A system for and a method of measuring ultrasonic wave velocities in a subterranean core specimen is provided. Ultrasonic wave velocities are measured from the side surfaces (faces) of a polygonal-shaped core specimen having at least ten sides or faces. Stress is introduced to the core specimen by hydraulic rams associated with each set of opposing sides. As stress is applied, ultrasonic waves are introduced to at least one side of the set of opposing sides and the wave transmitted through the core specimen is measured. Subsequently, the wave velocity for the ultrasonic wave can be calculated based on the measurements taken. Also, elastic properties associated with the core specimen can be calculated.

There is provided a method for measuring a contact force applied to each tube constituting a tube bundle disposed in a fluid from a vibration damping member by using a probe inserted into each tube. Characteristic data defining a relationship between a value measured by the probe and the contact force is previously prepared. Then, the probe is inserted into the tube, and the contact force is calculated using the measurement value of the probe, based on the characteristic data.

A method of measurement of the acting forces and/or the temperature in at least one region of a structure. The method includes an addition step in which at least one element is added to the structure, the addition generating a local vibration mode of the assembly formed by the structure and the added elements in each measurement region. The method also includes a step of analysis of the assembly, an excitation step of the assembly and a measurement step in which the variations produced in the resonance frequency of the assembly associated with the local vibration mode of each measurement region are measured. The method also includes a calculation step in which the acting forces and/or the temperature of the structure in the measurement region is determined based on the measured variation produced in the resonance frequency associated with the local vibration mode.

An ultrasonic tactile sensor for detecting a clamping force includes an ultrasonic detector and a sensing layer, and the sensing layer includes a first soft layer and a second soft layer, and the first soft layer has plural spherical microstructures arranged in contact with the ultrasonic detector, so that after a pressure is applied to the sensing layer, the ultrasonic detector generates an ultrasonic wave and receives a reflected wave signal, and the signal is provided for identifying the contact area of the spherical microstructures and deriving the force exerted on the tactile sensor.

A system for taking a measurement at a connection element. The system has a force sensor having a first side and a second side. The force sensor is configured to provide a measured value representative for a force acting between the first and the second side of the force sensor. The system also has an ultrasonic sensor and a positioning bushing The positioning bushing has a positioning bushing recess, which is configured to receive the ultrasonic sensor, at least in part. The system also has a separate sensor bushing, mechanically coupled to the first side of the force sensor, and having a sensor bushing recess. The sensor bushing recess is configured to receive, at least in part, the positioning bushing and the first end of the connection element. A second end of the connection element can be mechanically coupled to the second side of the force sensor.

A method for the ultrasonic double-wave measurement includes: obtaining a first mode wave time-of-flight and a second mode wave time-of-flight of an ultrasonic double-wave of a solid material at a first temperature and stress state; measuring a first mode wave time and a second mode wave time of the ultrasonic double-wave of the solid material in an unknown state; obtaining a first mode wave temperature influence coefficient and a second mode wave temperature influence coefficient of the solid material, and a first mode wave pre-tightening force influence coefficient and a second mode wave pre-tightening force influence coefficient in the solid material to be measured having the same specification and geometric shape; and obtaining a relative change relationship of ultrasonic double-wave time-of-flight according to the first-order or second-order Taylor approximation, and jointly solving to obtain a measured pre-tightening force and a measured temperature.

The present invention discloses an interface ultrasonic reflectivity-pressure relation curve establishment method and a loading testbed. The loading testbed comprises a force displayer, a control terminal, an oscilloscope, an immersion ultrasonic transducer, a large cylinder, a small cylinder, an upper panel, a movable plate, a force sensor, a lower panel, an ultrasonic transceiver and a small cylinder connecting plate. Compared with the existing schemes, the interface ultrasonic reflectivity-pressure relation curve establishment method and the loading testbed provided by the present invention can construct a more accurate ultrasonic reflectivity-pressure relation curve, and are high in detection precision

A compound sensor that is capable of being used with robotics is provided such that the compound sensor includes a distance measurement unit and a pressure measurement unit. Further, a contact detection unit, which is dedicated to performing a detection when a measurement target contacts with a surface of the sensor is included.

A method for measuring the applied load on a towing hook/or a tow bar accessory of a towing hook arrangement for a vehicle, and a towing hook arrangement for a vehicle. The towing hook arrangement comprises a towing hook and/or a tow bar accessory arranged on a tow bar, the towing hook arrangement also comprises a sensor arrangement having at least one actuator and at least one sensor, the sensor arrangement is adapted to detect an imparted vibration on the tow bar and use the detected imparted vibration to determine the applied load on the towing hook and/or the tow bar accessory.

A method for detecting residual stress induced by cold expansion (Cx) (Cx stress) at a hole in a structure. Two transducer pairs transmit and receive ultrasonic waves into the structure in a pitch-catch configuration along two first paths parallel to a tangent of the hole. The two paths are at different distances from the hole. Both transducer pairs are arranged such that their incident angle into the structure provides longitudinal critically refracted (LCR) waves within the structure. Time-of-flight (ToF) measurements of the LCR waves along the first path and the second path are the basis of acoustoelasticity calculations that determine if Cx stress is present at the hole.