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.

The invention relates to an adapter part (9) for connecting a medical hollow body (11) to a tension/compression measuring device (3), comprising a first connecting end (13), which is designed to connect the adapter part (9) to an interior (15) of a medical hollow body (11) in a fluid-tight manner, and comprising a second connecting end (17), which has a pressure chamber (19) and is designed to operatively connect the adapter part (9) to a tension/compression measuring device (3), so that a pressure in the pressure chamber (19) can be adjusted by means of the tension/compression measuring device (3), a hollow channel (21) passing through the adapter part (9) from the pressure chamber (19) to the first connecting end (13).

The outer housing for a pressure monitoring system includes a sidewall shell comprising an annular inner sidewall projection extending from a top end thereof; a cap mounted to the sidewall shell, the cap defining an inner cap surface, an outer cap surface, a cap bottom end, and an annular cap recess extending into the cap bottom end between the outer cap surface and the inner cap surface, wherein the annular inner sidewall projection is configured to engage the annular cap recess; and an antenna assembly directly mounted to the inner cap surface, the antenna assembly comprising an antenna.

A method of fabricating a conduit comprises steps of attaching a first tubular-outboard-ply-end of a tubular outboard ply to a first inner collar portion of a first collar with a second weld and attaching a second tubular-outboard-ply end of the tubular outboard ply to a second inner collar portion of a second collar with a fourth weld. The method also comprises steps of inserting a tubular inboard ply into the tubular outboard ply, threadably interconnecting the first inner collar portion and a first outer collar portion of the first collar, and threadably interconnecting the second inner collar portion and a second outer collar portion of the second collar. The method further comprises steps of attaching a corrugated inboard ply to the first outer collar portion with a first weld and attaching a corrugated inboard ply to the second outer collar portion with a third weld.

A piston ring is used for a reciprocating compressor. In the piston ring, polytetrafluoroethylene and polyetheretherketone or polyimide account for 50% or more by mass in total. The piston ring does not contain polyphenylene sulfide. The piston ring has a tensile strength within a range of more than 15 MPa and less than 100 MPa.

A blowby gas treatment device includes a pressure control valve, a fresh air induction pipe, a first blowby gas pipe, a second blowby gas pipe, a shutoff valve, a one-way valve, and a PCV valve. A leak diagnosis includes a first-stage diagnosis to determine whether or not falling of a pressure in a crank case after closing of the shutoff valve under a non-supercharging condition is normal. A second-stage diagnosis is implemented by using an air fuel ratio feedback control, and determining whether or not a sensed intake air quantity obtained by an air flow meter is equal to an actual intake air quantity flowing into a cylinder set. When the sensed intake air quantity is equal to the actual intake air quantity, presence of an in-system leak is determined, and when the actual intake air quantity is larger, presence of an out-of-system leak is determined.

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.

There is described a testing apparatus (20) for testing the integrity of a tank (12). The apparatus comprises a control tube (22) configured to be at least partially submerged within the tank (12). The control tube (22) being controlled to open and close to permit the ingress and capture of fuel into the control tube (22) from the tank (12). A first gas tube (29) is connectable to a remote gas source (40) and is configured to deliver gas to an outer surface of the control tube (22) at a predetermined location. A second gas tube (29) is connectable to the remote gas source (40) and configured to deliver gas to an inner surface of the control tube (22) at a predetermined location. A metering unit (30) is in fluid communication with the first gas tube (29) and the second gas tube (29) and having one or more pressure sensors (32) for measuring fuel mass inside the control tube (22) and fuel mass outside the control tube (22) and for comparing the two measurements to determine a change in fuel mass outside the control tube (22). The change in fuel mass outside the control tube (22) being indicative of a loss of integrity of the tank (12).

A flaw detection system may include a dedicated monitor volume within a structural component of a system. The monitor volume may establish an air tight space bounded by at least one joint where the joint establishes a portion of a boundary of the air tight space and is in fluid communication with the air tight space. The system may also include a pressure sensing device configured for sensing the pressure in the dedicated monitor volume. A method of monitoring a system for flaw development may include monitoring a pressure sensor configured to sense the pressure in a dedicated monitor volume of a structural component of a system. The method may also include inspecting the structural component to identify a flaw location when the pressure sensor identifies a change in pressure in the dedicated monitor volume.

In an evaporative fuel treatment device, a differential pressure specifying unit specifies a differential pressure between a pressure in a diagnosis target system and the atmosphere, and a pressure target setting unit sets a pressure target value so that the differential pressure attains a predetermined differential pressure value. A pump pressurizes or depressurizes the pressure in the diagnosis target system to the pressure target value, and a leakage diagnosis unit performs a leakage diagnosis based on a pressure change relation value related to the pressure change in the diagnosis target system and the leakage diagnosis threshold value. The fuel partial pressure estimation unit estimates a first partial pressure of fuel vapor in the fuel tank from a tank inside concentration and a tank absolute pressure of a specific component. A corresponding partial pressure specifying unit specifies a second partial pressure of the fuel vapor in the fuel tank based on a relation between the tank absolute pressure and the first partial pressure when the second partial pressure of the fuel vapor in the fuel tank when the pressure is increased or reduced to the target pressure value. A comparison unit compares the first partial pressure and the second partial pressure. A correction unit corrects, based on a comparison result of the comparison unit, a leakage diagnosis threshold value or the pressure change relation value used for the leakage diagnosis.