One embodiment of a fuel tank cap and mounting bracket apparatus includes a cap including protrusions on a lower surface of the cap, the protrusions including a raised portion adapted to be received within a recess of a mounting bracket to secure the cap to the mounting bracket. One embodiment of the mounting bracket includes slots to receive the protrusions of the cap and recesses to receive the raised portion of each protrusion. In one embodiment of the mounting bracket the slots and the recesses are surrounded by mounting bracket material on all sides so that the shape of the slots and recesses is protected against deformation during an impact, thereby inhibiting separation of the cap from the mounting bracket.

A closure system for a pressurized container system for a motor vehicle includes a fuel filler flap and at least one refueling connection. The refueling connection has a non-return valve and a protective cap. The protective cap is designed to be pluggable onto an end of the refueling connection. The fuel filler flap covers a refueling compartment which is set back from the vehicle body. On the side facing the refueling compartment, the fuel filler flap has such a contour that the fuel filler flap can be closed only if the protective cap is fitted on the refueling connection.

Methods and systems are provided for an adapter for a fluid refilling system. In one example, an adapter configured for use with a diesel exhaust fluid (DEF) system may include a first end configured to couple with a DEF refill passage, a second end including an aperture shaped to receive a DEF nozzle, a pivotable door closing the aperture and biased against the aperture by a biasing member, and a magnetic ring positioned within the adapter and downstream of the pivotable door. The pivotable door may be formed of a material permeable to DEF vapors and may include a plurality of vent holes configured to flow vapors from the DEF system to atmosphere.

One embodiment of a fuel tank cap and mounting bracket apparatus includes a cap including protrusions on a lower surface of the cap, the protrusions including a raised portion adapted to be received within a recess of a mounting bracket to secure the cap to the mounting bracket. One embodiment of the mounting bracket includes slots to receive the protrusions of the cap and recesses to receive the raised portion of each protrusion. In one embodiment of the mounting bracket the slots and the recesses are surrounded by mounting bracket material on all sides so that the shape of the slots and recesses is protected against deformation during an impact, thereby inhibiting separation of the cap from the mounting bracket.

An auxiliary fuel tank for a flexible fuel vehicle is provided. The auxiliary fuel tank is mounted to an auxiliary tank body for storing gasoline fuel and is installed in an engine compartment of a flexible fuel vehicle. The auxiliary fuel tank includes a canister that is coupled to the auxiliary tank body and has activated carbon therein. The canister is configured to collect fuel evaporation gas generated in the auxiliary tank body to supply fuel components to an engine.

A fuel tank cap includes a seal cap body and a detaching-proof unit. The cap body has a handheld wall and a surrounding wall that extends from the handheld wall and that is formed with an engaging groove. The detaching-proof unit includes a ring sleeve member and a connection member. The ring sleeve member has an outer ring wall that surrounds the surrounding wall, and a resilient wall that extends the outer ring wall and that is engaged resiliently with the engaging groove. The connection member is connected to the ring sleeve member to be connected to a cap installation portion of a vehicle body.

A grounded fuel tank assembly includes a non-metallic fuel tank having a container and a hollow filler neck, a fuel cap with a hollow stem, and an electrically conductive insert member. The insert member includes a hollow sleeve which is received by the neck, an annular frusto-conical first ring which is joined to an end of the sleeve, and a second ring which extends away from the first ring and which at least partially surrounds a portion of the neck. The sleeve has internal and external sleeve threads formed thereon. The internal sleeve threads engages external cap threads, and the external sleeve threads engages internal neck threads. An electrically conductive ground strap is exterior to the container and engages the second ring. The insert includes tabs which engage the neck to prevent rotation of the insert.

An auxiliary fuel tank for a flexible fuel vehicle is provided. The auxiliary fuel tank is mounted to an auxiliary tank body for storing gasoline fuel and is installed in an engine compartment of a flexible fuel vehicle. The auxiliary fuel tank includes a canister that is coupled to the auxiliary tank body and has activated carbon therein. The canister is configured to collect fuel evaporation gas generated in the auxiliary tank body to supply fuel components to an engine.

A fuel tank lid includes a lid part closing an opening of a fuel tank, and an internal terminal electrically connecting a pump provided inside the fuel tank with a drive circuit driving the pump. The lid part includes an inserted part inserted into the opening, a storage part located outside the fuel tank and storing the drive circuit in a hollow space of the storage part, and a connection part located outside the fuel tank and connecting the inserted part and the storage part. The fuel tank lid further includes a discharge part discharging a fuel vapor that tries to travel along an interface between the internal terminal and the lid part and enter the hollow space, to an external atmosphere, and a protection part covering the portion exposed from the lid part by the presence of the discharge part to protect the portion from a liquid.

The present invention relates to a sealing device designed for sealing a fuel inlet opening of an aircraft engine and to an aircraft engine provided with such a sealing device. The invention further relates to a method for sealing a fuel inlet opening of an aircraft engine.