95 results about "Mass element" patented technology

A computer-implemented automated building design and modeling and construction project cost estimating and scheduling system (“DMES system”) is described. The DMES system provides a central source for all of the design and construction information for a construction project in a coordinated two-dimensional and three-dimensional spatial database that is freely accessible by all of the members of an interdisciplinary construction project team as a means to produce automatically coordinated design development and construction document information. The DMES system acquires and stores all of the appropriate design, engineering, and construction expertise and information available for any building type for use in automatically assembling and coordinating the design, cost-estimating, and scheduling for a construction project. In one embodiment, the DMES system consists of a plurality of objects, comprising elements and massing elements arranged in an assembly hierarchy. Each of the objects includes programming code that defines an interface and discrete internal functions that define its behavior. When instantiated in the database, the objects automatically create further instances of other objects in the hierarchy, which in turn do the same, thus assembling a complete building model automatically from the initial manually-placed instance. The building model enables automatic generation of drawings and cost and scheduling information. By running automatic iterations of the building model, multiple designs may be evaluated to determine the optimum design.

A continuous or distributed resonator geometry is defined such that the fabrication process used to form a spring mechanism also forms an effective mass of the resonator structure. Proportional design of the spring mechanism and / or mass element geometries in relation to the fabrication process allows for compensation of process-tolerance-induced fabrication variances. As a result, a resonator having increased frequency accuracy is achieved.

A torsional vibration damper on the bridging clutch of a hydrodynamic clutch arrangement has a first connecting device, which can be brought into working connection with the clutch housing and with a drive-side transmission element. The drive-side transmission element is connected via first energy-storage devices to an intermediate transmission element. The torsional vibration damper also has a second connecting device for establishing a working connection via second energy-storage devices between the intermediate transmission element and a takeoff-side transmission element, which is connected to a takeoff-side component of the hydrodynamic clutch arrangement. The intermediate transmission element accepts a mass element, located operatively between the two connecting devices.

A sensor for sensing bioacoustic energy includes a housing comprising an interfacing portion configured to establish coupling with a body part during use. The sensor includes a transducer element coupled to the interfacing portion of the housing and configured to sense sounds produced by matter of biological origin. One or more conductors are coupled to the transducer element. A mass element is compliantly coupled to a surface of the transducer element. Intervening material is disposed between the transducer element surface and the mass element, and allows for differential motion between the transducer element surface and the mass element during excitation of the transducer element.

A tuned mass damper comprising a frame, at least one bendable spring element being connected from its ends to the frame, and at least one mass element being connected to the spring element at a distance from the ends of the spring element, at least one movable spring support element for adjusting the tuning frequency of the damper, and means for moving the spring support element.

Disclosed herein are various embodiments of a golf club head having improved mass distribution characteristics. The golf club head includes a body and a face positioned at a forward portion of the body. The golf club head also includes one or more mass elements positioned at predetermined locations about the head. The mass elements assist in achieving desired relationship between the moment of inertia about a center of gravity x-axis and the moment of inertia about a center of gravity z-axis.

The invention provides a golf club head having adjustable weight, allowing the golfer to fine tune the club for his or her swing. The club head includes a body having a ball-striking face, a sole, a crown, and a side extending rearwardly from the face. The body defines an interior cavity and a recess on a selected wall of the body spaced apart from the striking face. A threaded opening is disposed in the recess. The club head further includes a weight assembly having fastener and a mass element configured to be press-fit into the recess the such that a first end is adjacent the bottom of the recess. The mass element also has an aperture configured to receive the fastener flush. The fastener removably attaches the weighting assembly to the selected wall of the club head. Pressure from the fastener attachment provides a press-fit of the mass element in the tapered recess of the selected wall.

A rotary electric machine, in particular an electric motor, has a winding, an electronic control device, and an electrically conductive shielding plate arranged between the control device and the winding. A connection device which includes at least one coupling element for electrically connecting the control device to one or more lines and a mass element provided for connecting to an electric mass potential. In order to improve the machine with respect to electromagnetic interference, the shielding plate is electrically conductively connected to the mass element by way of a sheet metal tongue via a first electric pressure-contact.

Disclosed herein is an inertial sensor, which includes a diaphragm having a piezoelectric element or a piezoresistive element formed on one surface thereof, a mass element integrated with the center of the other surface of the diaphragm in which the distal end of the mass element has a larger width than the width of the proximal end in contact with the diaphragm, and a supporter formed along the edge of the other surface of the diaphragm, so that the use of the mass element having the above shape results in decreased spring constant and increased distance from the center of the diaphragm to the center of the mass element, thereby simultaneously realizing a reduction in the size of the inertial sensor and an increase in performance thereof. A method of manufacturing the inertial sensor is also provided.

