a boom shown in Figure 1 by reference numeral 50. The unwanted oscillations will be transverse to the length of the boom and accordingly it is desired that the mass 10 move in the same direction, i.e. from right to left in Figure 1. Accordingly, the damper 8 is shown mounted to boom 59 horizontally as indicated by dashed lines 52 and 54 and, as explained above, will vibrate
  • the apparatus of Figure 1 will perform satisfactorily, but for some high accuracy or specialized uses, there may be inaccuracies or unnecessary costs associated with the Figure 1 damper.
  • the damping fluid 38 in chamber 20 is first chosen to have a viscosity which is believed to provide the best abso ⁇ tion of energy from the oscillating system and provide the desired amount of damping for the specific intended use.
  • the boom and the damper are then tested to check the damping characteristics and, if they are not right, the fluid has to be drained and new fluid with different viscosity inserted for a re-test. This process is repeated until the desired damping characteristics of the system are obtained.
  • Such a procedure is quite costly and time consuming and adds considerable cost to the damper.
  • a damper 108 (which may also be attached to a beam as in Figure 1 but not shown in Figure 2 for simplicity) is shown comprising a moveable mass 1 10, slideably mounted in a cylindrical container 112 having a first cylindrical end piece 114 fastened to the right end of cylinder 1 12 by conventional means, not shown.
  • a spring 116 has a first end fastened in a recess 118 of mass 112 and a second end fastened to end piece 114 so that mass 110 is positioned thereby.
  • Mass 1 10 is shown having an orifice 120 extending between its left and right sides in Figure 2 so as to permit the passage of the damping fluid therethrough.
  • the damping fluid may be inserted in the cylindrical container 112 in a manner similar to that shown in Figure 1.
  • the mass 1 10 and the spring 116 are chosen to have the frequency of oscillation matching the particular use to which it is to be put e.g. the frequency of the boom to which it will be mounted.
  • a plurality of troughs 122, 124, 126 and 128 are shown in the outer edge of mass 110 and are cross-sectionally shaped to constrain the movement of balls such as 132, 134, 136 and 138 in all but the desired direction, horizontally in Figure 2.
  • the grooves may be of slightly greater diameter than the balls as is shown in Figure 3a where a semicircular groove 122a supports the ball 132a, or, as shown in Figure 3b, may be a "V" shaped groove 122b supporting a ball 132b.
  • the ball is constrained for motion only into and out of the plane of the paper.
  • the plurality of balls 132, 134, 136 and 138 in the troughs 122, 124, 126 and 128 respectively engage the inner surface of cylinder 112 and provide rolling motion for mass 110.
  • the lengths of the troughs are made to accommodate the amount of motion expected of mass 110 oscillating back and forth in use. In the event that the mass 110 moves more than expected, the balls (although moving less distance than the mass) may nevertheless reach the ends of the trough where they may encounter greater friction due to the worming effect and/or tolerance errors.
  • the device is completely self centering so that when the motion decreases to the expected limits, the balls will move to the center and at rest assume the position shown in Figure 2.
  • This feature assures the device will remove the maximum amount of energy from the system by minimizing mass friction.
  • Using the balls eliminates the sliding friction between the mass 1 10 and the cylinder 112 and since a single ball is used, there is no friction between balls. Thus the possible excessive friction of the Figure 1 damper has been avoided.
  • Cylindrical end piece 1 14 has an abutment 140 and a first cylindrical end member 142 is seated thereon.
  • Cylindrical end member 142 has an inwardly extending ledge 144 and a removable end cap 146 with a hole 148 extending centrally therethrough.
  • End cap 146 is mounted against ledge 144.
  • a first bellows 150 has a right end which is fixed to the ledge 144 and extends to the left towards the interior of cylindrical container 112. The left end of bellows 150 is sealed to a circular plate 152 which has a central rod 154 extending back to the right so as to be guided in the hole 148.
  • a spring 156 is positioned in the interior of bellows 150 between the circular plate 152 and the end cap 146 and provides additional volumetric stiffness to the bellows 150.
  • the left end of damper 108 in Figure 2 is similar to the right end.
  • a second cylindrical end piece 164 is fastened to the left end of cylindrical container 112 by conventional means, not shown.
  • End piece 164 has an abutment 166 and a second cylindrical end member 168 is seated thereon.
  • Cylindrical end member 168 has an inwardly extending ledge 170 and a removable end cap 172 with a hole 174 extending therethrough. End cap 172 is mounted against ledge 170.
  • a second bellows 180 has a left end which is fixed to the ledge 170 and extends to the right towards the interior of cylindrical container 112.
  • the right end of bellows 180 is sealed to a circular plate 182 which has a central rod 184 extending back to the left so as to be guided in the hole 174.
  • a spring 186 is positioned in the interior of bellows 180 between the circular plate 182 and the end cap 172 and provides additional volumetric stiffness to the bellows 180.
  • the first and second bellows may be omitted and a single temperature compensating bellows such as shown in Figure 1 employed.
  • two dampers mounted on the member at right angles to each other may be employed.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Vibration Prevention Devices (AREA)
  • Vibration Dampers (AREA)
PCT/US1996/018224 1996-01-25 1996-11-13 Tuned mass damper with tunable damping and antifriction rolling mass Ceased WO1997027408A1 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
EP96939697A EP0871826B1 (en) 1996-01-25 1996-11-13 Tuned mass damper with tunable damping and antifriction rolling mass
JP9526826A JP2000504087A (ja) 1996-01-25 1996-11-13 調整可能減衰と減摩転動質量塊を有する質量緩衝装置
DE69611624T DE69611624T2 (de) 1996-01-25 1996-11-13 Adaptierter, dynamischer dämpfer mit abstimmbarer dämpfung und reibungsfrei rollendem gewicht

