Systems and methods for reducing vibrations perceived by a human due to an artificial heart valve include a vest that is wearable around a torso of the human, a plurality of sensors mounted to the vest, a plurality of vibration-generating actuators mounted to the vest, and a controller. The plurality of sensors detects vibrations in the human generated by the artificial heart valve. The controller is operable to receive signals representing the detected vibrations from the plurality of sensors, and is operable to produce anti-vibration signals that substantially attenuate the detected vibrations. A first sensor of the plurality of sensors is located near a first vibration-generating actuator of the plurality of vibration-generating actuators to form a sensor/actuator set. In the sensor/actuator set, the anti-vibration signals generated by the controller for the first vibration-generating actuator correspond to the vibrations detected by the first sensor.

Systems and methods for reducing vibrations perceived by a human due to an artificial heart valve include a vest that is wearable around a torso of the human, a plurality of sensors mounted to the vest, a plurality of vibration-generating actuators mounted to the vest, and a controller. The plurality of sensors detects vibrations in the human generated by the artificial heart valve. The controller is operable to receive signals representing the detected vibrations from the plurality of sensors, and is operable to produce anti-vibration signals that substantially attenuate the detected vibrations. A first sensor of the plurality of sensors is located near a first vibration-generating actuator of the plurality of vibration-generating actuators to form a sensor/actuator set. In the sensor/actuator set, the anti-vibration signals generated by the controller for the first vibration-generating actuator correspond to the vibrations detected by the first sensor.

A sensing module for configuring on a vibrating machine or structure, such as a pump or pump assembly is provided. The sensing module includes an outer shell configured with a recessed portion, and encapsulated electronics having a multicolored light array arranged inside the outer shell. The multicolored light array responds to signaling containing information about a condition being sensed or monitored by the sensing module and provides along a projection axis at least one beam of light containing information about the condition. The signaling is received from one or more of the other encapsulated electronics, including an accelerometer or temperature sensing device. The sensing module includes a domed lens configured in the recessed portion of the outer shell, and configured to project the at least one beam of light along the projection axis with a visibility of 360° for viewing from afar, by an observer visually monitoring the sensing module.

A sensing module for configuring on a vibrating machine or structure, such as a pump or pump assembly is provided. The sensing module includes an outer shell configured with a recessed portion, and encapsulated electronics having a multicolored light array arranged inside the outer shell. The multicolored light array responds to signaling containing information about a condition being sensed or monitored by the sensing module and provides along a projection axis at least one beam of light containing information about the condition. The signaling is received from one or more of the other encapsulated electronics, including an accelerometer or temperature sensing device. The sensing module includes a domed lens configured in the recessed portion of the outer shell, and configured to project the at least one beam of light along the projection axis with a visibility of 360° for viewing from afar, by an observer visually monitoring the sensing module.

A method for monitoring an aircraft engine vane wheel (22), which includes: acquiring at least one time signal relative to moments when the vane wheel blades (23) pass in front of a sensor (21); determining a common flight phase of the aircraft; for each flight in a series of flights of the aircraft, correlating at least part of each time signal with a predetermined flight phase; and for each blade (23), each flight, and each predetermined flight phase, measuring the mean position (24C), the so-called “balance position”, of the top of the blade. The invention also relates to a device for implementing such a method. One advantage of the invention is providing a diagnosis of the blades using a small number of sensors and low computing power.

An attachment monitoring system according to an embodiment includes a working machine, attachments, a measurement unit, a terminal device, and a server device. The working machine includes a working arm. Each of the attachments is attached to a leading end part of the working arm so as to be driven by a fluid pressure. The measurement unit is provided to measure at least one of a vibration and the fluid pressure when each of the attachments identified on the basis of individual identifying information is driven. The terminal device is provided in the working machine to acquire measured results of the measurement unit. The server device collects the measured results of the respective attachments from the terminal device, and analyzes operation states of the respective attachments on the basis of the collected measured results.

An attachment monitoring system according to an embodiment includes a working machine, attachments, a measurement unit, a terminal device, and a server device. The working machine includes a working arm. Each of the attachments is attached to a leading end part of the working arm so as to be driven by a fluid pressure. The measurement unit is provided to measure at least one of a vibration and the fluid pressure when each of the attachments identified on the basis of individual identifying information is driven. The terminal device is provided in the working machine to acquire measured results of the measurement unit. The server device collects the measured results of the respective attachments from the terminal device, and analyzes operation states of the respective attachments on the basis of the collected measured results.

A measurement method for early detection of damage to a blade of an impeller of a turbine is provided. During operation, in a rotational direction of the blade along a circumference which surrounds the impeller, at a plurality of points, in each case a plurality of magnetic fields are generated next to one another substantially in an oscillation direction of the blade, which magnetic fields are influenced by a tip of a turbine blade during transit. Positional values of the tip are detected by at the plurality of points. A positional profile of the turbine blade is then formed from the positional values and a frequency is determined from the positional profile. The frequency is compared with defined frequency values. An alarm event is recognized in case of a sudden and/or pronounced change in the frequency. In addition, a turbine is provided which is configured to carry out the method.

The present invention relates to a method for determining a value of at least one state parameter of a rail vehicle and/or of a track for a railway vehicle, wherein in at least one capturing step, at least one actual first capturing signal correlated with the actual value of the state parameter is captured, via a first signal sensor on a structure in the interior of the rail vehicle, wherein, for capturing the actual first capturing signal, a first signal sensor of a mobile end device is used. For determining the value of the at least one state parameter a frequency range of the first capturing signal actual above 1 Hz to 2 Hz, preferably 4 Hz to 15 kHz, more preferably from 10 Hz to 1 kHz, is evaluated.

The present invention relates to a method for determining a value of at least one state parameter of a rail vehicle and/or of a track for a railway vehicle, wherein in at least one capturing step, at least one actual first capturing signal correlated with the actual value of the state parameter is captured, via a first signal sensor on a structure in the interior of the rail vehicle, wherein, for capturing the actual first capturing signal, a first signal sensor of a mobile end device is used. For determining the value of the at least one state parameter a frequency range of the first capturing signal actual above 1 Hz to 2 Hz, preferably 4 Hz to 15 kHz, more preferably from 10 Hz to 1 kHz, is evaluated.