Abstract: In a pressure sensor, a cap-shaped shielding member (17) to block an electric field undesirable for a signal processing electronic circuit unit of a sensor chip (16) is supported by an end surface of a disk conductive plate (19) between one end surface of the sensor chip (16) in a liquid sealing chamber (13) and a diaphragm (32). The conductive plate (19) is electrically connected via a group of input-output terminals (40ai) and bonding wires (Wi), for example, and the sensor chip (16) is supported by one end portion of a chip mounting member (18) which is electrically connected via the group of input and output terminals (40ai) and the bonding wires (Wi).

Abstract: In a pressure sensor, a cap-shaped shielding member (17) to block an electric field undesirable for a signal processing electronic circuit unit of a sensor chip (16) is supported by an end surface of a disk conductive plate (19) between one end surface of the sensor chip (16) in a liquid sealing chamber (13) and a diaphragm (32). The conductive plate (19) is electrically connected via a group of input-output terminals (40ai) and bonding wires (Wi), for example, and the sensor chip 16 is supported by one end portion of a chip mounting member (18) which is electrically connected via the group of input and output terminals (40ai) and the bonding wires (Wi).

Abstract: An intelligent fastener unit for fastening together structural members. The fastener unit includes a fastener with an externally threaded shank, an internally threaded mating member for threaded engagement with the fastener, and an intelligent washer having an RFID tag and an antenna mounted on one surface of a centrally aperture body member, and a pressure sensor mounted on the opposite surface for generating electrical signals representative of the compressive force applied to structural members captured by the fastener, the mating member and the washer. An air gap is formed in the washer body member between the outer periphery and the central aperture to reduce eddy current formation when the RFID tag is interrogated by an RFID tag reader using r.f. signaling.

Abstract: A force sensor comprising a substrate, a semiconductor body, and a piezoresistive element provided on a top surface of the semiconductor body. The semiconductor body is connected to the substrate in a force-fit manner, and includes a first wing which is provided on the top surface of the semiconductor body and being connected to the semiconductor body in a force-fit manner. A first force application area is provided on the first wing. A second wing has a second force application area provided opposite the first wing. The piezoresistive element is disposed between the first wing and the second wing. A force distribution component is connected to the first force application area and the second force application area in a force-fit manner. The force distribution component having a first surface which is oriented away from the top surface of the semiconductor body and includes a third force application area.

Abstract: A sensor for measuring pressure, temperature or both may be provided. The sensor may include a diaphragm that may respond to a change in temperature or pressure, a base connected to the diaphragm, a cavity, and an optical fiber that may conduct light reflected off of a surface of the diaphragm. The diaphragm and base may be sapphire elements. An interrogator may be provided for detecting a deflection of the diaphragm.

Abstract: In an embodiment, an apparatus includes a first substrate. The first substrate may have a first side for accommodating a first diaphragm. The first substrate may also have a second side. The second side may include a polygonal-shaped depression that is sized to accommodate a second diaphragm associated with a second substrate. The first substrate and first diaphragm may be included in a first assembly and the second substrate and second diaphragm may be included in a second assembly. The first assembly and the second assembly may be included in a stack where at least a portion of the second diaphragm is positioned to fit inside the polygonal-shaped depression in the stack.

Abstract: In an operation amount detecting apparatus, a brake pedal is coupled with an operation rod by a coupling shaft, respective end portions of an elastic member are supported at support positions of a brake pedal by support shafts, the brake pedal is away in a direction orthogonal to an axis line direction of an operation rod with respect to the coupling shaft, an intermediate portion of the elastic member is relatively displaceably coupled by the coupling shaft and a coupling hole, and the elastic member is disposed with output strain sensors which detect an elastic deformation amount of the elastic member and output the elastic deformation amount as a brake operation amount.

Abstract: A first substrate that includes pressure sensors which are disposed in plural around a reference point; an approximately hemispherical elastic protrusion that is positioned so that the center of the elastic protrusion is approximately disposed in a position which is overlapped with the reference point, and is elastically deformed by an external force; and a second substrate that is separated from the elastic protrusion and installed on a side which is opposite to the first substrate are provided. When the external force is applied, a predetermined calculation is performed by using a pressure value which is detected through each pressure sensor, and the direction and the intensity of the applied external force are obtained.