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/591,922 1996-01-25
US08/591,922 US5873438A (en) 1996-01-25 1996-01-25 Tuned mass damper with tunable damping and anti friction rolling mass

Publications (1)

Publication Number Publication Date
WO1997027408A1 true WO1997027408A1 (en) 1997-07-31

Family

ID=24368518

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US1996/018224 Ceased WO1997027408A1 (en) 1996-01-25 1996-11-13 Tuned mass damper with tunable damping and antifriction rolling mass

Country Status (5)

Country Link
US (2) US5873438A (enExample)
EP (2) EP0964179B1 (enExample)
JP (2) JP2000504087A (enExample)
DE (2) DE69611624T2 (enExample)
WO (1) WO1997027408A1 (enExample)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1998042998A3 (en) * 1997-03-21 1999-02-25 Honeywell Inc Pneumatic tuned mass damper
WO1999027275A1 (en) * 1997-11-22 1999-06-03 Honeywell Inc. Direct fluid shear damper
CN101492941B (zh) * 2008-12-26 2011-03-16 中铁大桥局集团武汉桥梁科学研究院有限公司 一种液体质量双调谐减振方法
EP2399831A1 (en) * 2010-06-28 2011-12-28 Honeywell International, Inc. Tunable mass damper for use with a reaction wheel assembly
WO2018196276A1 (zh) * 2017-04-26 2018-11-01 中铁大桥科学研究院有限公司 一种超低频液体质量调谐阻尼器
US11268587B2 (en) * 2018-10-18 2022-03-08 Siemens Aktiengesellschaft Active vibration damper, usable in a plurality of orientations

