Robotic platforms and methods of use are disclosed that include: at least one robot or robotic device, at least one computer-based control system, wherein the system is at least in part located on the at least one robot, at least one communications system, wherein the communications system is designed to communicate between the computer-based control system and the at least one robot, and at least one evaluation system that is designed to implement and process at least one nondestructive testing method.

The invention relates to an acoustic sensor system (1) for detecting a defect (2) of a pipeline wall (3), having: at least one transmitter unit (4) which is configured to emit ultrasound in the direction of a pipeline wall (3) and detect an ultrasound echo reflected by the pipeline wall (3); and a control unit (5) which is connected to the at least one transmitter unit (4) for signaling purposes and which is configured to detect a defect (2) of the pipeline wall (3) using a present change in he ultrasound echo. The invention additionally relates to an in-line inspection device comprising the sensor system (1), to a method for detecting a defect (2) in a pipeline wall (3), to a computer program, to a data carrier signal, and to a data storage unit.

A method for determining the prestress force of a connection component (10) is proposed. In the method, ultrasonic signals (22) are introduced into the connection component (10) and ultrasonic echoes (24) of the ultrasonic signals (22) are received again. The method comprises the following steps: a) introducing a longitudinal ultrasonic signal and determining a first signal time of flight FTOF.sub.L of the longitudinal ultrasonic signal until the reception of an echo of the longitudinal ultrasonic signal, b) introducing a transverse ultrasonic signal and determining a second signal time of flight FTOF.sub.T of the transverse ultrasonic signal until the reception of an echo of the transverse ultrasonic signal, and c) determining an effective temperature T.sub.eff and the prestress force of the connection component (10) on the basis of the first signal time of flight FTOF.sub.L, the second signal time of flight FTOF.sub.T, previously determined reference data and calibration factors using the assumption that a prestress force F.sub.L ascertained using the first signal time of flight FTOF.sub.L and a prestress force F.sub.T ascertained using the second signal time of flight FTOF.sub.T are equal in magnitude,
wherein steps a) and b) are carried out successively in any desired order or in parallel. A further aspect of the invention relates to a device for carrying out the method.

A method for determining the prestress force of a connection component (10) is proposed. In the method, ultrasonic signals (22) are introduced into the connection component (10) and ultrasonic echoes (24) of the ultrasonic signals (22) are received again. The method comprises the following steps: a) introducing a longitudinal ultrasonic signal and determining a first signal time of flight FTOF.sub.L of the longitudinal ultrasonic signal until the reception of an echo of the longitudinal ultrasonic signal, b) introducing a transverse ultrasonic signal and determining a second signal time of flight FTOF.sub.T of the transverse ultrasonic signal until the reception of an echo of the transverse ultrasonic signal, and c) determining an effective temperature T.sub.eff and the prestress force of the connection component (10) on the basis of the first signal time of flight FTOF.sub.L, the second signal time of flight FTOF.sub.T, previously determined reference data and calibration factors using the assumption that a prestress force F.sub.L ascertained using the first signal time of flight FTOF.sub.L and a prestress force F.sub.T ascertained using the second signal time of flight FTOF.sub.T are equal in magnitude,
wherein steps a) and b) are carried out successively in any desired order or in parallel. A further aspect of the invention relates to a device for carrying out the method.

The invention relates to an acoustic sensor system (1) for detecting the wall thickness (WT1, WT2) of a material layer (2) of a pipeline wall (3), having at least one transmitter unit (4), which is configured to emit ultrasound in the direction of a material layer (2) and detect an ultrasound echo reflected by the material layer (2), and a control unit (5), which is connected to the at least one transmitter unit (4) for signaling purposes and is configured to detect the wall thickness (WT1, WT2) of the material layer (2) using the ultrasound echo. The invention additionally relates to an in-line inspection device comprising the sensor system (1), to a method for detecting the wall thickness (WT1, WT2) of a material layer (2) of a pipeline wall (3), to a computer program, to a data carrier signal, and to a data storage unit.

The invention relates to an acoustic sensor system (1) for detecting the wall thickness (WT1, WT2) of a material layer (2) of a pipeline wall (3), having at least one transmitter unit (4), which is configured to emit ultrasound in the direction of a material layer (2) and detect an ultrasound echo reflected by the material layer (2), and a control unit (5), which is connected to the at least one transmitter unit (4) for signaling purposes and is configured to detect the wall thickness (WT1, WT2) of the material layer (2) using the ultrasound echo. The invention additionally relates to an in-line inspection device comprising the sensor system (1), to a method for detecting the wall thickness (WT1, WT2) of a material layer (2) of a pipeline wall (3), to a computer program, to a data carrier signal, and to a data storage unit.

A method for ultrasonic inspection of composite parts includes providing a composite part to be inspected with a plurality of layers, determining the runtime and/or attenuation of an ultrasonic signal propagating through the composite part to be inspected, providing the runtime and/or attenuation of the ultrasonic signal propagating through a reference composite part, subtracting the runtime and/or attenuation of the ultrasonic signal in the reference composite part from the runtime and/or attenuation of the ultrasonic signal in the composite part to be inspected, or vice versa, and determining from the result of the subtraction one or more missing and/or additional layers in the inspected composite part. The difference of the runtime and/or attenuation of the ultrasonic signal in the inspected composite part relative to the reference composite part, and/or the difference of the thickness between the composite part and the reference part, is/are visualized.

The invention relates to an ultrasonic method for estimating a nonlinear shear wave elasticity of a medium, the method comprising the following steps: A1. a first collection step in which a first set comprising one shear wave elasticity data point of the medium is collected at a first level of deformation applied to the medium, A2. a second collection step in which a second set comprising one shear wave elasticity data point of the medium is collected at a second level of deformation applied to the medium different to the first level, A3. a deformation estimation step in which the difference of deformation between the first and the second level of deformation is estimated, B1. a calculation step in which a gradient between at least two data points respectively belonging to the first and the second set is calculated as a function of the difference of deformation between the first and the second level of deformation, B2. an elasticity estimation step in which the nonlinear shear wave elasticity of the medium is estimated as a function of the gradient.

The invention relates to an ultrasonic method for estimating a nonlinear shear wave elasticity of a medium, the method comprising the following steps: A1. a first collection step in which a first set comprising one shear wave elasticity data point of the medium is collected at a first level of deformation applied to the medium, A2. a second collection step in which a second set comprising one shear wave elasticity data point of the medium is collected at a second level of deformation applied to the medium different to the first level, A3. a deformation estimation step in which the difference of deformation between the first and the second level of deformation is estimated, B1. a calculation step in which a gradient between at least two data points respectively belonging to the first and the second set is calculated as a function of the difference of deformation between the first and the second level of deformation, B2. an elasticity estimation step in which the nonlinear shear wave elasticity of the medium is estimated as a function of the gradient.

In some examples, a distributed acoustic detector system may include a frame structure and multiple acoustic detectors. The frame structure may be configured to be retained in a laser-based ophthalmo-logical surgical system aligned to an eye of a patient during therapeutic treatment of the eye of the patient with the laser-based ophthalmological surgical system. The acoustic detectors may be coupled to the frame structure and may be spaced apart from each other and electrically separated from each other.