Abstract: A sensing insert device (100) is disclosed for measuring a parameter of the muscular-skeletal system. The sensing insert device (100) can be temporary or permanent. Used intra-operatively, the sensing insert device (100) comprises an insert dock (202) and a sensing module (200). The sensing module (200) is a self-contained encapsulated measurement device having at least one contacting surface that couples to the muscular-skeletal system. The sensing module (200) comprises one or more sensing assemblages, electronic circuitry (307), an antenna (2302), and communication circuitry (320). The sensing assemblages are between a top plate (1502) and a bottom plate (1504) in a sensing platform (121). The sensing assemblages comprise a load disc (2004) and a piezo-resistive sensor (2002) to measure the parameter. An elastic support structure or springs (1108) is coupled between the top plate (1502) and the bottom plate (1504) to prevent cantilevering of a surface.

Abstract: A multicapacitor sensor system facilitates the measurement of applied shear and moment forces. In one disclosed configuration, moments may be detectable in x, y and z directions, resulting in a full, 3-axis load cell with 6 degrees of freedom. The system may further include electrical circuitry to generate electrical drive pulses, sense amplify and buffer the voltages induced on the sense plates, and compute applied forces. An array of multicapacitor sensors that can be addressed individually without cross-talk and globally produce a map of forces and moments applied to the whole array. A MEMS implementation enables in vivo application.

Abstract: A force sensor includes a first surface and a second surface located opposite the first surface, the first surface translatable against a resilient force in a direction towards and/or from the second surface; a distance sensor, arranged to measure the distance between the first surface and the second surface; characterized in that the force sensor comprises a flexible coupling extending along the direction, flexibly coupling the first surface to the second surface; and in that the flexible coupling is provided with a resilient means to provide the resilient force; and a space encompassed by the flexible coupling together with the first surface and the second surface being accessible to the distance sensor, the space filled with a medium for providing the resilient force.

Abstract: The force calculation system of the present invention is provided with: an air blowing unit for blowing air at a predetermined pressure; a flow passage for air blown from air blowing unit; a sensing unit for changing the ease of flow of air that flows through a flow passage by deforming when an external force is given; a storage unit for storing in advance the flow volume-force correspondence information showing the correspondence between the magnitude of the force received by the sensing unit and the flow volume at which air blown from air blowing unit flows through the flow passage; and a processing unit for calculating the magnitude of external force received by the sensing unit, on the basis of the flow volume of air flowing through the flow passage as measured by a flow volume meter; and the flow volume-force correspondence information stored in the storage unit.

Abstract: A non-rigid electrical component includes a first layer of a compressible material. The first layer has at least one aperture therethrough. A second layer of an electrically conductive material is positioned on one side of the first layer across the aperture and a third layer of an electrically conductive material is positioned on an opposite side of the first layer across the aperture. The first layer is compressible such that the second and third layers of material may be brought into contact with each other in the aperture of the first layer to complete an electrical connection between the second and third layers upon application of a compression force. The first layer is also made of a resilient material such that when the compression force is removed, the first material expands to separate the second and third layers, thereby breaking the electrical connection.

Abstract: A force gauge assembly used to measure forces or spring rate of an object utilizing a diaphragm strain gauge for mechanically compensating for loads not being centrally applied to the gauge. The construction of the gauge provides readings that will be substantially the same as if the load were applied in perfect alignment. The gauge utilizes internal components that remain the same even though the force gauge is adaptable for measuring different objects.

Abstract: A force-measuring ring includes an annular housing which contains at least one piezoelectric measuring element, and a pressure transmission element which is attached to the housing via inner and outer circular-annular membrane areas. The inner and outer membrane areas of the force measuring ring are situated on opposite sides of a symmetry plane defined by the at least one piezoelectric measuring element.

