A gas turbine engine, comprising: a fan section configured to induce air from a surrounding environment into the gas turbine engine; a compressor section in fluid communication with the fan section and configured to compress the air received from the fan section; a combustor section in fluid communication with the compressor section and configured to ignite a fuel-air mixture to generate combustion gases; a turbine section in fluid communication with the combustor section; and characterised by a debris capture device to remove particulate matter from fluids associated with lubricating rotating components of the gas turbine engine, comprising: an oil filtration assembly including a housing having a thickness defined between an internal surface of the housing and an external surface of the housing, the housing configured to receive a first filter and define an outer annular flow passage between a first outer surface of the first filter and the internal surface of the housing; an inlet pipe in fluid communication with the oil filtration assembly, the inlet pipe configured to inject an oil into the housing to impart a centrifugal force; an outlet pipe in fluid communication with the oil filtration assembly to discharge the oil from the housing; and a collection area disposed towards an end of the outer annular flow passage distal the inlet pipe, the collection area configured to collect the particulate matter from the oil; wherein a width of the outer annular flow passage increases towards the collection area. a fan section configured to induce air from a surrounding environment into the gas turbine engine; a compressor section in fluid communication with the fan section and configured to compress the air received from the fan section; a combustor section in fluid communication with the compressor section and configured to ignite a fuel-air mixture to generate combustion gases; a turbine section in fluid communication with the combustor section; and characterised by a debris capture device to remove particulate matter from fluids associated with lubricating rotating components of the gas turbine engine, comprising: an oil filtration assembly including a housing having a thickness defined between an internal surface of the housing and an external surface of the housing, the housing configured to receive a first filter and define an outer annular flow passage between a first outer surface of the first filter and the internal surface of the housing; an inlet pipe in fluid communication with the oil filtration assembly, the inlet pipe configured to inject an oil into the housing to impart a centrifugal force; an outlet pipe in fluid communication with the oil filtration assembly to discharge the oil from the housing; and a collection area disposed towards an end of the outer annular flow passage distal the inlet pipe, the collection area configured to collect the particulate matter from the oil; wherein a width of the outer annular flow passage increases towards the collection area. an oil filtration assembly including a housing having a thickness defined between an internal surface of the housing and an external surface of the housing, the housing configured to receive a first filter and define an outer annular flow passage between a first outer surface of the first filter and the internal surface of the housing; an inlet pipe in fluid communication with the oil filtration assembly, the inlet pipe configured to inject an oil into the housing to impart a centrifugal force; an outlet pipe in fluid communication with the oil filtration assembly to discharge the oil from the housing; and a collection area disposed towards an end of the outer annular flow passage distal the inlet pipe, the collection area configured to collect the particulate matter from the oil; wherein a width of the outer annular flow passage increases towards the collection area.