Abstract: A method for determining the set of focal laws of a plurality of focal points located in a test object includes the steps of providing a bidimensional array of transducer elements in a coupling medium and defining at least a scan line by a set of focal points. For each scan line, the method comprises performing the sub-steps of choosing a two preliminary focal points, calculating a first auxiliary time-of-flight corresponding to the time-of-flight of a wave emitted from the corresponding transducer element and received in the first preliminary focal point, and a second auxiliary time-of-flight corresponding to the time-of-flight of a wave emitted from the same transducer and received in the second preliminary focal point.

Abstract: A gas turbine engine includes a liner positioned within a compressor section or a turbine section of the gas turbine engine and at least partially defining a core air flowpath through the gas turbine engine. The gas turbine engine also includes a casing at least partially enclosing the liner. Additionally, the gas turbine engine includes a pressure sensor assembly having a body, an extension member, and a pressure sensor. The pressure sensor is positioned at least partially within the body and the body is positioned at least partially on an outer side of the casing, the extension member extending from the body through a casing opening in the casing and towards a liner opening in the liner. The extension member defines a continuous sense cavity exposing the pressure sensor to the core air flowpath.

Abstract: A gas turbine engine includes a liner positioned within a compressor section or a turbine section of the gas turbine engine and at least partially defining a core air flowpath through the gas turbine engine. The gas turbine engine also includes a casing at least partially enclosing the liner. Additionally, the gas turbine engine includes a pressure sensor assembly having a body, an extension member, and a pressure sensor. The pressure sensor is positioned at least partially within the body and the body is positioned at least partially on an outer side of the casing, the extension member extending from the body through a casing opening in the casing and towards a liner opening in the liner. The extension member defines a continuous sense cavity exposing the pressure sensor to the core air flowpath.

Abstract: The present patent application describes an approach to the protection of voltage sensitive instruments using a protection circuit that may be easily integrated in a three-terminal device, and which overcomes the drawbacks of previous approaches. The protection circuit of the invention performs very fast against overvoltages (in a few nanoseconds), automatically switching to a low impedance conduction state as soon as the overvoltage situation ends. It also minimizes insertion losses, shows a very low level of thermal noise and allows for obtaining broad bandwidths due to its low serial impedance in the conduction state. Furthermore, it does not require any power source or control signal.