A conduit guide for guiding at least one conduit section between a first element and a second element with an insert part, having a tubular guiding element and arrangeable at the first element, and a tubular receiving part, arrangeable at the second element, wherein the guiding element of the insert part is arranged so as to be axially movable in the receiving part.

An assembly for sealing an interface between a conduit and a case includes a boot and a bushing. The boot includes a tube and rubber flange. The rubber flange extends generally radially outward from the tube. The rubber flange includes an opening passing through a portion of the rubber flange. The bushing is disposed in the rubber flange and includes a tubular body, a channel, and a lip. The tubular body is disposed in the opening of the rubber flange. The channel extends through a center of the body. The lip is generally flat and extends radially outward from the tubular body. The lip is in contact and engages with the rubber flange so as to compress the rubber flange against the case.

Quick coupling device 1 for transferring liquid for an aircraft, comprising a female member 7 configured to be connected to a first reservoir, said female member 7 forming a passage and comprising a cylindrical portion 13 and a radial portion 14, a male member 2 configured to be connected to a second reservoir, said male member 2 forming a passage, slidably mounted in a liquid-tight manner in the female member 7 and comprising a cylindrical portion 3 and a radial portion 4, and a member 40 for locking the male member 2 in the female member 7, the locking member 40 being disposed between the radial portion 14 of the female member 7 and the radial portion 4 of the male member 2, the locking member 40 surrounding the male member 2 and leaving a limited sliding extent for the male member 2 with respect to the female member 7, engaging with the female member 7 in the locked position and releasing the female member 7 in the unlocked position, the locking member 40 comprising an axial blocking lock that can be actuated by an axial then rotating movement and that can be released by an axial then rotating movement, and a rotation brake, the lock and the brake being active in the locked position.

A firestop system for fire stopping a bus duct that passes through an opening in a marine deck or a marine bulkhead includes a boot seal wrapped around the bus duct housing. The boot seal has a top end attached to the bus duct, and a bottom end attached to the division. The boot seal is made of flexible material to allow for movement of the bus duct relative to the division due to vibration. The boot seal may be made of a thermal barrier wrap or other high-temperature insulating mat materials to allow heat generated under normal condition to escape while providing firestopping and temperature resistance under fire exposure conditions. The firestop system may also have a gasket positioned between the bus duct and the boot seal to accommodate irregularities in the outside surface of the bus duct housing.

A line penetration for routing a line through a building part, which has a closure plate for covering a passage opening in the building part and a fastening arrangement. The closure plate has at least one line opening for receiving the line. The fastening arrangement can be fastened to the building part, for holding the closure plate, so that a relative displacement of the closure plate along a surface direction of the closure plate is permitted and the closure plate is fixed perpendicular to the surface direction of the closure plate.

The invention relates to an umbilical termination assembly for terminating a cable or umbilical. The termination assembly comprises a plurality of umbilical elements extending from an umbilical and which pass through a bulkhead plate. The seated ball element has a spherical body through which an umbilical element passes. The ball element is seated in a cup member which allows the ball element to rotate through a large range of angles allowing it to be aligned with the umbilical element without the umbilical element needing to be manipulated or forced into position. The umbilical element can then be attached to the ball element which is supported by the cup member on the bulkhead. This allows the axial tension in the umbilical element to be transferred to the bulkhead.

A pipe support for supporting a pipe of an aircraft fuel system is disclosed. The pipe support has first and second parts which together form a collar to retain the pipe. The first and second parts of the pipe support are able to be moved relative to each other between an open condition, in which the pipe is insertable between the first and second parts, and a closed condition, in which the first and second parts are brought together to retain the pipe. The collar is locatable in an opening in a structural member, such as a wing rib. When the collar is located in the opening in the wing rib, the pipe support is restricted from moving from the closed condition.

An assembly for sealing an interface between a conduit and a case includes a boot and a bushing. The boot includes a tube and rubber flange. The rubber flange extends generally radially outward from the tube. The rubber flange includes an opening passing through a portion of the rubber flange. The bushing is disposed in the rubber flange and includes a tubular body, a channel, and a lip. The tubular body is disposed in the opening of the rubber flange. The channel extends through a center of the body. The lip is generally flat and extends radially outward from the tubular body. The lip is in contact and engages with the rubber flange so as to compress the rubber flange against the case.

A line penetration for routing a line through a building part. The line penetration includes a first lamellar element with a hollow-cylindrical first base part for receiving the line in a straight-through line opening, and with first circumferential lamellas, which extend outwardly transverse to an axial direction of the first base part; a second lamellar element with a hollow-cylindrical second base part for arrangement in a passage opening of the building part, and with second circumferential lamellas, which extend inwardly transverse to an axial direction of the line opening, where the first and second lamellas mesh with one another in the manner of a comb, so that the side faces of the lamellas are impermeable to gas and bear slidingly on one another.

A line feed-Through for feeding a line through a building component can include one or more sealing arrangements for feeding the line through, wherein the one or more sealing arrangements have at least two sealing structures lying opposite each other, wherein at least one first of the sealing structures has an arrangement of elongate fins adjacent to each other, the protruding ends of which lie against a second of the sealing structures and thus seal the passage region.