An improved vibrational energy harvester includes a housing and at least one energy transducer. In an embodiment, a second mass element is arranged to receive collisionally transferred kinetic energy from a first mass element when the housing is in an effective state of mechanical agitation, resulting in relative motion between the housing and at least one of the second and further mass elements. The energy transducer is arranged to be activated by the resulting relative motion between the housing and at least one of the second and further mass elements. In a further embodiment, kinetic energy is collisionally transferred in a velocity-multiplying arrangement from the first to a second or further mass element that has a range of linear ballistic motion. The energy transducer is arranged to be activated, at least in part, by the ballistic motion of the second or further mass element. The energy transducer, or a portion of it, may be attached to the housing, or it may be attached to another of the mass elements.

An acceleration sensor includes a substrate and a first mass element, which is connected to the substrate in such a way that the first mass element is rotatable about an axis, the first mass element being connected to a second mass element in such a way that the second mass element is movable along a first direction parallel to the axis, and the first mass element being connected to a third mass element in such a way that the third mass element is movable along a second direction perpendicular to the axis.

This invention pertains to a tire having a plurality of vibration absorbers wherein, (i) the vibration absorbers have at least one spring element and at least one absorber mass element, each element having a first and second surface such that the first surface of the spring element is attached to the tire carcass or attached to or embedded into the tire inner liner, and (ii) the first surface of the absorber mass element is attached to the second surface of the spring element, or the absorber mass element is embedded into the spring element.

A passive distributed vibration absorber that utilizes multiple discrete mass elements and a viscoelastic layer and that effectively attenuates vibration in modally dense structures excited by a broadband input noise excitation and is tunable to multiple natural frequencies in such modally dense vibrating structures including low frequencies

A torsional vibration damper, particularly for a drivetrain in a motor vehicle, having a substantially disk-shaped flywheel mass element having a friction surface for cooperating with friction facings of a friction clutch and a damper element arrangement communicating with the flywheel mass element, wherein the flywheel mass element is produced from a sheet metal material.

The invention relates to a biaxial differential capacitive micro-accelerometer, which belongs to the field of inertial sensors in a micro-electro-mechanical system. The micro-accelerometer comprises a sensitive mass element composed of a silicon sheet, four square movable electrodes arranged on the silicon sheet and insulating layers for isolating the movable electrodes, a substrate horizontally opposite to the silicon sheet, four square fixed electrodes arranged on the substrate and corresponding to the four square movable electrode, two lateral folding beams arranged on both ends of the silicon sheet for fixing the silicon sheet, two longitudinal folding beams for fixing the lateral folding beams, and pillars for fixing the two longitudinal folding beams on the substrate, so that the planes of the four movable electrodes are suspended and parallel to the substrate. The invention has the advantages of simple structure and high sensitivity, and can achieve high-accuracy two-dimensional acceleration measurement.

The torsional vibration damper acting between a drive and a housing of a hydrodynamic clutch arrangement includes a flywheel mass element, a drive-side damping element having a first side connected nonrotatably to the flywheel mass element, a takeoff-side damping element, the second side of the drive-side damping element being connected by elastic elements to the takeoff-side damping element for rotation in common, the elastic elements also allowing a small rotation of the drive-side damping element relative to the takeoff-side damping element, and an axially flexible drive plate. The takeoff-side damping element can be connected to the housing of the hydrodynamic clutch arrangement nonrotatably but with a certain freedom of axial movement by means of the drive plate.

The systems and methods described herein relate to, among other things, a transducer capable of producing acoustic and tactile stimulation. The transducer includes a rigid mass element disposed on the diaphragm of a speaker. The mass element may optionally be removable and may have a mass selected such that the resonant frequency of the transducer falls within the range of frequencies present in an input electrical audio signal. The systems and methods advantageously benefits from both the fidelity and audio performance of a full-range speaker while simultaneously producing high-fidelity, adjustable and palpable haptic vibrations.

A circuit module, in particular for use in a vehicle tire, having at least: a housing (2), a piezoelectric generator (3), which has a mass element (10) that is movable within the housing (2) and a spring device (12, 14), which has at least one piezoelectric element (14), the mass element (10) and the spring device (12, 14) forming an oscillatory system, and the piezoelectric element (14) being elastically deformable in response to the oscillation of the oscillatory system (10, 12, 14); and a current-supply circuit (5) for receiving a piezoelectric voltage output by the piezoelectric element (14) in response to the mechanical deformation thereof and for supplying power to the circuit module (1).

The invention relates to an apparatus and method for constructing a flywheel for energy storage, the flywheel having a drive transfer element (60) and a rim comprising a mass element (10), the drive transfer element being coupled to the rim by a winding (80) around each.

