The present invention relates to a differential pressure sensor for a leak detection device comprising: at least two bodies in which a cavity is created; a membrane that is arranged between the two bodies and separates said cavity so as to define a test chamber in each one of said bodies; at least one electrode arranged in each one of the test chambers and facing said membrane so as to form therewith a capacitor;
characterised in that said sensor comprises at least two seals arranged between each of said bodies and the membrane.

Pressure sensor systems that include a pressure sensor die and other components in a small, space-efficient package, where the package allow gas or liquid to reach either or both sides of a membranes of the pressure sensor die. A package can include a substrate and a cap, where either or both the substrate and the cap divide the package internally into two chambers. The substrate can have a solid bottom layer, a middle layer having a slot or path running a portion of the length of the layer, and a top layer having two through-holes that provide access to the slot or path. The cap can have two ports. A first port can lead to a first chamber where a top side of a pressure sensor is in the first chamber. A second port can lead to a second chamber and the slot or path, where the slot or path leads to a bottom side of the pressure sensor.

A method of predicting a lifetime of a gas filling of an electrical switchgear is disclosed, wherein pressure values p.sub.1, p.sub.2 in a system of the electrical switchgear containing the gas filling at a predefined temperature T.sub.p at different points in time t.sub.1, t.sub.2 are measured. Based on the pressure difference Δp between the pressure values p.sub.1, p.sub.2 the lifetime of the gas filling is calculated. Alternatively, the pressure values p.sub.1, p.sub.2 can be taken at temperatures T.sub.1, T.sub.2 within a predefined temperature range at different points in time t.sub.1, t.sub.2.

A pressure sensor includes a cylindrical case defining an inner space in communication with an outer space; a pressure detector provided in the inner space and configured to detect a gauge pressure of a target fluid; an atmospheric pressure detector configured to detect an atmospheric pressure; and an electronic component configured to calculate an absolute pressure of the target fluid on a basis of the gauge pressure and the atmospheric pressure. The absolute pressure is obtained without requiring airtightness of the case between the inner space and the outer space, and thus, there is no requirement for a seal member to be included between the inner space and the outer space.

A micromechanical component for a pressure and inertial sensor device. The component includes a substrate having an upper substrate surface; a diaphragm having an inner diaphragm side oriented towards the upper substrate surface and an outer diaphragm side pointing away from the upper substrate surface, the inner diaphragm side bordering on an inner volume, in which a reference pressure is enclosed, and the diaphragm being able to be warped using a pressure difference between a pressure prevailing on its outer diaphragm side and the reference pressure; and a seismic mass situated in the inner volume, a sensor electrode, which projects out on the inner diaphragm side and extends into the inner volume, being displaceable with respect to the substrate due to a warping of the diaphragm. A pressure and inertial sensor device, and a method of manufacturing a micromechanical component for a pressure and inertial sensor device, are also described.

A spiral wound membrane module including a specialized endcap assembly including a connecting conduit defining a passageway extending radially inward from its outer periphery, and a differential pressure sensor connected to the passageway of the connecting conduit.

A pressure sensor chip includes a base, a first layer including a first cavity and joined to an upper surface of the base, a second layer joined to an upper surface of the first layer, a third layer including a second cavity and joined to an upper surface of the second layer, and a fourth layer including a third cavity and joined to an upper surface of the third layer. The second layer includes a first diaphragm between the first and second cavities. The fourth layer includes a second diaphragm between the second cavity and a space in communication with outside. A top end of the third cavity is in communication with outside. The bottom end of the third cavity is in communication with the second cavity. The first cavity is sealed. The pressure in the first cavity is lower than the pressure in the second cavity.

The present disclosure relates to differential pressure transducers. The teachings thereof may be embodied in diaphragm-beam configurations for measuring small values of differential pressure and/or a bridge circuit for converting mechanical strains into an electric output signal. For example, a diaphragm-beam structure for measuring differential pressure may include: a frame; a paddle; a resilient beam member; a diaphragm; and a gap defined between the paddle and the frame. The diaphragm flexes under pressure on one surface. The resilient beam member anchors the paddle to the frame. The second surface of the diaphragm is mounted to the first surface of the paddle and the frame to bridge the gap. The paddle moves due to flexure of the diaphragm. The resilient beam member bends due to movement of the paddle. The thickness of the diaphragm is less than 50 micrometers.

A pressure sensor die assembly for a differential pressure sensor comprises a base substrate including a first overpressure stop structure on a first surface, and a diaphragm structure coupled to the first surface. The diaphragm structure comprises a first side with a cavity section that includes a first cavity and a second cavity surrounding the first cavity, and a second side opposite from the first side. A pressure sensing diaphragm portion is defined by the first cavity and is located over the first overpressure stop structure. An overpressure diaphragm portion is defined by the second cavity. A top cap coupled to the second side of the diaphragm structure includes a second overpressure stop structure. The overpressure stop structures are each sized to support substantially all of a strained area of the pressure sensing diaphragm portion at an increasing overpressure on the first or second sides of the diaphragm structure.

An air pressure sensing system including a first sensing unit and a second sensing unit is provided. The first sensing unit includes a substrate, a diaphragm, and a supporting member. The substrate has a cavity connected with an exterior environment. The diaphragm is movably and deformably disposed at the substrate and suspended in the cavity. An electrostatic force is provided to the substrate and the diaphragm to move the diaphragm, such that a portion of the base, the supporting member and the diaphragm are contacted with each other and a closed space is formed therebetween in the cavity. The closed space and the exterior environment are divided by the diaphragm, and the diaphragm is deformed due to an air pressure difference between the closed space and the exterior environment. An air pressure sensing method is also provided.