An apparatus for ultrasonically inspecting a component of a gas turbine engine at a centre frequency required for ultrasonic inspection of the component. The apparatus comprises an ultrasonic transducer and a waveguide. The ultrasonic transducer and the waveguide are mounted in a holder, the holder is movably mounted in a carrier, and the carrier is movably mounted in a frame. The waveguide has a first end, a second end and a surface. The waveguide is circular in cross-section, the surface of the waveguide between the first end and the second end is concave, and the waveguide reduces in diameter from the first end to the second end. The length of the waveguide is equal to or greater than 0.5 times and equal to or less than 3 times the wavelength of an ultrasonic signal at the centre frequency required for the ultrasonic inspection.

Systems and methods of determining physical conditions of a battery, such as state of charge (SOC), state of health (SOH), quality of construction, defect, or failure state include driving two or more acoustic signals of two or more amplitudes, each acoustic signal having two or more frequencies, into the battery and detecting vibrations generated in the battery based on the two or more acoustic signals. Nonlinear response characteristics of the battery for the two or more acoustic signals are determined from the detected vibrations. The physical conditions of the battery are determined based at least in part on the nonlinear response characteristics, using nonlinear acoustic resonance spectroscopy (NARS) or nonlinear resonant ultrasound spectroscopy (NRUS).

The invention relates to non-destructive ultrasonic testing of flat-bottom rails, laid on track, and can be used for detection of defects in tips of the rail foot on aluminothermic welded joints, performed by the intermediate casting method. During the ultrasonic testing of aluminothermic welded joints, at least two zones for ultrasonic testing were determined with selecting one of at least two zones on the weld bead (reinforcing bead) from the lateral surface of the tip of the rail foot. At least two specific zones are grinded on the weld collar (reinforcing collar) with creation of at least two flat areas, which are able to ensure acoustic contact. The ultrasonic transducer is placed on every flat area of the collar, which is connected to at least one ultrasonic flaw detector. Ultrasonic testing of weld is performed using at least one flaw detector Delta-method or echo-method. As a result of the invention implementation, there is no any blind zone in the base of the rail welded joint. The described invention ensures higher accuracy in detection of welds defects within the tips of the rail foot area. 2 z.p. f-ly, 8 il.

Provide an inspection apparatus and an inspection method capable of quickly inspecting a situation of joining between members in a joined body. The inspection apparatus is an inspection apparatus inspecting a situation of joining between a plurality of members in a joined body including the members joined to and overlapped one another.

The invention relates to a system which provides a real time update on an estimated positioning of an ultrasonic which is having an ultrasonic generator placed near the inspection probe in the 3D surface, which generates an ultrasonic guided wave travelling along the surface of 3D component and includes positioning more than one ultrasonic receiver probes along the length of 3D component.

The present application provides systems and methods for measuring cell function or tissue function. More particularly, the present application provides systems and methods for determining cell or tissue contractility using ultrasound; systems and methods for measuring the effect an agent has on cell or tissue contractility using ultrasound; and systems and methods for determining material properties of a material using ultrasound.

According to one embodiment, an ultrasonic device includes an ultrasonic transmitter. The ultrasonic transmitter includes a first element, a second element, and a driver. The first element is flexing-vibratable at a first resonant frequency. The second element is flexing-vibratable at a second resonant frequency different from the first resonant frequency. The driver is configured to supply a first electrical signal to the first element and to supply a second electrical signal to the second element. The first electrical signal includes a first signal having the first resonant frequency. The second electrical signal includes a second signal having the second resonant frequency.

An apparatus which includes a mounting, a plurality of detection means provided to detect a condition of at least one parameter indicative of presence of one or more materials in a gutter channel and data processing means. A sequence of signals are transmitted and received when the apparatus is in a detection mode, and the data processing means analyses the received signals to provide an indication if a material is detected as being present in the channel and, if detected, a type of the material. On the basis of this analysis and identification of material, a decision can be made as to whether any remedial action is required to clear the material and/or decide upon an ongoing monitoring and maintenance schedule for the guttering.

Disclosed are a method and an apparatus for generating a tactile sensation. The method of generating the tactile sensation according to an embodiment of the present disclosure may include: determining a tactile sensation information; generating wave signals associated with each tactile sensation information; generating ultrasonic driving signals in which phases and output timings of the wave signals are adjusted based on frequencies and a number of the wave signals; and generating the tactile sensation associated with the ultrasonic driving signals.

An acoustic sensor system for an aircraft, and method for operating the same, includes a transmitter, at least one microphone, and a control circuit. The transmitter is configured to emit acoustic signals external to the aircraft. The at least one microphone is positioned on an exterior of the aircraft and configured to sense the acoustic signals as sensed data. The control circuit is configured to receive the sensed data and control the transmitter through a drive circuit, and is configured to detect an environmental condition and control the transmitter to emit the acoustic signals at a reduced intensity based on the detected environmental condition.