A shock simulation system including a support plane, a first mass element and a first spring element attached between the support plane and the first mass element. Also included, is a second mass element that is attached to the first mass element with a second spring element as well as a cocking apparatus, positioned between the support plane and the second mass element, that is capable of accumulating and storing energy in the spring elements. The system also includes a trigger for releasing the energy stored in the springs and for causing a mechanical shock event that is substantially transferred to the second mass.

A ring gyroscope which comprises a substantially circular and flexible ring which defines a ring plane, one or more primary piezoelectric split transducers configured to drive the ring into resonance oscillation, four or more mass elements which form a symmetrical mass distribution in relation to both a first and a second transversal symmetry axis and to a first and a second diagonal symmetry axis. The ring gyroscope also comprises a suspension structure configured to support the weight of the ring and the mass elements, wherein the suspension structure comprises N outer suspenders, where N is an integer greater than or equal to two, and each outer suspender extends along a ring tangent from a suspension attachment point on the outer edge of the ring to an anchor point.

The present invention relates to an acceleration sensor, especially to a triaxial acceleration sensor, which includes a substrate and a first mass element, which is connected to the substrate in sucha way that the first mass element is rotatable about an axis, the first mass element being connected to a second mass element in such a way that the second mass element is movable along a first direction parallel to the axis, and the first mass element being connected to a third mass element in such a way that the third mass element is movable along a second direction perpendicular to the axis.

The invention discloses a two-free endpoint dynamic vibration absorber, relating to the technical field of dynamic vibration absorber. The two-free endpoint dynamic vibration absorber comprises a spring (1), a damper (2) and an inertial mass energy accumulator (8); wherein the spring (1) is connected with the damper (2) in parallel and then is connected with the inertial mass energy accumulator (8) in series; the spring (1) is a helical compression one, and the damper (2) is a drum-type hydraulic one. The invention can be applied to the occasion that an endpoint can not be taken as a reference point and grounded and has wider application range compared with the traditional dynamic vibration absorber; the vibration absorber is provided with two free endpoints and can be placed horizontally, vertically and obliquely, vibration of master vibrator at any direction can be absorbed, thus being convenient to mount the vibration absorber; the inertial mass energy accumulator has the function of amplifying mass property, the weight thereof is far lighter than a mass element, thus greatly reducing the weight of large-scale dynamic vibration absorber.

The invention discloses a universal gravitation interference calculation method based on tetrahedral mass element division for a pure gravity rail, belonging to the technical field of astrodynamics and scientific computing. The method comprises the following steps of: firstly, selecting a tetrahedron as the shape of a mass element to divide a spacecraft and defining the following parameters: a scale parameter SR, a length / width ratio parameter AR, a force geometry factor FGP and a gradient geometry factor GGP; then calculating the FGP and the GGP under different values of the SR and the AR toobtain a curve for representing the influence of the scale and the shape of the tetrahedral mass element on the calculation accuracy; then determining the scale of the tetrahedral mass element according to the required calculation accuracy and the influence curve and dividing a model of the spacecraft through the tetrahedral mass element according to the scale of the mass element; and finally, calculating the universal gravitation. Through the method, the universal gravitation of the spacecraft to the quality verification according to the required accuracy can be calculated. Under a given accuracy, the corresponding requirement on the scale of the tetrahedral mass element can be obtained and the mass element is divided according to the requirement so that the calculation of the universal gravitation is finished and the required accuracy is met.

The disclosure relates to a microelectromechanical gyroscope comprising at least one mass element, a drive actuator and sense electrodes. The at least one mass element is configured to be driven by the drive actuator into oscillating movement with a drive oscillation frequency ωD, and the sense electrodes are configured to produce a sense signal from the oscillating movement of the at least one mass element. The gyroscope control circuit comprises an amplitude detection unit which detects a sense signal amplitude at the frequency 2ωD. This amplitude yields a measure of drive oscillation amplitude. Amplitude detection at the frequency ωD yields a measure of angular rotation rate.

The invention relates to a sensor element for pressure measurement, having a substrate (5) and at least one mass element (1), which is arranged spaced apart from the substrate (5) and is connected in an oscillating manner to the substrate (5) and / or a support body (6) fixed relative to the substrate (5), so that a gap is formed between the mass element (1) and the substrate (5), the width of which can be varied through oscillations of the mass element (1). At least one recess and / or at least one bushing (4) is located in the surface of the substrate (5) delimiting the gap, which recess is used for reducing the damping of the oscillation of the mass element through the gas or plasma surrounding the mass element (1). The sensor element is used in particular in pressure sensors for measuring pressures in the vacuum range. Through the use of the sensor element according to the invention as a pressure sensor, maximum pressures up to the range of atmospheric air pressure can be recorded. The lowest pressures to be determined are in the range of 10−6 mbar.