WO2017152101A1 - Transducteur de charge à deux axes à ensemble de sollicitation - Google Patents

Transducteur de charge à deux axes à ensemble de sollicitation Download PDF

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Publication number
WO2017152101A1
WO2017152101A1 PCT/US2017/020743 US2017020743W WO2017152101A1 WO 2017152101 A1 WO2017152101 A1 WO 2017152101A1 US 2017020743 W US2017020743 W US 2017020743W WO 2017152101 A1 WO2017152101 A1 WO 2017152101A1
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WO
WIPO (PCT)
Prior art keywords
transducer
clevis
sensor body
biasing
support
Prior art date
Application number
PCT/US2017/020743
Other languages
English (en)
Inventor
Richard A. Meyer
Robert L. JOSEPHSON
Jason A. Christopherson
Todd Robert OSMUNDSON
Nicholas Devon LAMOORE
Riley August ROGOTZKE
Original Assignee
Mts Systems Corporation
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 Mts Systems Corporation filed Critical Mts Systems Corporation
Publication of WO2017152101A1 publication Critical patent/WO2017152101A1/fr

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Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M9/00—Aerodynamic testing; Arrangements in or on wind tunnels
    • G01M9/06—Measuring arrangements specially adapted for aerodynamic testing
    • G01M9/062—Wind tunnel balances; Holding devices combined with measuring arrangements
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L1/00—Measuring force or stress, in general
    • G01L1/26—Auxiliary measures taken, or devices used, in connection with the measurement of force, e.g. for preventing influence of transverse components of force, for preventing overload

Definitions

  • the present disclosure relates to devices that transmit and measure linear forces along and moments about three orthogonal axes. More particularly, the present disclosure relates to devices that are particularly well suited to measure forces and moments upon a test specimen in a test environment, such as but not limited to in a wind tunnel.
  • Test specimens can be placed on a platform balance located in a pit of the wind tunnel.
  • the platform balance can be arranged to receive a model of a vehicle, a vehicle, or other actual or modeled test specimen.
  • the platform balance can be equipped with a rolling belt to rotate the wheels, which can make a significant improvement in measurement accuracy.
  • Platform balances have a tendency to be susceptible to various physical properties of the test environment that can lead to inaccurate measurements without additional compensation. For example, temperature transients in the wind tunnel can result in thermal expansion of the platform balance that can adversely affect the transducers. In addition, large test specimens are prone to create large thrust loads on the transducers that can cause inaccurate measurements.
  • One general aspect is a transducer body, including: a support including a pair of clevis halves; and a sensor body coupled to each of the clevis halves, where the sensor body is disposed between the clevis halves and includes a generally rigid peripheral member disposed about a spaced-apart central hub, the central hub being joined to each of the clevis halves with the peripheral member spaced apart from each clevis half, where at least three flexure components couple the peripheral member to the central hub, and where the flexure components are spaced-apart from each other at generally equal angle intervals about the central hub; and a biasing assembly connected between the support and the sensor body and configured to provide a bias force between the sensor body and the support; where the biasing assembly includes a pair of cantilevered beams, a first cantilevered beam extending from a first side of the transducer body on the first clevis half, and a second cantilevered beam extending from a second, opposite, side of the transducer body
  • Implementations may include one or more of the following features.
  • the transducer body where the biasing assembly further includes a biasing connector configured to operate in tension to provide the bias force.
  • the transducer body where the biasing connector includes a strap coupled between the support and the sensor body.
  • the transducer body where the biasing connector includes a spring coupled between the support and the sensor body.
  • One general aspect is a transducer body, including: a support including a pair of clevis halves; and a sensor body coupled to each of the clevis halves, where the sensor body is disposed between the clevis halves and includes a generally rigid peripheral member disposed about a spaced-apart central hub, the central hub being joined to each of the clevis halves with the peripheral member spaced apart from each clevis half, where at least three flexure components couple the peripheral member to the central hub, and where the flexure components are spaced-apart from each other at generally equal angle intervals about the central hub; and a biasing assembly connected between the support and the sensor body and configured to provide a bias force between the sensor body and the support; where the biasing assembly includes a first cantilevered beam on the first clevis half, and a second cantilevered beam on the second clevis half.
  • Implementations may include one or more of the following features.
  • the transducer body where the first cantilevered beam extends from a first side of the transducer assembly toward a second side of the transducer assembly, and where the second cantilevered beam extends from the second side of the transducer assembly toward the first side of the transducer assembly.
  • the transducer body where the first and the second cantilevered beams each include a plurality of slots therein, extending along a longitudinal length of a cantilevered portion of their respective cantilevered beams.
  • the transducer body where the biasing assembly further includes a first biasing connector for the first cantilevered beam, and a second biasing connector for the second cantilevered beam, the first and second biasing connectors configured to operate in tension to provide the bias force.
  • the transducer body where the first and second biasing connectors each includes a strap.
  • the transducer body where the first and second biasing connectors each includes a spring.
  • One general aspect is a transducer body, including: a support including a pair of clevis halves; and a sensor body coupled to each of the clevis halves, where the sensor body is disposed between the clevis halves and includes a generally rigid peripheral member disposed about a spaced-apart central hub, the central hub being joined to each of the clevis halves with the peripheral member spaced apart from each clevis half, where at least three flexure components couple the peripheral member to the central hub, and where the flexure components are spaced-apart from each other at generally equal angle intervals about the central hub; and a biasing assembly connected between the support and the sensor body and configured to provide a bias force between the sensor body and the support; where the biasing assembly includes a pair of spring assemblies disposed on opposite sides of the transducer assembly.
  • Implementations may include one or more of the following features.
  • each of the pair of spring assemblies includes a spring having a first end coupled to a perimeter body of the sensor body.
  • each of the pair of spring assemblies further includes a mount coupled to the perimeter body with fasteners.
  • the transducer body where the transducer body further includes a first connecting member joining the first and the second clevis halves together at a first end of the transducer body, and a second connecting member joining the first and second clevis halves together on a second end opposite the first end.
  • the transducer body where the second connecting member further includes opposed ears configured to secure a second end of each spring to a corresponding ear of the second connecting member and thus to the first and second clevis halves.
  • One general aspect is a transducer body, including: a support including a pair of clevis halves; and a sensor body coupled to each of the clevis halves, where the sensor body is disposed between the clevis halves and includes a generally rigid peripheral member disposed about a spaced-apart central hub, the central hub being joined to each of the clevis halves with the peripheral member spaced apart from each clevis half, where at least three flexure components couple the peripheral member to the central hub, and where the flexure components are spaced-apart from each other at generally equal angle intervals about the central hub; and a biasing assembly connected between the support and the sensor body and configured to provide a bias force between the sensor body and the support, the biasing assembly including: a flexible member fixedly connected to one of the sensor body or the support, the flexible member comprising a beam cantilevered from one of the sensor body or the support, the cantilevered beam including a plurality of slots therein; and a biasing connector to couple the flexible
  • the transducer body also includes a flexible member fixedly connected to one of the sensor body or the support, the flexible member including a beam cantilevered from one of the sensor body or the support, the cantilevered beam including a plurality of slots therein.
