A hydrocarbon generation pyrolysis simulation experimental device for centrifugal continuous gas sampling of a hydrocarbon source rock, including a centrifugal turntable, a motor, a quartz sample tube, a heating set, a cooling set, a rotary joint mounted coaxially with a rotating shaft of the centrifugal turntable, a vacuum pump, and vacuum gas collecting pipes, wherein a sealing plug is arranged at an orifice of the quartz sample tube, a thermocouple and a first exhaust pipeline connected with an inlet of the rotary joint are mounted on the sealing plug, the rotary joint is communicated with a vacuum pump through a second exhaust pipeline, a plurality of vacuum gas collecting pipes are respectively communicated with the second exhaust pipeline through an electromagnetic valve, a vacuum pump switching valve is mounted on the second exhaust pipeline at an inlet end of the vacuum pump, and a control circuit board is mounted on the centrifugal turntable.

A catalyst for a gas sensor includes a support and a core-shell type complex contained in the support. The complex includes a metal-containing core and a porous nanostructured shell. A contact combustion type gas sensor includes the catalyst.

A catalyst for a gas sensor includes a support and a core-shell type complex contained in the support. The complex includes a metal-containing core and a porous nanostructured shell. A contact combustion type gas sensor includes the catalyst.

A heat tone sensor includes a housing with a gas inlet and with a gas outlet as well as a device for generating a gas stream of a gas to be tested between the gas inlet and the gas outlet. A measuring element, around and/or through which the gas stream flows, is configured to catalytically burn at least a portion of the gas stream and to send a measurement signal. The measurement signal indicates a quantity of heat released in the process.

Systems, methods, devices, and circuitries are provided for determining a material property. In one embodiment, a measurement device includes analysis circuitry and indicia circuitry. The analysis circuitry is configured to determine a sample thermal property value of a material sample; determine an environmental characteristic value; identify a range of environmental characteristic values mapped to the sample thermal property value; determine a suitability result corresponding to a suitability of the material sample to the environmental characteristic value based on whether the environmental characteristic value falls within the identified range of environmental characteristic values. The indicia circuitry is configured to communicate the suitability result.

Systems, methods, devices, and circuitries are provided for determining a material property. In one embodiment, a measurement device includes analysis circuitry and indicia circuitry. The analysis circuitry is configured to determine a sample thermal property value of a material sample; determine an environmental characteristic value; identify a range of environmental characteristic values mapped to the sample thermal property value; determine a suitability result corresponding to a suitability of the material sample to the environmental characteristic value based on whether the environmental characteristic value falls within the identified range of environmental characteristic values. The indicia circuitry is configured to communicate the suitability result.

A method of checking refuelling of an aircraft comprising a gas turbine engine and a fuel tank arranged to provide fuel to the gas turbine engine comprises: receiving an input of calorific value data for fuel provided to the aircraft on refuelling; independently determining at least one of: (i) the calorific value of fuel supplied to the gas turbine engine in use; and (ii) the calorific value of the fuel provided to the aircraft on refuelling; and providing an alert if the determined calorific value is inconsistent with the calorific value data input received

A method of checking refuelling of an aircraft comprising a gas turbine engine and a fuel tank arranged to provide fuel to the gas turbine engine comprises: receiving an input of calorific value data for fuel provided to the aircraft on refuelling; independently determining at least one of: (i) the calorific value of fuel supplied to the gas turbine engine in use; and (ii) the calorific value of the fuel provided to the aircraft on refuelling; and providing an alert if the determined calorific value is inconsistent with the calorific value data input received

A gas measuring device includes: a filter to which a power supply that applies a voltage or current is connected, which generates resistance heat, and which combusts a predetermined combustible gas in contact therewith; and a gas sensor configured to detect the combustible gas that has passed through the filter.

A gas measuring device includes: a filter to which a power supply that applies a voltage or current is connected, which generates resistance heat, and which combusts a predetermined combustible gas in contact therewith; and a gas sensor configured to detect the combustible gas that has passed through the filter.