Abstract: A gearbox de-oiler comprises a housing mounted to a shaft for rotation therewith. The housing defines a chamber containing a porous separator matrix. The chamber has an air-oil mixture inlet, an oil outlet and an air outlet. A separation plate separates the porous separator matrix into a primary flow path segment and a secondary flow path segment. The primary flow path segment extends axially from and fluidly connects the air-oil mixture inlet to a radial passage. The secondary flow path segment extends axially from and fluidly connects the radial passage to the air outlet. The secondary flow path segment axially overlaps the primary flow path segment and is disposed radially inwardly with respect thereto. Oil collector tubes projects radially outwardly from the separation plate across at least a portion of the primary flow path segment for fluidly connecting the secondary flow path segment to the oil outlet.

Abstract: A heat exchange system for an aircraft engine, has: a fuel conduit; an oil conduit; a first heat exchanger having a fuel passage and an oil passage, the fuel passage in heat exchange relationship with the oil passage; and a second heat exchanger having a fluid passage and an air passage fluidly in heat exchange relationship with the fluid passage, the air passage in fluid communication with a compressor, the fluid passage in fluid communication with one of: the oil conduit, the fluid passage flowing at least part of the oil flow through the fluid passage, the fluid passage of the second heat exchanger located upstream of the oil passage of the first heat exchanger relative to the oil flow, and the fuel conduit, the fluid passage flowing at least part of the fuel flow through the fluid passage.

Abstract: An oil tank and scavenge pipe assembly of a gas turbine engine comprises a tank, and a scavenge pipe having a discharge portion disposed inside the tank. The discharge portion comprises a first portion having first and second ends. The first end is adapted to connect to an oil return line for receiving a mixture of oil and air. A bend extends from the second end downstream thereof relative to a flow of the mixture of oil and air through the scavenge pipe. The bend is configured to cause stratification of the mixture of oil and air as the mixture of oil and air flows through it. An outlet downstream of the bend delivers the mixture of oil and air to the tank. A method of delivering an oil and air mixture to a rotating oil volume of a tank of a gas turbine engine is also presented.

Abstract: An oil tank and scavenge pipe assembly of a gas turbine engine comprises a tank, and a scavenge pipe having a discharge portion disposed inside the tank. The discharge portion comprises a first portion having first and second ends. The first end is adapted to connect to an oil return line for receiving a mixture of oil and air. A bend extends from the second end downstream thereof relative to a flow of the mixture of oil and air through the scavenge pipe. The bend is configured to cause stratification of the mixture of oil and air as the mixture of oil and air flows through it. An outlet downstream of the bend delivers the mixture of oil and air to the tank. A method of delivering an oil and air mixture to a rotating oil volume of a tank of a gas turbine engine is also presented.

Abstract: An oil tank and scavenge pipe assembly of a gas turbine engine comprises a tank, and a scavenge pipe having a discharge portion disposed inside the tank. The discharge portion comprises a first portion having first and second ends. The first end is adapted to connect to an oil return line for receiving a mixture of oil and air. A bend extends from the second end downstream thereof relative to a flow of the mixture of oil and air through the scavenge pipe. The bend is configured to cause stratification of the mixture of oil and air as the mixture of oil and air flows through it. An outlet downstream of the bend delivers the mixture of oil and air to the tank. A method of delivering an oil and air mixture to a rotating oil volume of a tank of a gas turbine engine is also presented.

Abstract: An oil tank and scavenge pipe assembly of a gas turbine engine comprises a tank, and a scavenge pipe having a discharge portion disposed inside the tank. The discharge portion comprises a first portion having first and second ends. The first end is adapted to connect to an oil return line for receiving a mixture of oil and air. A bend extends from the second end downstream thereof relative to a flow of the mixture of oil and air through the scavenge pipe. The bend is configured to cause stratification of the mixture of oil and air as the mixture of oil and air flows through it. An outlet downstream of the bend delivers the mixture of oil and air to the tank. A method of delivering an oil and air mixture to a rotating oil volume of a tank of a gas turbine engine is also presented.

Abstract: A lubrication system for a gas turbine engine including at least one porous element located in a cavity containing at least one rotating component receiving a flow of the lubricant, the porous element being located across a path taken by a portion of the lubricant expelled from the at least one respective rotating component such that the portion of the lubricant circulates therethrough, the at least one porous element being made of a material resistant to a temperature of the lubricant, the at least one porous element reducing a velocity of the portion of the lubricant circulating therethrough.

Abstract: A lubrication system for a gas turbine engine including at least one porous element located in a cavity containing at least one rotating component receiving a flow of the lubricant, the porous element being located across a path taken by a portion of the lubricant expelled from the at least one respective rotating component such that the portion of the lubricant circulates therethrough, the at least one porous element being made of a material resistant to a temperature of the lubricant, the at least one porous element reducing a velocity of the portion of the lubricant circulating therethrough.