A sufficient sealing property of a through hole is ensured. A sealing structure includes a cylindrically-shaped body part inserted into the through hole, formed of a thin plate of a first thickness, one end of the body part being open and another end of the body part being closed, a tapered part connected to the opened one end of the body part and including a diameter gradually expanding outward as a distance from the body part increases, and a first bent part connected to the tapered part, formed of a thin plate thinner than the first thickness, and bent inward so that a protruding part protruding outward elastically abuts against an inner peripheral surface of the through hole.

A sufficient sealing property of a through hole is ensured. A sealing structure includes a cylindrically-shaped body part inserted into the through hole, formed of a thin plate of a first thickness, one end of the body part being open and another end of the body part being closed, a tapered part connected to the opened one end of the body part and including a diameter gradually expanding outward as a distance from the body part increases, and a first bent part connected to the tapered part, formed of a thin plate thinner than the first thickness, and bent inward so that a protruding part protruding outward elastically abuts against an inner peripheral surface of the through hole.

A system to provide at least two circumferential metal to metal seals between coaxial tubulars. Where a first tubular includes a circumferential shoulder having a circumferential first metal seal and a circumferential second metal seal. A second tubular has a circumferential shoulder that matches and abuts the first tubular circumferential shoulder. Each metal seal is of a material having a higher yield strength than the second tubular shoulder such that the first metal seal and the second metal seal will penetrate the material of the second tubular shoulder thereby providing a seal. Additionally a test port is provided from the exterior of the exterior tubular to a point on either the first or second tubular between the first and second metal seals.

A system to provide at least two circumferential metal to metal seals between coaxial tubulars. Where a first tubular includes a circumferential shoulder having a circumferential first metal seal and a circumferential second metal seal. A second tubular has a circumferential shoulder that matches and abuts the first tubular circumferential shoulder. Each metal seal is of a material having a higher yield strength than the second tubular shoulder such that the first metal seal and the second metal seal will penetrate the material of the second tubular shoulder thereby providing a seal. Additionally a test port is provided from the exterior of the exterior tubular to a point on either the first or second tubular between the first and second metal seals.

A seal to prevent fluid transfer using double diameters to provide a tighter seal is disclosed. The double diameter seal has a body with a first diameter containing an upper contact area and a second diameter forming a lower contact point. A notch extends into the body between the upper contact area and the lower contact point for a predetermined distance to form a transition point. In use, the first diameter is dimensioned to place a portion of the length of the upper contact area in sliding engagement adjacent to a length of the first surface. The second diameter dimensioned to place the lower contact point contacting an angled second surface of a valve.

The aim of the invention is to propose an edging method that is quick, effective, easy to implement and makes it possible to obtain a lightweight panel. To this end, the aim of the invention is a method for sealingly edging a composite panel comprising; *a step (a) of providing a composite panel of redefined thickness having two planar faces and a side to be edged, and of providing a sealing strip made from a polymer material having a width greater than the thickness of the composite panel, and comprising a first face, referred to as the “inner” face, and a second face, referred to as the “outer” face, in reference to the position of use of same: *a step (b) of applying the strip and an adhesive to the side and to a peripheral portion of the planar faces of the composite panel in such a way that the adhesive is located between the composite panel and the inner face of the strip, which sealingly protects the composite panel against dust, foreign bodies and the absorption of moisture.

The aim of the invention is to propose an edging method that is quick, effective, easy to implement and makes it possible to obtain a lightweight panel. To this end, the aim of the invention is a method for sealingly edging a composite panel comprising; *a step (a) of providing a composite panel of redefined thickness having two planar faces and a side to be edged, and of providing a sealing strip made from a polymer material having a width greater than the thickness of the composite panel, and comprising a first face, referred to as the “inner” face, and a second face, referred to as the “outer” face, in reference to the position of use of same: *a step (b) of applying the strip and an adhesive to the side and to a peripheral portion of the planar faces of the composite panel in such a way that the adhesive is located between the composite panel and the inner face of the strip, which sealingly protects the composite panel against dust, foreign bodies and the absorption of moisture.

A liquid-tight strain relief includes a tubular-shaped bushing and a dome-shaped gland. The bushing includes a flange, a centrally-located aperture, a plurality of resilient outer fingers, and a plurality of resilient inner fingers extending from an inner wall into the aperture. The gland includes a head having a centrally-located membrane. The head is co-molded with and encapsulates the flange, resulting in a strain relief having a unitary construction. The strain relief is adapted to be inserted within an orifice of a work piece, and the outer fingers frictionally engage the work piece. A cable is inserted within the strain relief by piercing the membrane, which stretches and provides a seal against the cable. The cable is inserted through the aperture of the bushing and the resilient inner fingers flex outwardly to enable the cable to pass through, while engaging and digging into the cable to clasp it and provide strain relief.

A liquid-tight strain relief includes a tubular-shaped bushing and a dome-shaped gland. The bushing includes a flange, a centrally-located aperture, a plurality of resilient outer fingers, and a plurality of resilient inner fingers extending from an inner wall into the aperture. The gland includes a head having a centrally-located membrane. The head is co-molded with and encapsulates the flange, resulting in a strain relief having a unitary construction. The strain relief is adapted to be inserted within an orifice of a work piece, and the outer fingers frictionally engage the work piece. A cable is inserted within the strain relief by piercing the membrane, which stretches and provides a seal against the cable. The cable is inserted through the aperture of the bushing and the resilient inner fingers flex outwardly to enable the cable to pass through, while engaging and digging into the cable to clasp it and provide strain relief.

Methods and systems for metal-to-metal sealing and, in particular, to the use of sintered parts to create metal-to-metal sealing joints is disclosed. In one example, a metal-to-metal sealing joint may comprise: a first mating surface and a second mating surface; wherein the first mating surface is formed on a first assembly having an annular projection with one or more annular grooves and the second mating surface is formed on a second assembly; wherein the projection is configured such that when the first and second surfaces are brought into mating contact, the annular projection on the first mating surface deforms the second mating surface to form a sealing joint. In this way, the metal-to-metal sealing joint between the first and second mating surfaces may minimize oil leakage between two assemblies, thereby improving engine fuel economy while simplifying part manufacturing.