  • the transducer body also includes a biasing connector to couple the flexible member to the other of the support or the sensor body.
  • Implementations may include one or more of the following features.
  • the transducer body where the flexible member is integrally formed from a single unitary body of one of the sensor body or the support.
  • the transducer body where a flexible member is provided on each clevis half and a bridging block connects the flexible members together, the bridging block being spaced apart from the sensor body.
  • transducer body where the flexible member of the first clevis half extends from a first side of the transducer body, and where the flexible member of the second clevis half extends from a second opposite side of the transducer body.
  • the transducer body where the flexible member of the first clevis half and the flexible member of the second clevis half extend in substantially parallel directions toward each other from their respective sides of the transducer body.
  • the transducer body where a flexible member is provided on each clevis half and a bridging block connects the flexible portions together, the bridging block being spaced apart from the sensor body.
  • the transducer body where the flexible member includes a pair of cantilevered beams extending from a center support toward opposite sides of the transducer body.
  • the transducer body where the flexible member includes a pair of flexible members, a first flexible member on the first clevis half, and a second flexible member on the second clevis half, where the first flexible member extends substantially fully across a width of the first clevis half from a first edge of the transducer body to a second edge of the transducer body, and where the second flexible member extends substantially fully across a width of the second clevis half from the second edge of the transducer body to the first edge of the transducer body.
  • the transducer body where the flexible member includes a pair of flexible members extending in opposite directions.
  • each of the pair of flexible members includes a plurality of slots therein, the slots extending within the cantilevered portion of the flexible member but contained within a body of the cantilevered portion.
  • the transducer body where the biasing connector to couple the flexible member to the other of the support or the sensor body is a strap.
  • the transducer body where the biasing connector to couple the flexible member to the other of the support or the sensor body is a spring.
  • One general aspect includes a transducer body, including: a support including a pair of clevis halves; and a sensor body coupled to each of the clevis halves, where the sensor body is disposed between the clevis halves and includes a generally rigid peripheral member disposed about a spaced-apart central hub, the central hub being joined to each of the clevis halves with the peripheral member spaced apart from each clevis half, where at least three flexure components couple the peripheral member to the central hub, and where the flexure components are spaced-apart from each other at generally equal angle intervals about the central hub; and a biasing assembly connected between the support and the sensor body and configured to provide a bias force between the sensor body and the support, the biasing assembly including a pair of biasing connectors, where a biasing connector is provided for each of opposite portions of the transducer body that are symmetrical, each biasing connector including a cantilevered beam with one of the biasing connectors connected to one of the flexible members, the cantileve
  • a platform balance may be provided in another aspect with transducer bodies and aspects provided above, as shown or described. [0048] One or more of the foregoing features described above can be included in other embodiments as desired.
  • FIG. 1 is a side elevation view of a transducer body according to an embodiment of the present disclosure
  • FIG. 2 is a perspective view of a sensor body according to an embodiment of the present disclosure
  • FIG. 3 is a front elevation view of the sensor body of FIG. 2;
  • FIG. 4 is a view of the sensor body taken along lines 4— 4 of FIG. 3;
  • FIG. 5 is a close-up view of a portion of the sensor body of FIG.3;
  • FIG. 6 is a close-up view of a portion of the cut away view of FIG. 4;
  • FIG. 7 is a circuit diagram of a Wheatstone bridge for the sensor elements of FIG. 2;
  • FIG. 8 is a close up view of a portion of the sensor body of FIG. 2;
  • FIG. 9 is a front elevation view of a sensor body according to another embodiment of the present disclosure.
  • FIG. 10 is a perspective view of the sensor body of FIG. 9;
  • FIG. 11 is a close up view of a portion of the sensor body of FIG. 10;
  • FIG. 12 is a front elevation view showing locations of sensor elements on the sensor body of FIG.9;
  • FIG. 13 is a circuit diagram of a Wheatstone bridge for the sensor elements of FIG. 9;
  • FIG. 14 is a front elevation view of a sensor body according to another embodiment of the present disclosure.
  • FIG. 15 is a close up view of a flexure element of the sensor body of the FIG. 14;
  • FIG. 16 is a front elevation view of yet another sensor body according to another embodiment of the present disclosure.
  • FIG. 17 is a bottom view of the sensor body of FIG. 16;
  • FIG. 18 is a perspective view of the sensor body of FIG. 16;
  • FIG. 19 is a cut away view along lines 19—19 of FIG. 16;
  • FIG. 20 is a close up view of a flexure element of FIG. 16;
  • FIG. 21 is a close up view of an alternate flexure element according to another embodiment of the present disclosure;
  • FIG. 22 is a top view of a platform balance according to an embodiment of the present disclosure.
  • FIG. 23 is a side elevation view of the platform balance of FIG. 22;
  • FIG. 24 is a perspective view of a transducer body according to another embodiment of the present disclosure.
  • FIG. 25 is a front elevation view of the transducer body of FIG. 24;
  • FIG. 26 is a perspective view of a transducer body according to another embodiment of the present disclosure.
  • FIG. 27 is a front elevation view of the assembly of FIG. 26;
  • FIG. 28 is a right side elevation of the assembly of FIG. 26;
  • FIG. 29 is a cut away view showing a front elevation of a sensor body in place on the assembly of FIG. 26;
  • FIG. 30 is a close up view of a portion of FIG. 29;
  • FIG. 31 is a perspective view of a clamp assembly in place on a transducer body according to another embodiment of the present disclosure.
  • FIG. 32 is a close up and partial cut away view of a portion of the assembly of FIG. 31;
  • FIG. 33 is a perspective view of a transducer body in a fluid recirculating bath assembly according to another embodiment of the present disclosure.
  • FIG. 34 is a front elevation view of the assembly of FIG. 33;
  • FIG. 35 is a perspective view of a transducer assembly according to another embodiment of the present disclosure.
  • FIG. 36 is a front elevational view of the transducer assembly of FIG. 35;
  • FIG. 37 is a right-side elevational view of the FIG. 35;
  • FIG. 38 is a perspective view of the transducer assembly of FIGS. 35 with parts removed;
  • FIG. 39 is a sectional view of a portion of the transducer assembly of FIG. 35.
  • FIG. 40 is a perspective view of a transducer assembly according to another embodiment of the present disclosure.
  • FIG. 41 is a perspective view of a transducer assembly according to yet another embodiment of the present disclosure.