Abstract: A load sensing platform (121) is disclosed for capturing a transit time, phase, or frequency of energy waves propagating through a medium that measures a parameter of the muscular-skeletal system. The load sensing platform (121) comprises a sensing assemblage (1), substrates (702, 704, and 706), springs (315), spring posts (708), and spring retainers (710). The sensing assemblage (1) comprises a stack of a transducer (5), waveguide (3), and transducer (6). A parameter is applied to the contact surfaces (8) of the load sensing platform (121). The sensing assemblage (1) measures changes in dimension due to the parameter. Position of the applied parameter can be measured by using more than one sensing assemblage (1). The springs (315) couple to the substrates (702, 704) providing mechanical support and to prevent cantilevering. The spring posts (708) and spring retainers (710) maintain the springs (315) at predetermined locations in the load sensing platform (121).

Abstract: A sensing insert device (100) is disclosed for measuring a parameter of the muscular-skeletal system. The sensing insert device (100) can be temporary or permanent. Used intra-operatively, the sensing insert device (100) comprises an insert dock (202) and a sensing module (200). The sensing module (200) is a self-contained encapsulated measurement device having at least one contacting surface that couples to the muscular-skeletal system. The sensing module (200) comprises one or more sensing assemblages, electronic circuitry (307), an antenna (2302), and communication circuitry (320). The sensing assemblages are between a top plate (1502) and a bottom plate (1504) in a sensing platform (121). The sensing assemblages comprise a load disc (2004) and a piezo-resistive sensor (2002) to measure the parameter. An elastic support structure or springs (1108) is coupled between the top plate (1502) and the bottom plate (1504) to prevent cantilevering of a surface.

Abstract: The force sensing device includes a deformable member having portions arranged to make a pair with respect to the Z-axis. Three sets of strain detecting elements are formed on the deformable member for detecting deformations of the deformable member caused by a linear force in the X-axis, a linear force in the Y-axis and a rotational force about the Z-axis. The force sensing device includes a connecting member which connects between the pair of portions of the deformable member, and between the deformable member and a shaft of a manipulatable member. The force sensing device can be manufactured with easy wiring work and can detect the applied force in three degrees of freedom, including the linear force in the X-axis, the linear force in the Y-axis and the rotational force about the Z-axis.

Abstract: A displacement, strain, and/or force sensor assembly (10, 110) has a mounting structure (12) with an anisotropic stiffness to facilitate the measurement of displacements, strains, and/or forces along the X-axis, while minimizing errors due to undesired displacements, strains, and/or forces along the Y- and Z-axes, and rotations about the X-, Y-, and Z-axes. A pedestal (30, 130) configured to respond to axial displacements along the X-axis is centrally disposed on the X-axis of the mounting structure (12), and a displacement or strain sensor (38) is coupled to the pedestal (30) to provide a measure of the displacements, strains, and/or forces. Contact pads (14, 114) are formed on opposite ends of the X-axis of the mounting structure, to enable the displacement and/or strain sensor assembly to be secured to an application structure.

Abstract: A feedback system for identifying an external force, includes an operation plate and a pressure-sensing unit. The pressure-sensing unit includes an elastic member supporting the operation plate and a pressure sensor inside the elastic member. The pressure sensor includes a pressure sensitive film. An inner side of the elastic member is filled with fluid material which acts on the pressure sensitive film. The operation plate is driven by the external force to be slant which extrudes the elastic member to deform so as to change fluid pressure of the fluid material limited in the elastic member, and such change of the fluid pressure can be sensed by the pressure sensitive film of the pressure sensor so as to identify the movement and the intensity of the external force.

Abstract: In an operation amount detecting apparatus, a brake pedal (11) is coupled with an operation rod (15) by a coupling shaft (18), respective end portions of an elastic member (21) are supported at support positions of a brake pedal (11) by support shafts (28, 29), the brake pedal (11) is away in a direction orthogonal to an axis line direction of an operation rod (15) with respect to the coupling shaft (18), an intermediate portion of the elastic member (21) is relatively displaceably coupled by a support shaft 18 and a coupling hole (11a), and the elastic member (21) is disposed with output strain sensors (30a, 30b, 31a, 31b) which detect an elastic deformation amount of the elastic member (21) and output the elastic deformation amount as a brake operation amount.

