Disclosed herein is a wind measuring system including a first flow sensor and plural second flow sensors. The first flow sensor and the plural second flow sensors each include a microheater including a board, an insulating film, and a heater. The board includes a first principal surface and a second principal surface. The board has defined therein an opening portion passing through the board along a direction from the first principal surface toward the second principal surface. The insulating film includes a peripheral portion disposed on the first principal surface, a central portion having the heater disposed thereon, and a connection portion extending from the central portion to be connected to the peripheral portion to support the central portion over the opening portion. The first flow sensor and the plural second flow sensors each output a signal that varies according to a change in electrical resistance value of the heater.

Disclosed is a device for measurement of a flow speed of a gas comprises a probe, a voltage supply source and a pulse-counting detection circuit. The probe comprises an axial electrode whose exposed end has a small radius of curvature, and a peripheral electrode. The supply source applies an alternating voltage between both electrodes, and electrical discharges which are produced through the gas between the two electrodes are detected and counted by the detection circuit. Such a speed measurement device is particularly reliable, and suited for use on board an aircraft for measuring the speed thereof relative to the surrounding air.

Disclosed is a device for measurement of a flow speed of a gas comprises a probe, a voltage supply source and a pulse-counting detection circuit. The probe comprises an axial electrode whose exposed end has a small radius of curvature, and a peripheral electrode. The supply source applies an alternating voltage between both electrodes, and electrical discharges which are produced through the gas between the two electrodes are detected and counted by the detection circuit. Such a speed measurement device is particularly reliable, and suited for use on board an aircraft for measuring the speed thereof relative to the surrounding air.

An electromagnetic speedometer for a boat having hull containing an opening includes an electromagnetic coil supported by the hull for establishing an electromagnetic field in the water adjacent the hull opening. A plurality of electrodes are supported by an arrangement that both closes the hull opening and supports the electrodes in engagement with the water adjacent the hull opening. The electrodes are connected by conductors with a velocity measuring circuit arranged above the hull interior surface. Preferably, the electrode support arrangement includes guide tubes supporting the electrodes for removal relative to the boat hull, thereby to permit cleaning of the electrodes. The guide tubes are closed by valves when the electrodes are removed from the assembly. In one embodiment, the electromagnetic coil is of the end-fired type, and in another embodiment, the electromagnetic coil is annular and is arranged above and below the hull.

An electromagnetic speedometer for a boat having hull containing an opening includes an electromagnetic coil supported by the hull for establishing an electromagnetic field in the water adjacent the hull opening. A plurality of electrodes are supported by an arrangement that both closes the hull opening and supports the electrodes in engagement with the water adjacent the hull opening. The electrodes are connected by conductors with a velocity measuring circuit arranged above the hull interior surface. Preferably, the electrode support arrangement includes guide tubes supporting the electrodes for removal relative to the boat hull, thereby to permit cleaning of the electrodes. The guide tubes are closed by valves when the electrodes are removed from the assembly. In one embodiment, the electromagnetic coil is of the end-fired type, and in another embodiment, the electromagnetic coil is annular and is arranged above and below the hull.

A measurement apparatus comprising: a plurality of first electrodes, each of the first electrodes being spaced apart by at least a first predetermined spacing; a plurality of second electrodes, each of the second electrodes being spaced apart by at least a second predetermined spacing less than the first predetermined spacing; an energisation source arranged to energise at least one of said first electrodes so as to cause an electric field to be established between at least one pair of said first electrodes, and to energise at least one of said second electrodes so as to cause an electric field to be established between at least one pair of said second electrodes; a monitor arranged to monitor an electrical parameter at at least one of said first electrodes in response to said energisation of at least one of said first electrodes and to monitor an electrical parameter at at least one of said second electrodes in response to said energisation of at least one of said second electrodes; and a controller arranged to generate data indicative of a property of a material within a first region extending a first distance from the first electrodes, and to generate data indicative of a property of a material within a second region extending a second distance, less than the first distance, from the second electrodes, based upon said monitored electrical parameters.

A measurement apparatus comprising: a plurality of first electrodes, each of the first electrodes being spaced apart by at least a first predetermined spacing; a plurality of second electrodes, each of the second electrodes being spaced apart by at least a second predetermined spacing less than the first predetermined spacing; an energisation source arranged to energise at least one of said first electrodes so as to cause an electric field to be established between at least one pair of said first electrodes, and to energise at least one of said second electrodes so as to cause an electric field to be established between at least one pair of said second electrodes; a monitor arranged to monitor an electrical parameter at at least one of said first electrodes in response to said energisation of at least one of said first electrodes and to monitor an electrical parameter at at least one of said second electrodes in response to said energisation of at least one of said second electrodes; and a controller arranged to generate data indicative of a property of a material within a first region extending a first distance from the first electrodes, and to generate data indicative of a property of a material within a second region extending a second distance, less than the first distance, from the second electrodes, based upon said monitored electrical parameters.

The present disclosure discloses a multi-droplet sensing and actuation system, for use in a digital microfluidic chip operation wherein a linearly independent alternating current signal is applied to each discrete actuation electrode thus encoding the electrode's identity. The combined measured impedance signal from multiple channels is then processed to decode an impedance measurement for the volume between each discrete actuation electrode and its corresponding conductive counter electrode region, where the sensed impedance is inversely proportional to an amount of liquid within the volume.

The present disclosure discloses a multi-droplet sensing and actuation system, for use in a digital microfluidic chip operation wherein a linearly independent alternating current signal is applied to each discrete actuation electrode thus encoding the electrode's identity. The combined measured impedance signal from multiple channels is then processed to decode an impedance measurement for the volume between each discrete actuation electrode and its corresponding conductive counter electrode region, where the sensed impedance is inversely proportional to an amount of liquid within the volume.

A triboelectric nanogenerator with slit effect (SE-TENG) and a self-driven wind speed and wind direction sensing device are provided. The TENG includes a wind cavity with slit effect, a triboelectric layer, a hydroxyethyl cellulose (HEC) film, and indium tin oxide (ITO) electrodes. The wind cavity is provided with an inlet end and an outlet end. A layer of the electrode and a triboelectric layer are fixedly adhered to the upper surface and the lower surface of an inner wall of the wind cavity. The wind cavity is provided with a horizontally arranged support bar perpendicular to a wind direction in a middle close to the inlet end. The HEC film includes one end fixedly adhered to the support bar, and the other end extending freely toward the outlet end. The sensing device includes a plurality of SE-TENGs which is fixed on a circumference of a ring.