  • FIG. 42 is a perspective view of a transducer assembly according to still another embodiment of the present disclosure.
  • FIG. 43 is a perspective view of a transducer assembly according to still another embodiment of the present disclosure.
  • the transducer assembly 10 includes a sensor body 12 and a clevis assembly 14.
  • the clevis assembly 14 includes a first clevis half 16 and a second clevis half 18.
  • the clevis halves 16 and 18 are joined together at one end with a connecting member 17.
  • the sensor body 12 is disposed between the clevis halves 16 and 18, where the sensor body 12 and clevis halves 16 and 18 are joined together with a suitable fastener assembly.
  • the sensor body 12 includes a plurality of apertures 15 (Fig.
  • a bolt or threaded rod can extend through aligned bores 19, 21, and 23 (Fig. 1) in each of the clevis halves 16 and 18 and sensor body 12.
  • a nut (not shown) can be provided on one end of the rod and a super nut can be threaded upon an opposite end.
  • a plurality of set screws extends though apertures in the super nut to engage in end of one of the clevis halves 16 or 18. This fastening technique is described in US Patent 7,788,984, which is incorporated herein by reference in its entirety.
  • the sensor body 12 is preferably integral, being formed of a signal unitary block of material.
  • the sensor body 12 includes a rigid central hub 20 upon which the surfaces 15A and 15B reside, and a rigid perimeter body 22 that is concentric with or disposed about central hub 20.
  • a plurality of flexure structures 24 join the central hub 20 to the perimeter body 22.
  • the plurality of flexure structures 24 comprise four components 31, 32, 33 and 34. Each of the components 31-34 extend radially from the central hub 20 along corresponding longitudinal axis 31 A, 32A, 33A and 34A.
  • axis 31A is aligned with axis 33A, while axis 32A is aligned with axis 34A.
  • axes 31A and 33A are perpendicular to axes 32A and 34A.
  • the plurality of flexure components 31-34 are spaced at equal angular intervals about a central axis indicated at 35.
  • an intermediate member 41 is integral with, being formed from the unitary block of material, or otherwise connected to flexure component 31 at an end opposite central hub 20.
  • Intermediate member 41 is preferably symmetric with respect to flexure component 31 or longitudinal axis 31A having side portions 41 A and 4 IB on opposite sides of flexure component 31 or longitudinal axis 31 A.
  • Each side portion 41A, 41B is connected to perimeter body 22 through a flexure assembly 51A, 51B, respectively.
  • flexure assembly 51A by way of example, each of the flexure assemblies 51A and 51B, in the embodiment illustrated, include a rigid connecting member 55.
  • the connecting member 53 is connected or joined to one of the side portions 41 A, 4 IB through a thin flexible web 55.
  • the connecting member 55 is connected to perimeter body 22 through a thin web 57.
  • the webs 55 and 57 are relatively wide being, for example, similar to the width or thickness of the perimeter body 22; however, each of the webs 55 and 57 are thin in a direction normal to the width of the perimeter body 22.
  • the orientation of each of the webs 55 and 57 connecting the intermediate member 41 to the perimeter body 22 are oriented perpendicular to the flexure component associated with each intermediate number 41.
  • each of the connecting webs 55 and 57 are relatively wide in a direction parallel to the central axis 35, but thin in a cross-section perpendicular to axis 35.
  • each of the flexure components 31-34 are thin in a direction parallel to the central axis 35 and relatively wide in a cross-section perpendicular to the axis 35.
  • the connecting webs 55 and 57 are compliant for forces along the longitudinal axis of the flexure component to which it is connected, but stiff for an axis orthogonal to the axis of the flexure component to which it is associated with, and the axis orthogonal to the foregoing axes (or the axis parallel to the central axis 35).
  • the flexure components 31-34 operate in pairs for forces along an axis that is orthogonal to the longitudinal axes of each pair of flexure components (31,33 and 32,34) and orthogonal to the central axis 35.
  • flexure components 31 and 33 transfer forces between the central body 20 and the perimeter body 22 for forces along an axis 61 (wherein connecting webs 55 and 57 associated flexure components 32 and 34 are compliant in this direction), while flexure components 32 and 34 transfer forces between the central body 20 and the perimeter body 22 for forces along an axis 63 (wherein connecting webs 55 and 57 associated flexure components 31 and 33 are compliant in this direction).
  • the flexure assemblies 51A and 5 IB (herein by example connecting member 53 and connecting webs 55, 57) associated with each flexure component 31- 34 (on opposite sides of the flexure component) are disposed so as to coincide at least approximately with a midpoint along the length of the corresponding flexure component. Referring to the enlarged view of FIG.5 a midpoint of the longitudinal length of the flexure component 31 is indicated at 66.
  • the flexure assemblies 51 A, 5 IB on opposite sides of the flexure component 31 are orthogonal to the associated flexure component in a planar sense, but are configured or disposed so as to be approximately inline with the midpoint 66 as represented by dashed line 68, or substantially proximate to the midpoint 66.
  • the web(s) of the flexure assemblies 51 A, 5 IB on each side of the flexure component they are associated with can be defined by corresponding planes, the planes of which are orthogonal to a plane representing the flexure component.
  • the flexure components 31-34 and associated flexure assemblies 51 A, 5 IB are connected in the manner described above about center axis 35, the sensor body 12 includes flexure elements (flexure components 31-34) that can be used to sense forces with respect to two orthogonal axes 61, 63 that can carry high loads with high resolution.
  • each flexure assembly is configured such that forces transferred between central hub 20 and the peripheral member 22 cause a first force at the connection of the flexure component to the central hub 20 to be equal and opposite to a second force at the connection of the flexure component to the peripheral member 22, wherein the first and second force are tangential to the radial direction of each corresponding flexure component.
  • one aspect of the invention is use of the flexure assemblies being configured such that on each side of the flexure component they are connected to provide compliance in a direction of the longitudinal length of the flexure component from the hub to the outer perimeter.
  • the flexible elements of the flexure assemblies are defined by aligned corresponding planes, the planes of which are orthogonal to the direction of compliance and coincide at least approximately with a midpoint along the length of the corresponding flexure component.
  • each of the flexure components 31-34 includes sensor elements to measure shear deflection or strain therein.
  • the sensing elements can take any number of forms known to those skilled in the art, including electrically and optically based sensor elements to name just a few.
  • strain gauges are connected in a Wheatstone bridge with strain gauge elements placed on both sides of the flexure component on the principle stress axis. Referring to the enlarged view of FIG. 5 and the circuit diagram of FIG. 7, the Wheatstone bridge 70 includes sensor elements 71 and 72, on one side of the flexure component, while on a side opposite of the flexure component that is shown in FIG.
  • each of the flexure components 31- 34 are relatively thin in a direction parallel to central axis 35.
