A system and method of analyzing duct pressure within a pipe monitors and detects vacuum pressure of gases. The system includes a pressure monitor and a target duct. The pressure monitor preferably includes an alarm light, a speaker, a sensing light, a service light, and a battery alert. The method begins by periodically capturing a plurality of pressure readings inside the target duct with the pressure monitor. Each pressure reading is timestamped with the pressure monitor. Each pressure reading is compared to each situational alert with the pressure monitor to identify at least one matching alert for at least one specific reading. The matching alert is from the plurality of situational alerts. The specific reading is from the plurality of pressure readings. The matching alert is visually and/or audibly outputted with the pressure monitor, if the matching alert is identified for the specific reading.

A connection socket for fluid-conducting line systems, and including a fluid channel extending along a fluid channel axis. The fluid channel may be connected to guide channels on at least a first and second connection ends of the connection socket. A measurement section is located between the first and second connection ends and a sensor system is provided therein to measure the pressure of a medium flowing within the fluid channel. The sensor system includes a connection interface for connecting to a control unit and measuring pressure in the fluid channel. For pressure measurement, at least two strain measurement sensors are arranged around the fluid channel axis on an outer wall of the measurement section. A control unit may be connected to the sensor system for measuring the pressure of a fluid in the connection socket.

A dynamic quantity sensor includes a first substrate and a second substrate. The first substrate has one surface, another surface opposite to the one surface, and a depressed portion defining a thin portion. The second substrate has one surface attached to the first substrate and a recessed portion disposed corresponding to the depressed portion. At least a part of a first projection line obtained by projecting the recessed portion is disposed outside of a second projection line obtained by projecting a boundary line between side walls of the depressed portion and the thin portion. The thin portion disposed inside the periphery of the recessed portion provides a film portion which is displaceable corresponding to a physical quantity applied to the film portion, and a region sandwiched between the film portion and a portion connected to the periphery of the recessed portion provides a stress release region.

In a sensor module for measuring a pressure of a fluid, having at least one supporting element, at least one electronic circuit, particularly an integrated circuit, arranged on at least one circuit carrier, and with at least one pressure measuring chip that has at least one pressure measuring membrane, wherein at least sections of the circuit carrier are surrounded by a protective material to protect it from surrounding fluids, it is provided as essential to the invention that the pressure measuring chip and the circuit carrier are arranged vertically one underneath the other, and that the pressure measuring chip is at least partially mechanically decoupled from the supporting element.

An inclination sensor for determining an angle of inclination relative to the gravitational vector comprising a fluid container and a first pressure sensor pair having a first and a second pressure sensor arranged in an edge region of the fluid container such that they are connected to each other by the connecting fluid and have a fixed and defined positional relation to each other. The first and the second pressure sensor are each configured to measure a hydrostatic pressure in the connecting fluid. A processor is configured to determine a relative height (h) in the direction of gravity between the first and the second pressure sensor based on the hydrostatic pressures measured, and to determine an angle of inclination with respect to the gravitational vector based on the determined relative height (h) and the known fixed locations of the pressure sensors within the fluid container.

The invention relates to a sensor device (10), in particular for use in a motor vehicle, comprising a housing (11) for receiving a sensor element (1), wherein the sensor element (1) has contact surfaces (21 to 23) that are electrically conductively connected with electrical plug connections (27) arranged in the housing (11), in the region of contacts (24 to 26), wherein the sensor element (1) is applied with force by a housing element (13), in particular formed as a housing cover, in the direction of the contacts (24 to 26) for the purposes of electrical contacting, and wherein a support in the form of a 3-point contact is formed between the sensor element (1) and the housing (11). According to the invention, the sensor element (1) has at least two measuring devices (5, 6), and the at least two measuring devices (5, 6) have three contact surfaces (21 to 23) that form the 3-point contact.

Disclosed is a pressure detecting device having a temperature sensor, the device including: a housing having a first chamber, a second chamber, and a port part having a fluid guide tube that guides a pressure transmitting fluid to the second chamber; a lead frame coupled to the housing and configured for being connected to an external device; a circuit substrate electrically connected to the lead frame and including a first surface and a second surface; a pressure detecting element provided on the second surface of the circuit substrate and generating an electrical signal according to a pressure change; a tube coupled to the port part, whereby a first end of the tube is open and provided inside the first chamber; and a temperature detecting element provided inside the tube and transmitting an electrical signal generated according to a temperature change to the circuit substrate.

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.

A receiver surge test tool (STT) assembly, system and method for receiver surge pressure testing. The receiver STT assembly has a receiver surge test tool (STT) configured to simulate surge pressure conditions of a receiver aircraft, and to measure one or more surge pressures generated when receiving a fuel flow of fuel from a refueling source during the receiver surge pressure testing that is ground based. The receiver STT has a pipe manifold structure with inlet port(s), outlet port(s), and one or more flow lines disposed therebetween. Each flow line includes a flow meter, a pressure transducer, a shutoff valve having varying valve close rates, and a manual back pressure valve. The receiver STT assembly has a control system for controlling open and close positions of the shutoff valve, and the receiver STT, and has a data system for collecting and recording data generated during the receiver surge pressure testing.

A Discrete Sample Introduction Module (DSIM) apparatus includes an internal tubing system to receive into the DSIM apparatus a discrete gas sample having a received concentration. A plurality of valves selectively partitions the internal tubing system to form a plurality of loops corresponding to a plurality of loop volumes to contain the discrete gas sample. The plurality of loop volumes receives a carrier gas to dilute the discrete gas sample to a plurality of preselected dilutions. The DSIM apparatus circulates a given one of the plurality of preselected dilutions for analysis by a spectrometer coupled to the DSIM apparatus.