A measurement system for an aircraft gas turbine engine includes a probe and a heated-gas source in fluid communication with the pressure probe. The probe includes a probe body defining an internal cavity of the probe. The probe further includes a plurality of sensor inlet ports extending through the probe body and configured to receive a sensed fluid flow. The probe further includes a plurality of probe conduits. Each probe conduit of the plurality of probe conduits is coupled to a respective sensor inlet port of the plurality of sensor inlet ports and extending from the respective sensor inlet port to an exterior of the probe body. The heated-gas source is configured to supply a heated gas flow to one or both of: the plurality of sensor inlet ports via the plurality of probe conduits and an interior of the probe body outside of the plurality of probe conduits.

A measurement system for an aircraft gas turbine engine includes a probe and a heated-gas source in fluid communication with the pressure probe. The probe includes a probe body defining an internal cavity of the probe. The probe further includes a plurality of sensor inlet ports extending through the probe body and configured to receive a sensed fluid flow. The probe further includes a plurality of probe conduits. Each probe conduit of the plurality of probe conduits is coupled to a respective sensor inlet port of the plurality of sensor inlet ports and extending from the respective sensor inlet port to an exterior of the probe body. The heated-gas source is configured to supply a heated gas flow to one or both of: the plurality of sensor inlet ports via the plurality of probe conduits and an interior of the probe body outside of the plurality of probe conduits.

A temperature sensor assembly having a support tube defining an interior, a temperature sensor having a distal end and a proximal end located within the interior, and, a concentric ring surrounding at least a portion of the temperature sensor and the concentric ring is positioned between the temperature sensor and the support tube for holding the temperature sensor in the support tube.

A temperature sensor assembly having a support tube defining an interior, a temperature sensor having a distal end and a proximal end located within the interior, and, a concentric ring surrounding at least a portion of the temperature sensor and the concentric ring is positioned between the temperature sensor and the support tube for holding the temperature sensor in the support tube.

A cabin air state sensing system for a vehicle may include a divergence structure facilitating measurement of cabin air temperature and dust concentration in a cabin through suction of air using an air suction device and an operation method thereof.

A cabin air state sensing system for a vehicle may include a divergence structure facilitating measurement of cabin air temperature and dust concentration in a cabin through suction of air using an air suction device and an operation method thereof.

An apparatus for performing thermal testing of a memory device and a method of thermally testing the memory device. The apparatus includes a tester; an interface board disposed over the tester and configured to receive the semiconductor device and connect the semiconductor device to the tester; a shield disposed over the interface board and including a recess; a gas-supplying unit including a conduit extending through the shield and accessible to the recess; a temperature-sensing device disposed within the recess; and a controller configured to control and communicate with the tester, the gas-supplying unit and the temperature-sensing device.

A thermally isolated sensor associated with a gas turbine engine includes a sensor probe configured to measure a temperature of a fluid associated with the gas turbine engine, and a base to be coupled to the gas turbine engine. The thermally isolated sensor includes a leading projection coupled to the base that extends into the fluid. The leading projection is configured to be heated by a heat source associated with the gas turbine engine. The thermally isolated sensor includes a trailing projection coupled to the base that extends into the fluid. The trailing projection is downstream from the leading projection. The trailing projection includes an inlet, and the sensor probe is disposed within the inlet and thermally isolated from the leading projection.

Systems, methods, and computer-readable media are disclosed for a pulse switched high side driver for vehicle sensor. An example method may include switching a transistor of a vehicle circuit to connect a first resistor to a vehicle sensor for a first time period in which exhaust gas temperature values of the vehicle are within a first range of exhaust gas temperatures values. The example method may also include switching, by providing a pulse-width modulation (PWM) signal with an on signal value, the transistor to connect a second resistor to a vehicle sensor for a second period of time in which exhaust gas temperature values of the vehicle are within a second range of exhaust gas temperatures values that are greater than the first range of exhaust gas temperature values, wherein the second resistor and vehicle sensor are also included in the vehicle circuit, wherein the second resistor is in parallel with a first resistor and connected between the transistor and the vehicle sensor. The example method may also include switching, by providing a pulse-width modulation (PWM) signal with an off signal value, the transistor to disconnect the second resistor from the vehicle sensor for a third period of time, the third period of time being greater than the second period of time. The example method may also include reading, using an analog to digital converter (ADC) an output of the vehicle sensor during or after the first period of time.

Systems, methods, and computer-readable media are disclosed for a pulse switched high side driver for vehicle sensor. An example method may include switching a transistor of a vehicle circuit to connect a first resistor to a vehicle sensor for a first time period in which exhaust gas temperature values of the vehicle are within a first range of exhaust gas temperatures values. The example method may also include switching, by providing a pulse-width modulation (PWM) signal with an on signal value, the transistor to connect a second resistor to a vehicle sensor for a second period of time in which exhaust gas temperature values of the vehicle are within a second range of exhaust gas temperatures values that are greater than the first range of exhaust gas temperature values, wherein the second resistor and vehicle sensor are also included in the vehicle circuit, wherein the second resistor is in parallel with a first resistor and connected between the transistor and the vehicle sensor. The example method may also include switching, by providing a pulse-width modulation (PWM) signal with an off signal value, the transistor to disconnect the second resistor from the vehicle sensor for a third period of time, the third period of time being greater than the second period of time. The example method may also include reading, using an analog to digital converter (ADC) an output of the vehicle sensor during or after the first period of time.