  • the component is not thin in this direction in order to necessarily provide compliance but rather, the thickness of the flexure components are minimized in order to obtain a high output signal (maximize deflection) and a higher signal to noise ratio.
  • FIG. 1 In yet an alternative embodiment illustrated in FIG.
  • the flexure component 31 includes a sensing portion 80 upon where the sensor elements 71 and 72 are disposed (sensor elements 73 and 74 being on the opposite side of sensing portion 80) and portions 82A and 82B that are on opposite sides of sensor portion 80 and are of greater thickness in order to provide greater stiffness in the direction parallel to the central axis 35, while still maintaining required sensitivity in the axis of measurement.
  • FIGS. 9-13 Another sensor body is indicated at 102 at FIGS. 9-13, which can be used in place of the sensor body 12, described above, in one exemplary embodiment.
  • the sensor body 102 has elements similar in function to that described above with respect to sensor body 12 and has such similar components are identified with the same reference numbers.
  • the sensor body 102 includes flexure components 31 and 33, intermediate members 41, connecting members 53 and connecting webs 55-57.
  • the flexure components 31 and 33 measure forces between the central body 20 and the perimeter body 22 for forces in a direction parallel to axis 61.
  • Sensor body 102 however includes flexure structures 102 and 104 to transfer forces between the central body 20 and the perimeter body 22 along axis 63.
  • the flexure structures 103 and 104 are designed to be substantially stiffer then the flexure components 31 and 33 so as to transfer substantially larger forces between the central body 20 and the perimeter body 22.
  • each of the flexure structures 103 and 104 include two flexure components 112A and 112B extending from the central body 20 to an intermediate member 111.
  • the flexure components 112A, 112B each have a longitudinal axis indicated at 113 A and 113B wherein an acute angle 116 is formed between the axes 113A, 113B.
  • the flexure components 112A, 112B are oriented so as to converge in a direction toward the intermediate member 111; however, in an alternative embodiment, if desired, an acute angle can be formed between the flexure components with convergence toward the central body 20 rather than the intermediate member 111.
  • the intermediate member 111 is connected to the perimeter body 22 with flexure assemblies 115A and 115B (herein by example each comprising a connecting web 117) on opposite sides of the intermediate member 111.
  • the flexure assemblies 115A and 115B are substantially stiff for forces along axis 63, but significantly more compliant for forces along axis 61 such that these forces are transferred between the central body 20 and the perimeter body 22 through the flexure components 31 and 33.
  • each of the pairs of the flexure components 112A, 112B for flexure structures 103 and 104 includes sensor elements to measure component deflection or strain therein.
  • the sensor elements can take any number of forms known to those skilled in the art, including electrically and optically based sensor elements to name just a few.
  • strain gauges are connected in a Wheatstone bridge with strain gauge elements placed on opposite sides of each flexure components 112A, 112B.
  • a Wheatstone bridge 130 includes sensor elements 131 and 132 on opposite sides of flexure component 112A, while sensor elements 133 and 134 are on opposite sides of flexure component 112B.
  • FIG. 12 illustrates location of the sensor elements 131 and 133 on the sides of each of the flexure components 112A and 112B (i.e. parallel to the sides of the sensor body 102, rather than between the sides of the sensor body 102).
  • FIGS. 14-15 Another sensor body is indicated at 202 at FIGS. 14-15, which can be used in place of the sensor body 12, described above, in one exemplary embodiment.
  • the sensor body 202 has elements similar in function to that described above with respect to sensor body 12 and sensor body 102 and as such similar elements are identified with the same reference numbers.
  • the sensor body 202 includes flexure components 31 and 33, intermediate members 41, connecting members 53 and connecting webs 55-57.
  • the flexure components 31 and 33 measure forces between the central body 20 and the perimeter body 22 for forces in a direction parallel to axis 61.
  • Sensor body 202 however includes flexure structures 203 and 204 to transfer forces between the central body 20 and the perimeter body 22 along axis 63.
  • the flexure structures 203 and 204 are designed to be substantially stiffer then the flexure components 31 and 33 so as to transfer substantially larger forces between the central body 20 and the perimeter body 22.
  • Each of the flexure structures 203 and 204 include a flexure component 212 that is rectangular (preferably square) in cross-section along the length thereof, but at least two sides, preferably opposite to each other, are tapered along the length of the flexure component 212 such that one end portion of the flexure component 212 is smaller in cross-section than the other end portion, herein end portion 212A connected to intermediate member 111 is smaller in cross- section (before connection to intermediate member 111). In the illustrated embodiment all sides are tapered along the length of the flexure component 212, i.e.
  • strain field in the center of the flexure component 212 can be approximately 80 % (although this value is adjustable based on the shape of the flexure component 212) of the strain in the connecting fillets at the ends of the flexure component 212.
  • Each of the sides of the flexure component 212 can include a sensor element such as those described above connected in a conventional Wheatstone bridge (not shown). Strain gauges 231 and 232 are illustrated by way of example.
  • FIG. 16-21 Yet another sensor body is indicated at 242 at Figs. 16-21, which can be used in place of the sensor body 12, described above, in one exemplary embodiment.
  • the sensor body 242 has elements similar in broad function to that described above with respect to sensor body 12 and as such similar elements are identified with the same reference numbers.
  • the sensor body 242 includes flexure components 251 and 253, intermediate members 41, connecting members 53 and connecting webs 55-57.
  • the flexure components 251 and 253 measure forces between the central body 20 and the perimeter body 22 for forces in a direction parallel to axis 61.
  • flexure components 252 and 254, intermediate members 41, connecting members 53 and connecting webs 55-57 measure forces between the central body 20 and the perimeter body 22 for forces in a direction parallel to axis 63 and are also substantially the same as the flexure structures for measuring forces in a direction parallel to axis 61.
  • this is not a requirement as demonstrated by the previous embodiments.
  • any of the other flexure structures can be used, typically in pairs, but otherwise without limitation, of any of the previous embodiments for either measuring forces in a direction parallel to axis 61 or to axis 63.
  • the flexure components 251-254 are very similar to flexure components 31-34; however, flexure components 251-254 include corresponding apertures 251 A, 252A, 253A and 254A.
  • the strain gauges on the flexure components 251-254 are configured to measure strain in bending (as parallel double cantilever bending beams 255A and 255B illustrated in Fig. 20) rather than to measure strain in shear as flexure components 31- 34 operate.
  • Each of the flexure components 251-254 includes sensor elements to measure bending deflection or strain therein.
  • the sensing elements can take any number of forms known to those skilled in the art, including electrically and optically based sensor elements to name just a few.
  • resistive strain gauges connected in a suitable Wheatstone bridge can be secured to each of the beams 255A and 255B of each flexure component 251-254.
