A container for containing a liquid within a vehicle, an internal combustion engine comprising a container, a vehicle comprising a container and a method of directing flow of liquid are disclosed. The container comprises an outer wall configured to contain a liquid and a plurality of baffles configured to direct flow of the liquid within the container. The plurality of baffles define a pickup chamber, at least three outer chambers positioned adjacent to the pickup chamber and at least one respective gap for each said outer chamber to allow liquid flow from each outer chamber through the at least one respective gap into the pickup chamber. A directing means is configured to cause liquid flowing from each of the outer chambers to flow around a vertical axis within the pickup chamber.

A lubrication and hydraulic actuation system for a transfer case (120) includes a pump (220), a pump sump (210) formed in the transfer case (120), and having an opening (430) in communication with an interior of the transfer case (120), and a fluid retention element (510, 710). The fluid retention element (510, 710) is disposed in the opening (430) of the pump sump (210) and has at least one baffle structure (550) to allow fluids to enter the pump sump (210) through the fluid retention element (510, 710) and restrain fluids from exiting the pump sump (210) through the fluid retention element (510, 710).

A preventing apparatus for concentrating oil of a vehicle includes: a chamber disposed in an oil pan to enclose the surrounding of an oil strainer and having both sides provided with through holes through which oil inflows and outflows; and an oil blocking module disposed to be spaced apart from the through holes in the chamber and operated in an opposite direction to a turning direction of the vehicle when the vehicle turns in order to block one of the through holes of the chamber.

An oil circulation device for an internal combustion engine includes an oil pan, a partition, and a communication groove. The oil pan is disposed below a cylinder block and includes a bottom wall and a sidewall to define a recessed portion that opens upward. The partition extends upward from the bottom wall so as to have a protruding end and divide the recessed portion into a first recessed portion and a second recessed portion. The communication groove extends downward from the protruding end of the partition in a thickness direction of the partition to connect the first recessed portion and the second recessed portion.

A fluid delivery system includes a reservoir for storing fluid, a rotary pump having a first pump port and a second pump port, a first fluid conduit connecting the first pump port to the reservoir, and a second fluid conduit connecting the second pump port to the reservoir. The rotary pump rotates in a first delivery direction in a normal mode and in a second delivery direction in an alternative mode. A first valve separates the first pump port from the reservoir when the rotary pump is in its alternative mode, and a second valve separates the second pump port from the reservoir when the rotary pump is in its normal mode.

An apparatus and methods for the lubrication of the engine of an off-road vehicle, such as when the vehicle is airborne or upside down due to tipping over. The apparatus includes an upper chamber and a lower chamber. Fluid communication is established between the upper chamber and the lower chamber by way of a central tube. One or more vanes are arranged in the interior of the central tube to inhibit oil flow from the lower chamber to the upper chamber when the vehicle is upside down. An inlet hose connector is configured for receiving engine oil from an oil cooler and supplying the engine oil to the lower chamber. An outlet hose connector is configured for conducting the engine oil from the lower chamber to the engine. A bypass hose connector is configured for allowing the engine oil to exit from the upper chamber to the engine.

Aircraft engine oil tanks, lubrication systems, and associated methods are provided. The oil tank includes a first tank portion defining a first volume for holding oil and a second tank portion defining a second volume for holding oil, in fluid communication with the first volume. The first tank portion includes an oil outlet for delivering oil to a lubrication load via a pump. The first volume is in fluid communication with a vent opening for venting the oil tank. At least part of the second tank portion is disposed higher than the vent opening for retaining a quantity of oil inside the oil tank during a negative-g force flight condition and facilitate the recovery of the lubrication system following the negative-g force flight condition.

A transmission oil sump comprises a main oil compartment, in which a suction line of an oil pump is located, and a secondary oil compartment. The secondary oil compartment is in fluid communication with the main oil compartment via an opening. To prevent the introduction of air during rapid acceleration, cornering at high speeds and/or rapid deceleration of the vehicle, a barrier closes the opening to prevent the flow of oil out of the main oil compartment into the secondary oil compartment so that the oil level, required for the oil pump in the main compartment, remains adequately high. When not closed, the opening of the secondary oil compartment is open to ensure oil flow from the secondary oil compartment to the main oil compartment. The secondary oil compartments is arranged so as to collect oil that leaks from transmission components.

Aircraft engine oil tanks, lubrication systems, and associated methods are provided. The oil tank includes a first tank portion defining a first volume for holding oil and a second tank portion defining a second volume for holding oil, in fluid communication with the first volume. The first tank portion includes an oil outlet for delivering oil to a lubrication load via a pump. The first volume is in fluid communication with a vent opening for venting the oil tank. At least part of the second tank portion is disposed higher than the vent opening for retaining a quantity of oil inside the oil tank during a negative-g force flight condition and facilitate the recovery of the lubrication system following the negative-g force flight condition.

A lubrication fluid reservoir apparatus for a vehicle engine is disclosed herein. The apparatus includes a sump plate having a tunnel port assembly, a valve assembly, and a baffle assembly that are operable to minimize agitation of lubrication fluid in the sump plate and maintain lubrication fluid available to a lubrication fluid take-up tube during high G-force turns of the vehicle to prevent engine oil starvation, in various aspects.