A system for purging an aircraft fuel reservoir includes a body (48) configured to be assembled on the aircraft fuel reservoir (16) and a valve (50), received in the body (48), and having a released configuration of an outlet channel (70) and a tight closed configuration of the outlet channel (70). The system further comprises a transport pipe (44) secured to the body (48), the transport pipe (44) being configured to be fluidly connected to a fuel supply pipe (20) configured to supply an energy producing device. The transport pipe (44) extends at least between a fuel suction inlet (52) and a discharge outlet (54), the suction inlet (52) being configured to emerge in the aircraft fuel reservoir (16) and the discharge outlet (54) being configured to emerge in the supply pipe (20) when the body (48) is mounted on the aircraft fuel reservoir (16).

A system for purging an aircraft fuel reservoir includes a body (48) configured to be assembled on the aircraft fuel reservoir (16) and a valve (50), received in the body (48), and having a released configuration of an outlet channel (70) and a tight closed configuration of the outlet channel (70). The system further comprises a transport pipe (44) secured to the body (48), the transport pipe (44) being configured to be fluidly connected to a fuel supply pipe (20) configured to supply an energy producing device. The transport pipe (44) extends at least between a fuel suction inlet (52) and a discharge outlet (54), the suction inlet (52) being configured to emerge in the aircraft fuel reservoir (16) and the discharge outlet (54) being configured to emerge in the supply pipe (20) when the body (48) is mounted on the aircraft fuel reservoir (16).

A Presta valve connector includes a housing and a stripping assembly rotatably connected to the housing. The housing is provided with a channel and an airtight ring having a connection hole. The airtight ring and the stripping assembly are disposed at two opposite ends of the channel. One end of the stripping assembly is disposed in the channel, and another end of the stripping assembly is exposed out of the channel. One end of the stripping assembly is provided with a driving groove faced to the connection hole. The driving groove is provided with a first driving face formed as a plane.

A Presta valve connector includes a housing and a stripping assembly rotatably connected to the housing. The housing is provided with a channel and an airtight ring having a connection hole. The airtight ring and the stripping assembly are disposed at two opposite ends of the channel. One end of the stripping assembly is disposed in the channel, and another end of the stripping assembly is exposed out of the channel. One end of the stripping assembly is provided with a driving groove faced to the connection hole. The driving groove is provided with a first driving face formed as a plane.

A fluid coupling including a first adapter, a second adapter configured to selectively connect with and disconnect from the male adapter, an inner sleeve, a first seal between the first adapter and the inner sleeve, a second seal between the second adapter and the inner sleeve, and at least one thermally-activated seal between two of the first adapter, the second adapter, and the inner sleeve. During normal operation, the at least one thermally-activated seal may be spaced apart from at least one of the two of the first adapter, the second adapter, and the inner sleeve. At or above a predetermined temperature, the thermally-activated seal may be configured to expand to create a seal between the two of the first adapter, the second adapter, and the sleeve.

A build material container outlet structure, and a build material nozzle structure is described. The build material container outlet structure comprises a connector to releasably connect to a nozzle structure of an external aspiration system. The outlet structure comprises an aspiration channel to aspire build material from a build material container to the nozzle structure of the external aspiration system. The outlet structure comprises a protrusion protruding from an inner wall of the aspiration channel, to extend into an end portion of a tube of the nozzle structure that is inserted into the aspiration channel and retain a valve element of the nozzle structure in an open configuration.

A fluid coupler includes: an outer body; an end connector being at least partially received inside the outer body and configured to receive pressurized fluid; an inner body received inside the outer body, the inner body being moveable with respect to the outer body; a seat holder and a valve seat both located inside of the inner body, the valve seat being configured to press against an inner surface of the inner body to close the fluid coupler; a connector partially housed within the inner body, the connector comprising a first end secured to the seat holder and a second end. The fluid coupler defines a pressurized fluid flow path enabling pressurized fluid to contact and pressurize the end connector, the inner body, the seat holder, and the connector without contacting and pressurizing the outer body.

A fluid coupler includes: an outer body; an end connector being at least partially received inside the outer body and configured to receive pressurized fluid; an inner body received inside the outer body, the inner body being moveable with respect to the outer body; a seat holder and a valve seat both located inside of the inner body, the valve seat being configured to press against an inner surface of the inner body to close the fluid coupler; a connector partially housed within the inner body, the connector comprising a first end secured to the seat holder and a second end. The fluid coupler defines a pressurized fluid flow path enabling pressurized fluid to contact and pressurize the end connector, the inner body, the seat holder, and the connector without contacting and pressurizing the outer body.

A first tubular and a second tubular define a fluid passage. A feather is positioned within the first tubular. The feather is configured to axially translate towards the second tubular and pivot towards a center of the first tubular. The feather includes a hinge on a pivoting end. A first end of a spring is coupled to the feather and a second end of the spring is coupled to the first tubular. The spring is loaded to actuate a movement of the feather between an open position and a closed position. A trigger is positioned between the first tubular and the second tubular to provide an interference with the feather. The interference retains the feather in the open position when the first tubular and second tubular are coupled.

A first tubular and a second tubular define a fluid passage. A feather is positioned within the first tubular. The feather is configured to axially translate towards the second tubular and pivot towards a center of the first tubular. The feather includes a hinge on a pivoting end. A first end of a spring is coupled to the feather and a second end of the spring is coupled to the first tubular. The spring is loaded to actuate a movement of the feather between an open position and a closed position. A trigger is positioned between the first tubular and the second tubular to provide an interference with the feather. The interference retains the feather in the open position when the first tubular and second tubular are coupled.