Lubricating system for gas turbine engines and pump for such a system
AssigneeMTU Motoren- und Turbinen-Union Muenchen GmbH
InventorsJoachim Lorenz, Martin Gattinger
Life of this patent
Estimating the term…
Abstract
A lubricating system for bearing shafts and the like, for example, in a gas turbine power plant especially for an aircraft, has an oil-air separator which is vented to the atmosphere. A pump wheel is used for the separation of the oil and the air out of an oil-air mixture. The pump wheel is so constructed that centripedal and centrifugal forces are employed for the oil-air separation. The air passes by centripedal force through a sponge type filter structure and out through a hollow central shaft carrying the pump wheel or forming an integral one-piece component with said pump wheel. The oil does not travel through the filter but is reversed in its travel direction by centrifugal force for return into the lubricant circulating system.
Claims12
A pump for separating a gas from a liquid, comprising pump housing means (106), a pump wheel, hollow shaft means for rotatably supporting said pump wheel in said pump housing means and for providing a gas discharge duct for venting separated gas, approximately radially extending flow channels in said pump wheel, porous filter means (6) located in a central zone of said hollow shaft for cooperation with said flow channels, said porous filter means having a large surface area relative to a volume of said porous filter means, screen drum means surrounding said filter means, said screen drum means having screen openings which are relatively large compared to pores in said porous filter means, said porous filter means being connected to said radial channels through said relatively large openings in said screen drum means, and wherein said pump wheel has a wall extending outwardly beyond the radial channels and forming a wheel disk having an outer circumference provided with drive means for driving said pump wheel.
A system for lubricating a point or component of a gas turbine engine, comprising lubricant supply conduit means and lubricant return conduit means for forming a substantially closed lubricant circulating circuit, lubricant pressure pump means in said lubricant supply conduit means for transporting lubricant to said point, lubricant-air separator means in said lubricant return conduit means for separating lubricant and air, said lubricant-air separator means comprising a pump wheel and a hollow shaft supporting said pump wheel, approximately radially extending flow channels in said pump wheel, porous filter means (6) located in a central zone of said hollow shaft for cooperation with said flow channels, said porous filter means having a large surface area relative to a volume of said porous filter means, screen drum means surrounding said filter means, said screen drum means having screen openings which are relatively large compared to pores in said porous filter means, said porous filter means being connected to said radial channels through said relatively large openings in said screen drum means, said approximately radially extending flow channels in said pump wheel having such a configuration and position that a lubricant air mixture is transported through said channels in a centripedal direction toward said filter means, whereby oil is returned directly from the surface of said filter means back into said closed lubricant circulating circuit due to centrifugal force caused by rotation of said pump wheel, and wherein said pump wheel has a wall extending outwardly beyond the radial channels and forming a wheel disk having an outer circumference provided with drive means for driving said pump wheel.
Dependencies are inferred from the claim text.