  • the strain gauges are secured to the inwardly facing surface 254B of each beam 255A, 255B formed by each aperture 251A-254A, although the strain gauges could also be secured to the outwardly facing surfaces 254C, which face in opposite directions.
  • the sensing gauges for sensing deflection of each of the beams 255A and 255B are located approximately at the midpoint of each beam 255A, 255B of each flexure component 251-254 and where the flexible elements (connecting members 53 and connecting webs 55-57) of the flexure assemblies are defined by aligned corresponding planes, the planes of which are orthogonal to the direction of compliance and coincide at least approximately with a midpoint along the length of each beam 255A, 255B of the corresponding flexure component 251-254, or stated another way bisect each of the apertures 251A-254A.
  • the structure of the flexure components 251-254 provides high stiffness with very good resolution and low crosstalk.
  • apertures 251-254 are illustrated as round holes, it should be understood that the apertures could be of any suitable shape, such as but not limited to square apertures with rounded corners, or the like, without departing from the scope of the disclosure.
  • FIGS. 22-23 An exemplary embodiment of any of the foregoing transducer bodies with suitable sensing elements to form a transducer assembly can be incorporated in a platform balance 300 an example of which is illustrated in FIGS. 22-23.
  • the platform balance 300 can include a first frame support 302 and a second frame support 304.
  • the platform balance 300 can be used to measure forces and moments applied to a test specimen of nominally large weight or mass such as a vehicle, plane, etc. or models thereof.
  • the frame supports 302 and 304 are nominally unstressed reaction frames, wherein each of the transducers comprises a two-axis force transducer as described above.
  • Various levels of flexure isolation can be provided in the platform balance 300 to provide increased sensitivity, while nominally supporting large masses.
  • the platform balance 300 is particularly well suited for measuring force and/or moments upon a large specimen such as a vehicle in an environment such as a wind tunnel.
  • the platform balance 300 can include flexures 315 isolating the frame support 302 and 304 from the test specimen and a ground support mechanism.
  • four flexures 315 are provided between each of the transducer assemblies, being coupled to the plates 320.
  • four flexures 324 are coupled to the mounting plates 322.
  • the flexures 315, 324 thereby isolate the frame supports 302 and 304.
  • the flexures 315, 324 are generally aligned with the sensor bodies of each corresponding transducer assembly.
  • the platform balance 300 is particularly well suited for use in measuring forces upon a vehicle or other large test specimen in a wind tunnel.
  • rolling roadway belts 332 are supported by an intermediate frame 334 coupled to the flexure members 315.
  • the rolling roadway belts 332 support the vehicle tires.
  • a single roadway belt is used for all tires of the vehicle.
  • the platform balance 300 and rolling roadway belt assemblies 332 are positioned in a pit and mounted to a turntable mechanism 336 so as to allow the test specimen, for example a vehicle, to be selectively turned with respect to the wind of the wind tunnel.
  • Each of the frame supports 302 and 304 comprise continuous hollow box components formed in a perimeter so as to provide corresponding stiff assemblies.
  • the frame support 302 holds the sensor bodies in position with respect to each other, while the frame support 304 holds the clevis assemblies in position with respect to each other.
  • Stiffening box frame members 333 can also be provided in the support frame as illustrated.
  • outputs from each of the two-axis sensing circuits from each of the transducer assemblies can be combined so as to sense or provide outputs indicative of forces and moments upon the platform balance in six degrees of freedom.
  • a coordinate system for platform 300 is illustrated at 331.
  • Output signals from transducer assemblies 340A and 340C are used to measure forces along the X-axis, because transducer assemblies 340B and 340D are compliant in this direction.
  • output signals from transducer assemblies 340B and 340D are used to measure forces along the Y-axis, because transducer assemblies 340A and 340C are compliant in this direction.
  • Outputs from all of the transducers 340A-340D are used to measure forces along the Z-axis.
  • the flexure components 251-254 are relatively stiff or rigid for lateral loads, that being in a direction parallel to axis 62. Overturning moments about the X-axis are measured from the output signals from transducers 340A and 340C; while overturning moments about the Y-axis are measured from the output signals from transducers 340B and 340D; and while overturning moments about the Z- axis are measured from the output signals from transducers 340A-340D.
  • Processor 380 receives the output signals from the sensing circuits of the transducers to calculate forces and/or moments as desired, typically with respect to the orthogonal coordinate system 331.
  • a counter balance system or assembly can be provided to support the nominal static mass of the test specimen, other components of the operating environment such as roadways, simulators and components of the platform balance itself.
  • the counter balance system can take any one of numerous forms such as airbags, hydraulic or pneumatic devices, or cables with pulleys and counter weights.
  • An important characteristic of the counter balance system is that it is very compliant so as not to interfere with the sensitivity or measurement of the forces by the transducer assemblies in order to measure all of the forces and moments upon the test specimen.
  • the counter balance system is schematically illustrated by actuators 330.
  • the counter balance system can be removed as explained below, which can be a very large cost savings.
  • the sensor body 242 includes a biasing structure 402 disposed on the sensor body 242 so as to develop a biasing offset force in a selected direction, herein by way of example along the axis 63 in the Z-direction.
  • the biasing structure 402 comprises cantilevered beams 404A and 404B.
  • remote ends 406A and 406B extend in opposite directions where each of the beams 404A and 404B are mounted to the sensor body 242 by a base support 408.
  • the cantilevered beams 404A and 404B can each have a separate base support secured to sensor body 242; however use of a single base support 408 is of a simpler construction.
  • the beams 404A and 404B extending in opposite directions alternative embodiments may have the beams extend toward each other.
  • the biasing structure 402 need not be a cantilevered beam, but can be any structure that is configured to provide a biasing force for the purpose described below.
  • the biasing structure 402 can be formed integral with the sensor body 242 from a single unitary body; however, this should not be considered limiting in that individual components can be joined together and/or joined to the sensor body 242 to realize the same structure.
  • biasing retaining elements 418 connect the biasing structure 402 (located between the clevis halves 16 and 18) to the clevis halves 16 and 18.
  • the biasing retaining elements 418 operate in tension and herein comprise elongated connectors 420 each joined at a first end 420A to one of the remote ends 406A or 406B with a suitable fastener herein bolts 422.
  • a second end 420B of the elongated connectors 420 is joined to both of the clevis halves 16 and 18, herein by a bridging block 424 separately connected to each of the clevis halves 16 and 18 with a suitable fastener herein bolts 426.
  • Biasing retaining elements 418 in one embodiment comprise straps or flexible members. As shown, straps 418, under tension, are coupled at one end 420A to a cantilevered beam at its remote end, and are coupled at the other end 420B to bridging block 424 coupled to clevis halves 16 and 18. Together, the biasing elements 418, bridging block 424, and fasteners such as 422 and 426 comprise a biasing assembly connected between the support (clevis halves 16 and 18) and the sensor body 12 to provide a bias force between the sensor body 12 and the clevis halves. As shown, a width 423 of the straps 418 is greater than a thickness 425 of the straps 418.