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Publication number Priority date Publication date Assignee Title
US6292967B1 (en) 1999-09-14 2001-09-25 Construction Technology Laboratories, Inc. TMD-damped stay cable and method and TMD
AU2003205138A1 (en) 2002-01-15 2003-07-30 Honeywell International Inc. Tuned mass damper using a hexapod
US6634472B1 (en) 2002-04-03 2003-10-21 Toren S. Davis Tuned mass damper with translational axis damping
JP4012024B2 (ja) * 2002-09-10 2007-11-21 キヤノン株式会社 位置決め装置に於ける衝撃吸収装置
TWI225452B (en) * 2003-05-26 2004-12-21 Yi-Hsung Pang Braking buffer and turning balance apparatus for motor car
US7073865B2 (en) * 2003-07-03 2006-07-11 Lear Corporation Tuned vibration absorbing system for a seat system
FI119655B (fi) * 2003-10-20 2009-01-30 Waertsilae Finland Oy Värähtelyn vaimennin ja moottorin värähtelyn vaimennusjärjestely
US20050121896A1 (en) * 2003-12-04 2005-06-09 Robert Bonhard Torsional dynamic tuned absorber for vehicle steering system
US7121729B2 (en) * 2004-03-15 2006-10-17 Honeywell International, Inc. Damped bearing cage
US20050217954A1 (en) * 2004-03-31 2005-10-06 Hindle Timothy A Viscous isolation and damping strut utilizing a fluid mass effect
JP4782592B2 (ja) * 2005-03-22 2011-09-28 東洋ゴム工業株式会社 防振装置
US20060243549A1 (en) * 2005-04-28 2006-11-02 Honeywell International, Inc. Magnetic bearings for damping and/or isolation systems
DE102007037048A1 (de) * 2007-08-06 2009-02-12 Robert Bosch Gmbh Zusatzhandgriffvorrichtung
US8261896B2 (en) * 2008-09-18 2012-09-11 Honeywell International Inc. Tuned mass dampers and vibration isolation apparatus
US8272786B2 (en) 2009-02-18 2012-09-25 Honeywell International Inc. Vibration isolation mounting assembly
US8256750B2 (en) * 2009-02-18 2012-09-04 Honeywell International Inc. Vibration isolation mounting assembly
JP2010264785A (ja) * 2009-05-12 2010-11-25 Kanto Auto Works Ltd 車両用ドア開閉装置
US8327985B2 (en) * 2009-06-22 2012-12-11 Honeywell International Inc. Two stage vibration isolator
US20110193277A1 (en) * 2010-01-08 2011-08-11 University Of Connecticut Smart Vibration Absorber For Traffic Signal Supports
US8702377B2 (en) 2010-06-23 2014-04-22 Honeywell International Inc. Gas turbine engine rotor tip clearance and shaft dynamics system and method
DE102011007725A1 (de) * 2011-04-20 2012-10-25 Hilti Aktiengesellschaft Handwerkzeugmaschine und Tilger
CN103835384A (zh) * 2013-12-30 2014-06-04 同济大学 质量调谐减振装置
US9587702B2 (en) 2014-02-18 2017-03-07 Honeywell International Inc. Vibration isolator using externally pressurized sealing bellows and an external shaft
CN104389943B (zh) * 2014-09-12 2017-06-06 上海卫星工程研究所 一种卫星用液体阻尼隔振器
CN104455182A (zh) * 2014-11-21 2015-03-25 上海卫星工程研究所 卫星用液体阻尼隔振器
WO2017172720A1 (en) 2016-03-28 2017-10-05 Robert Berry Disruptive tuned mass system and method
DE102016107765A1 (de) 2016-04-27 2017-11-02 Karlsruher Institut für Technologie Schwingungsdämpfer
US9992890B1 (en) * 2016-12-07 2018-06-05 Raytheon Company Modules and systems for damping excitations within fluid-filled structures
US10041558B1 (en) 2017-10-06 2018-08-07 Topline Corporation Tunable apparatus for adjusting effective performance of particle impact damper
US10021779B1 (en) 2017-11-28 2018-07-10 TopLine Coporation Quick response particle damper for printed circuit boards and planar surfaces
JP7019476B2 (ja) * 2018-03-26 2022-02-15 日立Astemo株式会社 ダンパ装置
US10704639B2 (en) 2018-08-14 2020-07-07 Topline Corporation Unidirectional particle damper for printed circuit boards and planar surfaces
CN110410611A (zh) * 2019-07-26 2019-11-05 武汉地震工程研究院有限公司 一种建筑管道结构摩擦调谐减震装置
US11401993B1 (en) * 2020-09-17 2022-08-02 The United States Of America As Represented By The Secretary Of The Navy Shock mitigation utilizing quiescent cavitation
CN113639004B (zh) * 2021-08-24 2022-05-27 上海大学 一种挤压模式巨电流变液阻尼器

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US3911199A (en) * 1974-04-26 1975-10-07 Westinghouse Electric Corp Seismic motion-damper for upstanding electrical equipment
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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1998042998A3 (en) * 1997-03-21 1999-02-25 Honeywell Inc Pneumatic tuned mass damper
WO1999027275A1 (en) * 1997-11-22 1999-06-03 Honeywell Inc. Direct fluid shear damper
CN101492941B (zh) * 2008-12-26 2011-03-16 中铁大桥局集团武汉桥梁科学研究院有限公司 一种液体质量双调谐减振方法
EP2399831A1 (en) * 2010-06-28 2011-12-28 Honeywell International, Inc. Tunable mass damper for use with a reaction wheel assembly
US8726762B2 (en) 2010-06-28 2014-05-20 Honeywell International Inc. Tunable mass damper for use with a reaction wheel assembly
WO2018196276A1 (zh) * 2017-04-26 2018-11-01 中铁大桥科学研究院有限公司 一种超低频液体质量调谐阻尼器
US11268587B2 (en) * 2018-10-18 2022-03-08 Siemens Aktiengesellschaft Active vibration damper, usable in a plurality of orientations

Also Published As

Publication number Publication date
DE69611624D1 (de) 2001-02-22
DE69627546T2 (de) 2004-01-15
US5873438A (en) 1999-02-23
EP0871826B1 (en) 2001-01-17
JP2000504087A (ja) 2000-04-04
DE69627546D1 (de) 2003-05-22
DE69611624T2 (de) 2001-05-03
EP0871826A1 (en) 1998-10-21
JP4524319B2 (ja) 2010-08-18
EP0964179A1 (en) 1999-12-15
JP2008232446A (ja) 2008-10-02
EP0964179B1 (en) 2003-04-16
US6454063B1 (en) 2002-09-24

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