Catalytic converter for gas turbine bleed air extraction

An assembly for removing substantially all oil contamination from bleed air flowing at a temperature of the order of 600-650 degrees Fahrenheit from a bleed air port of a gas turbine aircraft engine to a duct leading through an air conditioning component to the cabin ventilation system of an aircraft, said assembly comprising a gas turbine aircraft engine having a bleed port containing bleed air at a temperature of the order of 600-650 degrees Fahrenheit, means defining a duct, a catalytic converter interposed between and sealably coupled between said port and said duct at a location with respect to said engine such that the temperature of bleed air entering the converter is in the range of 600-650 degrees Fahrenheit, said catalytic converter further comprising a pipe wherein there is sealably mounted at least one catalytic converter matrix element through which said bleed air must flow at a mean velocity and at a temperature of the order of 600 to 650 degrees Fahrenheit, each said matrix element comprising a parallel array of a large number of slender tubules through which said bleed air flows in parallel, said tubules being coated internally with a catalytically active coating comprising finely-divided particles of metals chosen from group VIII of the periodic table of the elements, said tubules having an element tubule length and small individual cross-dimension and mean individual cross-section area, effective tubule length of a series-arrayed plurality of such catalytic converter matrix elements being the sum of their element tubule lengths, flow residence time being the quotient of said effective tubule length divided by said mean flow velocity, and the ratio of said mean individual cross-section area to said flow residence time being not greater than 2.52 square centimeters per second.