  • a biasing assembly in one embodiment comprises a pair of straps provided on opposite portions of the transducer body that are symmetric in configuration, to allow for compliance in a direction orthogonal to the offset.
  • the straps 418 may have a square cross-section, that is, an equal width 423 and thickness 425, or cylindrical, with a constant diameter in every cross-section direction, or other symmetric configurations such as will be evident to those of skill in the art.
  • a biasing actuator 432 preloads the biasing structure 402 and in particular bends the cantilevered beams 404A and 404B by pulling on the bridging block 424 upwardly with the biasing actuator 432 operably connected to standoffs 434.
  • Any form of actuator can be used such as but not limited to a hydraulic, electric, etc.
  • the actuator 432 comprises a screw or bolt mechanically connecting the standoffs 434 with the bridging block 424.
  • a biasing force can be provided as follows. With a loose connection of the bridging block 424 to the clevis halves 16 and 18, each biasing actuator 432 on each side of the sensor body 242 is operated to obtain the desired preloading on the biasing structure 402 as a whole at which point the bridging blocks 424 are then securely fixed to the clevis halves 16 and 18 to retain the desired bias force.
  • the bias force from each cantilever 404A and 404B is iteratively increased until the desired bias force is obtained.
  • the contribution of the bias force from each cantilever 404A and 404B should be the same so as to not induce a moment in the sensor body 242, but rather provide a purely linear bias force in a direction parallel to axis 63 in the illustrated embodiment.
  • biasing structure need not be provided on the sensor body 242, or only on the sensor body 242.
  • Figs. 26-28 illustrate a transducer assembly 500 having many of the same components of the previous transducer assembly, which have been identified with the same reference numbers.
  • additional biasing structures 502 have been formed on each of the clevis halves 16 and 18.
  • the biasing structure 502 is similar to biasing structure 402 discussed above; and thus, much if not all the discussion applicable to biasing structures 402 is applicable to biasing structures 502.
  • cantilevered beams 504A and 504B and a single base support 508 are integrally formed from a single unitary body; however, this is but one embodiment, where other structures as described above with respect to biasing structure 402 can also be used.
  • biasing retaining elements 518 connect the biasing structures
  • each of the biasing retaining elements 518 operate in tension and herein comprise elongated connectors 520 with a first end having a bridging block 524 at a first end 520A connecting the remote ends 506A or 506B together with a suitable fastener herein bolts 522.
  • a second end 520B of each of the elongated connectors 520 is joined to the sensor body 242, with a suitable fastener herein bolts 526.
  • Biasing retaining elements 518 in one embodiment have the properties and characteristics described above with respect to biasing elements 418.
  • sensor body 242 also includes biasing structure 402 having similar components identified with the same reference numbers.
  • a biasing actuator not shown but connectable in a manner similar to that described above and is in effect removably connected to each of the beams 404 A, 404B so as to pull the beams 404 A, 404B upwardly in Fig. 28 at which point the retainer 418 is securely fixed to retain the bias force such as by securely fixing the bridging block 424 to the sensor body 242.
  • a biasing actuator not shown but connectable in a manner similar to that described above and is in effect removably connected to each of the beams 504A of each clevis 16, 18 so as to pull the beams 504A or 504B in pairs on each side of the transducer 500 using corresponding bridging blocks 524 and suitable standoffs as needed.
  • the associated end 520B of the bias retainer 518 can be securely fixed to the sensor body 242.
  • any form of actuator can be used such as but not limited to screws or bolts, hydraulic, electric, etc.
  • An overtravel stop can be provided to limit the bias force created by the pairs of beams 504A and 504B on the clevis halves 16 and 18.
  • a bolt 550 is secured to support 408 and extends through an aperture 552 provided in element 17 connecting the clevis halves 16, 18 together.
  • the head of the bolt 550 is of size to be larger than the aperture 552.
  • the bolt 552 is secured to the support 408 with the head of the bolt spaced apart from a surface of the connecting element a selected distance corresponding to a limit of bias force to be generated by beams 504A and 504B. Since loading of beams 504A and 504B causes the sensor body 242 to move upwardly in Fig. 29, contact of the head of the bolt 552 limits the bias force that can be generated.
  • the lock up assembly 600 includes friction plates 602 attached to each of the clevis halves. Each friction plate 602 is attached to its corresponding clevis half with a fastener 604 such as a plurality of fasteners in the center of the plate. However, it should be noted that only the center of the plate is in permanent contact with the corresponding clevis halves in that the extending ends 606 of the friction plates 602 are spaced apart from the outer surface of the corresponding clevis half.
  • a spacer 608 is securely fixed to the sensor body and is disposed between ends 606 of the friction plates 602 on each side of the transducer.
  • the length of the spacer 608 is slightly shorter than the distance between the inner surfaces of the friction plates such that a gap 610 is present between one or both of the end surfaces of the spacer 608 and corresponding inwardly facing surfaces 612 of the friction plates 602.
  • An actuator 614 is operably coupled to the friction plates 602.
  • the actuator 614 includes a pull rod 616 that extends through a bore 618 in the spacer.
  • the bore 618 is of size to maintain a gap between the pull rod 616 and the spacer 618 for movements of the sensor body 12 or the clevis halves 16 and 18 relative to the sensor body 12.
  • the actuator 614 When it is desired to inhibit movement of the sensor body 12 relative to the clevis halves 16 and 18, the actuator 614 is operated so as to retract the pull rod 616 which pulls the ends 606 of the friction plates 602 together thereby eliminating the gap(s) 610 between the end surface(s) of the spacer 608 and the inwardly facing surface(s) 612 of the friction plates 602 as well as eliminating the gap(s) 620 between the inwardly facing surface(s) 612 of the friction plates 602 and the outwardly facing surface 622 of each corresponding clevis half.
  • the actuator 614 when the actuator 614 is operated, a solid connection is formed between the spacer 608 and the friction plates 602 wherein the friction plates 602 frictionally engage the outer surfaces 622 of each corresponding clevis half.
  • the actuator 614 can be of any suitable form such as but not limited to an electric, hydraulic, or pneumatic actuator.
  • each of the friction plates 602 includes areas of reduced thickness that form flexible hinges 624.
  • the flexible hinges 624 ensure that the ends 606 of the friction plates 602 will maximize contact of the end surfaces of the friction plates 602 with the clevis halves 16 and 18 rather than being slightly at an angle if the flexible hinges 624 were not present.
  • the portion of the friction plates 602 that secure the friction plates 602 to the clevis halves by the fasteners indicated at 604 is maintained in a planar fashion to the corresponding clevis halves.