Abstract: The invention relates to a method for determining the elastic deformation of components, especially parallel kinematic devices, under a load. Said method is characterised in that the geometry of the articulation points on the fixed platform (9) and the mobile platform (10) is determined; the replacement spring constants of the actuators (K1, K2, K3) and the replacement spring constants of the bearings are determined; the theoretical length of the actuators is determined; the theoretical position of all of the articulation points in the area is determined therefrom; the forces acting on the individual actuators are determined from said geometry and the load (F); and the real geometrical image and thus the real position of the mobile platform are determined from said forces. The real position is compared with the calculated theoretical position and is brought into line by the actuation of corresponding actuators.

Abstract: A scale includes a stationary bracket, a movable bracket, a linear displacement sensor and a plurality of the resilient mechanisms. The movable bracket is disposed opposite to the stationary bracket. The linear displacement sensor is disposed between the stationary bracket and the movable bracket. The resilient mechanisms are disposed between the stationary bracket and the movable bracket. Each resilient mechanism includes a limiting shaft, a sleeve movably sleeved on the limiting shaft and a resilient member received in the sleeve. The limiting shaft is fixed to one of the stationary bracket or the movable bracket, and the sleeve is fixed to the other. The resilient member is elastically deformed by resisting a free end of the limiting shaft. The linear displacement sensor registers a displacement of the movable bracket.

Abstract: An elastic body for measuring loads and a non-contact load-measuring device are disclosed. The elastic body includes: an elastic body base; a multiple number of slits formed in the elastic body base; and a deforming space part formed in the elastic body base. Inside the deforming space part are formed: a hinge, a first deforming part coupled with the hinge, and a second deforming part that is coupled with the first deforming part and the hinge and is formed with a greater length than that of the first deforming part. The first deforming part and second deforming part are configured to undergo rotational movements about the hinge in correspondence to the load, the first deforming part moving downwards in correspondence to the load and the second deforming part moving upwards in correspondence to the load. The upward displacement of the second deforming part is used for measuring the load.

Abstract: A load sensing platform (121) is disclosed for capturing a transit time, phase, or frequency of energy waves propagating through a medium that measures a parameter of the muscular-skeletal system. The load sensing platform (121) comprises a sensing assemblage (1), substrates (702, 704, and 706), springs (315), spring posts (708), and spring retainers (710). The sensing assemblage (1) comprises a stack of a transducer (5), waveguide (3), and transducer (6). A parameter is applied to the contact surfaces (8) of the load sensing platform (121). The sensing assemblage (1) measures changes in dimension due to the parameter. Position of the applied parameter can be measured by using more than one sensing assemblage (1). The springs (315) couple to the substrates (702, 704) providing mechanical support and to prevent cantilevering. The spring posts (708) and spring retainers (710) maintain the springs (315) at predetermined locations in the load sensing platform (121).

Abstract: A sensing insert device (100) is disclosed for measuring a parameter of the muscular-skeletal system. The sensing insert device (100) can be temporary or permanent. Used intra-operatively, the sensing insert device (100) comprises an insert dock (202) and a sensing module (200). The sensing module (200) is a self-contained encapsulated measurement device having at least one contacting surface that couples to the muscular-skeletal system. The sensing module (200) comprises one or more sensing assemblages, electronic circuitry (307), an antenna (2302), and communication circuitry (320). The sensing assemblages are between a top plate (1502) and a bottom plate (1504) in a sensing platform (121). The sensing assemblages comprise a load disc (2004) and a piezo-resistive sensor (2002) to measure the parameter. An elastic support structure or springs (1108) is coupled between the top plate (1502) and the bottom plate (1504) to prevent cantilevering of a surface.

Abstract: The invention relates to a collision sensing device which can detect a collision between two or more objects. The collision sensing device comprises a deformable member (5) that defines a space (15) which can be assigned a pressure. In a first condition, the deformable member is undeformed, whereby the space (15) is assigned a first pressure (P1). In a second condition, the deformable member (5) is deformed whereby the space (15) is assigned a second pressure (P2). The pressure in the space is monitored. A collision with an object is detected when the pressure in the space changes from the first pressure to the second pressure. The invention can e.g. be applied in connection with machining, such as water jet cutting, but several other fields of application are also conceivable.

