A pressure monitoring device used to monitor for leaks in a tool such as a medical endoscope. The device includes a housing having an internal volume fluidically coupled with an internal volume of the tool to form a combined internal volume. A pump changes the pressure inside the combined internal volume thereby establishing a baseline pressure at a pressure differential from the ambient environment. During operation of the tool, the pressure inside the combined internal volume is monitored for a change exceeding a predefined limit and such a change results in the device issuing an alarm signal indicating a leak has occurred in the tool. The device housing can be directly mounted to the tool, located remotely and connected with a coupling hose, or integrated with an accessory device connected to the tool. Preferably, the pressure differential is negative relative to ambient when the tool is a medical endoscope.

A method of detecting leakage from a central detector unit 2 of an aspirating fire detection system 1 is described. The method includes actuating a valve 8 to block an outlet 8 of the detector unit 2, operating an aspirator 6 of the detector unit 2 at maximum power, and measuring a differential air pressure across the aspirator 6. If the resulting measured air pressure is below a predetermined threshold, it can be inferred that there is a leak within the central detector unit 2 downstream of the aspirator 6.

A method that includes coupling an external, removable fuel pressurization system to a fuel system of a vehicle. The fuel system of the vehicle is pressurized with the fuel pressurization system while the vehicle is parked and without activating a fuel consumer (e.g., an engine) of the vehicle. Decay of pressure of the fuel system is monitored following pressurization of the fuel system, and one or more of a leak, or a replaceable component, of the fuel system of the vehicle is detected based on at least in part on the decay of pressure that are monitored.

The present invention relates to a leak detection system for checking the leak-tightness of an object, the system including: a device for pressurising a space; a first pressure sensor configured to measure the variations in pressure of the pressurised space; a second pressure sensor configured to measure the variations in ambient pressure, such as atmospheric pressure; an electronic entity configured to determine a leak depending on the variations in the pressure ΔP in the pressurised space and the variations in the ambient pressure ϕP.sub.ext, the variations ΔP, ΔP.sub.ext being measured over a predetermined test time interval t.sub.test by the first and second sensors, respectively.

A leak detection device operable to measure fluid leaks in an element to be tested that is positioned in a first enclosure. In one example, a measuring module is positioned in a second enclosure and connected to the first enclosure and the element to be tested by an aeraulic connection. At least one of the first enclosure and the measuring module are thermally insulated using an insulating material.

The invention provides an apparatus and method for testing the integrity of a package, the apparatus comprising a first volume detecting means for detecting a first volume of the package at a first position; conveying means for moving the package from the first position to a second position downstream from the first position; compression means for providing a compression force on the package; a second volume detecting means for detecting a second volume of the package at the second position; determining means for determining the integrity of the package based upon a change in volume of the package; and rejecting means for removing packages, the integrity of which is determined by the determining means not to be intact, wherein the determining means is in electronic signal communication with each volume detecting means independently, wherein the determining means is in electronic signal communication with the rejecting means, wherein the compression means is located above a portion of the conveying means and wherein each volume detecting means independently comprises either two cameras for producing an image of the package or a single time of flight camera.

A method of assessing damage to a composite member requires the formation of a composite member comprising at least one cavity. A first pressure differential is then established between the cavity and the surrounding ambient pressure. The rate of change of the pressure differential over a first predetermined period is monitored and then the pressure differential is allowed to subside. The result of the monitoring step is stored as a reference value, so that after the composite member is damaged, or after it has been in service for a predetermined time, the test can be repeated and compared with the reference value. If the result of the repeated monitoring differs from the reference value by more than a predetermined amount, it is determined that the composite member is defective.

A leak check method includes: performing a first inspection of measuring a pressure in an internal space formed by a seal of the substrate holder, while evacuating the internal space, and detecting that the pressure reaches a first pressure threshold value within a predetermined first inspection time; performing a second inspection of closing the internal space that has been evacuated, measuring the pressure in the closed internal space, and detecting that the pressure in the closed internal space does not exceed a second pressure threshold value within a predetermined second inspection time; and performing a third inspection of measuring a pressure difference between the pressure in the closed internal space and a vacuum pressure in a master container, and detecting that an amount of increase in the pressure difference within a predetermined third inspection time is kept equal to or below a pressure difference threshold value.

A method that includes coupling an external, removable fuel pressurization system to a fuel system of a vehicle. The fuel system of the vehicle is pressurized with the fuel pressurization system while the vehicle is parked and without activating a fuel consumer (e.g., an engine) of the vehicle. Decay of pressure of the fuel system is monitored following pressurization of the fuel system, and one or more of a leak, or a replaceable component, of the fuel system of the vehicle is detected based on at least in part on the decay of pressure that are monitored.

A pressure sensor for an evaporated fuel leak detector is used for checking airtightness in a fuel tank and a canister. The pressure sensor includes a sensor unit, a case, and a sealing resin. The sensor unit has a pressure receiving portion, a plurality of conduction terminals, and a mold resin portion. The case has a fluid flow path and a housing recess. A buffer recess having an outer shape larger than the outer shape of a pressure receiving surface is formed at a pressure receiving side L1 of the bottom of the housing recess. Further, a protruding cylinder portion protruding into the buffer recess toward a back side L2 is formed at an outer edge of an opening end portion of the fluid flow path on the back side L2.