  • each of the end portions 606 of the friction plates 602 will contact the corresponding clevis half in a planar fashion. Any slight difference in width between the center sections of the friction plates 602 and the end portions of the friction plates 602 is accommodated by the middle sections between each of the flexible hinges 624.
  • a 20,000 pound upper frame is supportable with four transducer bodies while still allowing accurate measurement of loads in a full scale measure load of +/- 2,000 pounds vertical, without frequency degradation of a dead-weight type tare system.
  • Such embodiments are amenable to use with other load cells where tare mitigation is employed, without departing from the scope of the disclosure.
  • thermal expansion differences can lead to thermal structural temperature equilibration between components of the transducer body and any sensing elements therein.
  • Thermal expansion differences between, for example, parallel springs (e.g., the cantilevered beams) in series with straps and those in parallel with gauged beam assemblies, and the resulting disparate temperatures between elements, may result in thermal drift for a duration of a test.
  • FIG. 33 shows a fluid enclosure 700 for a transducer assembly such as the various transducer assembly embodiments described herein.
  • fluid enclosure 700 is an oil enclosure or oil bath, such as a fluid recirculating bath assembly. Elements of the transducer, especially straps, cantilevered beams, gauged elements, sensor body, clevis plates, and bottom plates, are immersed in the fluid of the fluid enclosure 700, and are held in one embodiment to a same temperature with a tolerance of about 0.1 °F for a testing cycle.
  • fluid enclosure 700 contains an oil 702 heated to a desired temperature at which the elements of the transducer are to be held. Oil 702 has high thermal mass and very good heat conduction and convection to and with the elements of the transducer assembly. This allows maintenance of thermal uniformity within a desired tolerance even when the transducer assembly is in an operating wind tunnel.
  • Oil enclosure 700 further comprises cross flow inlets 704 and outlets 706, and a fluid circulating bath tank 708 mounted to a plate 710.
  • a gasket 712 seals tank 708 to plate 710 in one embodiment.
  • Further gaskets 714 may be used to seal plate 710 to a bottom plate such as connecting member 17of a transducer body (FIG. 1), for example by sealing each bolt between bottom flexures 716 and connecting member 17, or by sealing with a larger gasket around a circumference of the bottom flexures 716.
  • Top flexures 718 may be coupled, for example with bolts, to the sensor body of the transducer assembly.
  • Associated plumbing (not shown) provides oil 702 at the desired temperature for the components to the enclosure 700 via inlets 704, recirculated to the plumbing and heater (not shown) via outlets 706.
  • a top cover 720 shown in FIG. 34, may be used to provide protection against contaminants such as dirt or dust into the tank 708.
  • oil is provided to fill tank 708 to fill line 722, so that sensing elements that may be in the transducer body are completely submerged in the oil.
  • FIGS. 35-39 illustrate a transducer body 800 having many of the same components of the prior transducer assemblies, the parts of which have been identified with the same reference numbers.
  • clevis halves 16 and 18 are joined together by the connecting member 17.
  • a sensor body 12, for example, similar to that illustrated in FIG. 2 includes a rigid perimeter structure 22 identified in FIGS. 35 and 37-39.
  • a biasing structure 802 is operably coupled to the clevis halves 16 and 18 and the sensor body 22.
  • the biasing structure 802 includes first and second spring assemblies 804a and 804b disposed on opposite sides of the transducer assembly 800.
  • Each assembly, 804a and 804b includes a spring 806 (herein operative in tension) having a first end 808coupled to the perimeter body 22 of the sensor body using a mount 810 secured to the perimeter by 22 with fasteners 812 (see also FIG. 38).
  • a second connecting member 814 also joins the clevis halves 16 and 18 together on ends opposite the connecting member 17.
  • the connecting member 814 includes opposed ears 816 that secure a second end 818 of each spring 806 to a corresponding ear 816 of connecting member 814 and thus to the clevis halves 16 and 18.
  • a biasing actuator 832 is provided for each of the springs 806. Referring also to
  • the biasing actuator 832 includes an actuating member herein comprising a bolt 834 having an end 836 in engagement with ear 816.
  • the actuating member or bolt 834 is used to create separation between a plate 838 and the ear 816.
  • the plate 838 is coupled to end 818 of spring 806 with rods 840 that extend from plate 838 and through suitable apertures provided in ear 816.
  • the rods 840 are connected to a mounting plate 842 that in turn is mounted to the end 818 of the spring 806 using a plurality of fasteners 844.
  • coupling rods 840 pull the end 818 of the spring 806 toward the ear 816 thereby creating a bias (tension force) between the sensor body 22 and the clevis halves 16 and 18.
  • the transducer assembly 800 includes mounts 860 fixedly secured to the connecting member 17 and thus the clevis halves 16 and 18. Likewise, mounts 862 are secured to or formed integrally as a single unitary body with the perimeter body 22. Each mount 862 extends through a corresponding aperture 864 provided in connecting member 814.
  • FIGS. 35-38 include the lock up assembly 600 having similar components identified with reference numbers as described above, in this embodiment extending end 606 directly engage the sensor body or perimeter body 22.
  • FIG. 40 illustrates a transducer body 900 having many of the same components of the prior transducer assemblies, the parts of which have been identified with the same reference numbers.
  • the biasing structure 402 of FIG. 18 is modified.
  • Sensor body 900 comprises a biasing structure 902 similar to that of structure 402 in FIG. 18.
  • pair of cantilevered beams 904A and 904B are used in place of the beams 404A and 404B.
  • the biasing structure 902 comprises cantilevered beams 904A and 904B.
  • remote ends 906A and 906B extend in opposite directions where each of the beams 904 A and 904B are mounted to the sensor body 900 by a base support 908.
  • Beams 904A and 904B comprise a body 910A and 910B, with bodies 910A,
  • FIG. 41 illustrates a transducer assembly 920 having many of the same components of the prior transducer assemblies, the parts of which have been identified with the same reference numbers.
  • FIG. 41 illustrates a transducer assembly 920 having many of the same components of the prior transducer assemblies, the parts of which have been identified with the same reference numbers.
  • biasing structure 922 having beams 924A and 924B is formed on clevis halves 16 and 18 instead of on a sensor body.
  • the biasing structure is similar to biasing structure 902 discussed above; and thus, much if not all the discussion applicable to biasing structures 902 is applicable to biasing structures 922.
  • cantilevered beams 924A and 924B having ends 926A and 926B and a single base support 928 are integrally formed from a single unitary body; however, this is but one embodiment, where other structures as described above with respect to biasing structure 902 can also be used.
  • the beams 924A and 924B are strapped in the same way as beams 504A and 504B as described above.
  • FIG. 42 illustrates a transducer assembly 950 having many of the same components of the prior transducer assemblies, the parts of which have been identified with the same reference numbers.