Abstract: A force-sensing device has a yoke having a location of force introduction for a force to be measured acting in a predetermined direction. A measuring spring has a first end rigidly connected to the yoke and is elastically deformable by the force to be measured. The measuring spring has a second end arranged on a support rigidly connectable to a machine frame. First predetermined measuring locations are provided that detect and evaluate a deformation of the measuring spring caused by the force to be measured. Parallel and spaced apart bending springs are connected to the yoke in such a way that the yoke is always guided in parallel in a transverse direction that is transverse to the predetermined direction of the force to be measured. Second predetermined measuring locations are provided on the bending springs and detect a transverse deformation caused by a force in the transverse direction.

Abstract: The weight sensing device may include a base, a cover, a first load cell attached to the base and the cover, a second load cell attached to the base and in contact with the cover but not attached, and an analyzing circuit which is connected by electrical wires to the load cells. The base may be a fork, for example, a lift truck fork. When a load is positioned on the load bearing surface of the cover, the load cells flex and cause an electrical signal to be transmitted over the wires to the analyzing circuit.

Abstract: The resolution and the signal-to-noise ration of known force sensors as e.g. capacitive force sensors decrease when scaling them down. To solve this problem there is a solution presented by the usage of a nanostructure as e.g. a carbon nanotube, which is mechanically deformed by a force to be measured. The proposed force sensors comprises a support with two arms carrying the carbon nanotube. The main advantage of this nanoscale force sensor is a very high sensitivity as the conductance of carbon nanotubes changes several orders of magnitude when a mechanical deformation arises.

Abstract: A force sensing device has a single-component metal housing. The housing has an upper rigid housing part and a lower rigid housing part that are interconnected by way of U-shaped spring elements and can be elastically displaced along a displacement axis in relation to each other by the action of a force. The spring elements are symmetrically arranged in relation to a section that is parallel to the displacement axis. A deflection sensor is disposed between the upper and lower rigid housing parts, for detecting the relative displacement of the two rigid housing parts in relation to each other. The housing is produced using metal injection molding technology.

Abstract: A force-sensing device has a yoke having a location of force introduction for a force to be measured acting in a predetermined direction. A measuring spring has a first end rigidly connected to the yoke and is elastically deformable by the force to be measured. The measuring spring has a second end arranged on a support rigidly connectable to a machine frame. First predetermined measuring locations are provided that detect and evaluate a deformation of the measuring spring caused by the force to be measured. Parallel and spaced apart bending springs are connected to the yoke in such a way that the yoke is always guided in parallel in a transverse direction that is transverse to the predetermined direction of the force to be measured. Second predetermined measuring locations are provided on the bending springs and detect a transverse deformation caused by a force in the transverse direction.

Abstract: A spring scale, in particular for weighing loads in the ?g-mg range, comprises a load platform suspended by at least three flexural springs in a surrounding frame, and has bridge-connected strain gauges arranged for measuring strain on one side of the flexural springs. The flexural springs extend in succession along substantially the whole periphery of the load platform in a gap between the load platform and the inner edge of the frame, and an attachment spot on the load platform for every flexural spring is arranged substantially directly opposite or past an attachment spot on the inner edge of the frame for a next flexural spring in the succession of springs. Preferably, the spring scale is made in one piece, and manufactured by means of semiconductor process technology.

Abstract: Various sensors use an electro-active device (11) electrically connected to a detector circuit. The electro-active device (11) comprises an electro-active structure in the form of a continuous electro-active member (12) curving in a helix around a minor axis (13) which is in itself curved for example in a helix around a major axis (14). On activation by relative displacement of the ends (16) of the device (11), the electro-active structure twists around the minor axis due to the fact that the minor axis (13) is curved. The continuous member (12) has a bender construction of a plurality of layers (21) and (22) including at least one layer of electro-active material so that concomitantly with the twisting the continuous member (12) bends generating an electrical signal detected by the detector circuit. The electro-active device (11) is advantageous as a sensing element in a sensor because it has a large displacement, high sensitivity and low compliance.