  • a biasing structure 952 is shown in FIG. 42.
  • Biasing structure 952 uses a single cantilevered beam 954 on each clevis half 16, 18.
  • Each single cantilevered beam 954 has a remote end 956 opposite a base support 958.
  • base support 958 is at one edge 962 of its clevis half, and the cantilevered beam 954 extends substantially entirely across the clevis half to opposite edge 964 and remote end 956.
  • Beam 954 comprises a body 960 having a plurality of milled slots 9622 therein.
  • the number of milled slots may be chosen for a desired amount of deflection. The higher the number of slots, the greater the deflection allowed.
  • a first beam 954 on one side of its sensor body has a cantilevered beam 854 that extends from support 958 at edge 962 to edge 964.
  • a second beam 954' on the other side of the sensor body has a cantilevered beam 954' that extends from its support 958' at edge 964 to edge 962.
  • Beam 954 is strapped to sensor body with a strap attached between the sensor body and end 956 in similar fashion to the strapping of beams 504A and 504B described above, but is only attached between its own outer plate (e.g., clevis half 18) and the sensor body, not between both outer plates (e.g., clevis halves 16 and 18).
  • Beam 954' is strapped to sensor body with a strap attached between the sensor body and end 956' in similar fashion to the strapping of beams 504A and 504B described above, but is only attached between its own outer plate (e.g., clevis half 16) and the sensor body, not between both outer plates (e.g., clevis halves 16 and 18).
  • remote ends 956 and 956' are at opposite edges of the sensor body, and beams 954 and 954' extend in opposite directions. With this configuration, forces of tension provided by the strap connections between the beams 954, 954' and the sensor body are balanced, so that no net torque is imparted on the system.
  • each beam 954, 954' is approximately 20 inches long, and approximately one inch tall, with four pockets 962, 962' milled in bodies 960, 960' .
  • pockets 962, 962' may be used without departing from the scope of the disclosure.
  • flexure components such as beams 904 A, 904B, 924 A,
  • 924B, 954, and 954' may be formed separately from the clevis halves 16, 18, and bolted thereto to provide tensioning for the sensor body.
  • a different material could be used, such as alloys that have different spring tensions and/or materials that respond in more predictable ways to temperature changes.
  • beams such as beams 904 A, 904B, 924 A, 924B, 954, and 954' may be formed from a material such as NI-SPAN-C®, which can be processed to have a constant modulus of elasticity at temperatures from -50 to 150°F.
  • FIG. 43 illustrates a transducer assembly 1000 having many of the same components of the prior transducer assemblies, the parts of which have been identified with the same reference numbers.
  • transducer assembly 1000 as in the earlier embodiment, clevis halves 1016 and 1018 sandwich a sensor body 12, for example, similar to that illustrated in FIG. 2.
  • a sensor body 12, for example, similar to that illustrated in FIG. 2 includes a rigid perimeter structure 22 identified in FIGS. 35 and 37-39.
  • a biasing structure 1002 is operably formed from portions of the clevis halves 1016 and 1018 and coupled to the sensor body 22.
  • the biasing structure 1002 for clevis half 1018 includes spring assemblies 1017 and 1019 formed as an upper portion of clevis half 1018.
  • Clevis half 1018 is separated from the sensor 12 by a gap 1020.
  • First and second spring assemblies 1017 and 1019 are disposed on opposite sides of center line 1021.
  • Spring assemblies 1017 and 1019 each have a first end 1022 coupled to connecting member 17 and a second end 1024 joining body 1026 of clevis half 1018.
  • Clevis halves 1016, 1018 are coupled to the perimeter body 22 of the sensor 12.
  • Spring assemblies 1017, 1019 allow tensioning along a center line 1021 of the transducer assembly 1000 at a midpoint between edges 1028 and 1030.
  • Spring assemblies 1017 and 1019 are shown in schematic form.
  • springs and assemblies may be used without departing from the scope of the disclosure.
  • a milled spring assembly, coil spring assembly, or the like could be used without departing from the scope of the disclosure.
  • the spring assemblies 1017, 1019 can be formed integral with each respective clevis halve 1016, 1018 as a single unitary body.

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  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Force Measurement Appropriate To Specific Purposes (AREA)

Abstract

Selon un aspect, l'invention concerne un corps de transducteur (800, 900, 920, 950, 1000) qui comprend : un support comprenant une paire de moitiés de manille (16, 18) ; et un corps de capteur (12) accouplé à chacune des moitiés de manille (16, 18). Le corps de capteur (12) est disposé entre les moitiés de manille (16, 18) et comprend un élément périphérique généralement rigide disposé autour d'un moyeu central espacé, le moyeu central étant relié à chacune des moitiés de manille (16, 18) avec l'élément périphérique espacée de chaque moitié de manille (16, 18), au moins trois éléments fléchisseurs accouplant l'élément périphérique au moyeu central. Les éléments fléchisseurs sont espacés les uns des autres à des intervalles d'angle généralement égaux autour du moyeu central ; et un ensemble de sollicitation est relié entre le support et le corps de capteur et conçu pour fournir une force de sollicitation entre le corps de capteur et le support. Des formes uniques d'ensembles de sollicitation sont décrites dans chacun des corps de transducteur (800, 900, 920, 950, 1000).
PCT/US2017/020743 2016-03-03 2017-03-03 Transducteur de charge à deux axes à ensemble de sollicitation WO2017152101A1 (fr)

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CN117572021A (zh) * 2024-01-17 2024-02-20 中国工程物理研究院电子工程研究所 敏感结构及加速度传感器

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US5974879A (en) * 1997-05-27 1999-11-02 Alliedsignal Inc. Micromachined rate and acceleration sensor
US7788984B2 (en) 2003-12-04 2010-09-07 Mts Systems Corporation Platform balance
WO2015017806A2 (fr) * 2013-08-01 2015-02-05 Mts Systems Corporation Corps de capteur à deux axes pour un transducteur de charge et balance à plateau en étant équipée

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Publication number Priority date Publication date Assignee Title
US5974879A (en) * 1997-05-27 1999-11-02 Alliedsignal Inc. Micromachined rate and acceleration sensor
US7788984B2 (en) 2003-12-04 2010-09-07 Mts Systems Corporation Platform balance
WO2015017806A2 (fr) * 2013-08-01 2015-02-05 Mts Systems Corporation Corps de capteur à deux axes pour un transducteur de charge et balance à plateau en étant équipée

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN117572021A (zh) * 2024-01-17 2024-02-20 中国工程物理研究院电子工程研究所 敏感结构及加速度传感器
CN117572021B (zh) * 2024-01-17 2024-04-05 中国工程物理研究院电子工程研究所 敏感结构及加速度传感器

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