Abstract: An object of the invention is to provide a pressure sensor, an object detecting system and an opening and closing system which realize the improvement in efficiency of sealing work on end portions of the pressure sensor and which are fabricated at low costs, as well as a pressure sensor fabricating method which requires no complex and troublesome steps. A pressure sensor (17) includes a pressure sensing means (a piezoelectric sensor (33)) for detecting a deformation due to an external force and a sensor accommodation body (a support means (35)) which incorporates therein the pressure sensing means and which is made from a thermoplastic elastomer, and the sensor accommodation body is sealed off at at least one end portion thereof through a thermal treatment.

Abstract: A mechanism for reducing horizontal force in load measurement is presented. The mechanism includes a structure having surfaces of nonuniform radii of curvature (e.g., oblate spheroid surfaces) at both ends. The ends of the structure contact a force-sensor coupling element and a base-coupling element, forming two interfaces. Each interface includes a contact area between a convex surface and a concave surface. When a horizontal force is applied, the contact area at each interface shifts, allowing the structure to tip from the vertically aligned position that it is in when no horizontal force is applied. Compared to conventional mechanisms, the structure of the invention has a lower effective height because interfaces between oblate spheroid surfaces allow a larger angle of deflection than flat interfaces. The oblate spheroid interfaces also allow deflection to occur with less wear and tear at the interfaces compared to the flat-interfaced structures.

Abstract: A load cell comprising a load carrying structural framework is arranged with at least one measuring zone (15, 16) arranged with a measuring means. A load F applied in the x-direction parallel to two outer beams (1, 4) of the framework is transferred to two inner beams (2, 3) by two side beams (5, 6). The load on the measuring zones (15, 16) is greater than the load applied parallel to outer beams (1, 4) in a ratio of the distance h between the joints of the two outer beams divided by the distance d between the joints of the two inner beams. When a load is applied in the y-direction parallel to the two side beams (5, 6), the load on the measuring zones is also greater than the load applied at the side beams, in this case by a ratio of the distance l between the joints (7 and 11), (10 and 14) divided by distance d.

Abstract: A soil or snow probe which incorporates a load cell in the probe head and also an accelerometer so that a vertical strength profile of the snow or soil can be established. The device does not need to be driven at a constant speed and can be manually driven into the soil or snow. The resistance to penetration is measured using a load cell which incorporates a low duro polymer selected for its ability to behave like a non compressible fluid. The device is portable and provides data quickly.

Abstract: In order for a load cell with a force transducer for recording a weight, the force transducer having a part which does not deform under loading and a force introduction part with an elastically deformable part, the elastically deformable part and the non-deforming part having in a measuring portion a defined spacing in relation to each other which changes under loading, with a sensor arrangement with an inductively operating sensor element, which is disposed in the measuring portion opposite a signaling face, in order to detect changing of the spacing as an electric signal, and with a circuit for converting the electric signal into a weighing signal, to be developed further in such a way that it can be used in particular in conditions which are very difficult in terms of measuring technology, and in particular under the other special ambient conditions within a vehicle, and the weighing signal of which is substantially uninfluenced by this, it is proposed that the force transducer has a recess in the elastica

Abstract: The invention relates to a system for measuring loading, stresses and/or material fatigue in a structure. The invention also relates to a measuring sensor unit (50) and a measuring sensor (302) suitable for use in connection with said method. The invention is applicable especially to the measurement of stresses and loading on a ship hull. One inventive idea is that the measuring sensor unit (50) of the measuring system comprises means (310) for processing a signal from the sensor so as to allow complete mathematical measuring results to be transmitted (316, 21) from the measuring sensor unit to the central processing unit. Another inventive idea is to form a measuring sensor from the sensor assembly and the strain gauge so that deformations are transmitted to the strain gauge attached to an elastic area of the sensor assembly. By means of the invention, the measuring units can be calibrated apart from the structure material and additional measuring units can be provided in the system whenever necessary.

Abstract: A transducer assembly adapted for use for measuring forces and moments including a stationary center load axle having an elongated extend extending along an elongated axis between spaced opposed ends. The transducer assembly including first and second load cells interposed in a force path between opposed first and second ends of the load axle measuring applied load in the suspension load path of a two wheel vehicle.