초록 ▼

A seal shaft for use in an air cycle machine has two axial edges. An axial distance is measured between contact faces at the axial edges, with a tolerance to the dimension. A greatest variation between the axial distance at a plurality of spaced locations on the edge face is maintained with a ratio

A seal shaft for use in an air cycle machine has two axial edges. An axial distance is measured between contact faces at the axial edges, with a tolerance to the dimension. A greatest variation between the axial distance at a plurality of spaced locations on the edge face is maintained with a ratio of the greatest variation to the tolerance being less than 0.2. A rotor assembly, an air cycle machine and a method are also disclosed.

대표청구항 ▼

1. A seal shaft for use in an air cycle machine comprising: a body centered on a central axis, said body defining an inner bore and an outer surface including radially outwardly extending ledges at each of two axial edges, and a radially inner surface at an outer peripheral surface, with radially ou

1. A seal shaft for use in an air cycle machine comprising: a body centered on a central axis, said body defining an inner bore and an outer surface including radially outwardly extending ledges at each of two axial edges, and a radially inner surface at an outer peripheral surface, with radially outwardly extending feature axially spaced on an opposed side of said radially inner surface relative to said outwardly extending ledges and a plurality of air holes extending from said outer peripheral surface to said inner bore;an axial distance measured between contact faces on said axial edges, a tolerance to said axial distance, and a greatest variation maintained between said axial distance at a plurality of spaced locations on said contact faces, with a ratio of said greatest variation to said tolerance being less than 0.2; andwherein said axial distance is 0.770 in (1.95 cm), said tolerance is 0.002 in (0.005 cm) and said greatest variation is 0.0003 in (0.762 cm). 2. The seal shaft as set forth in claim 1, wherein said ratio is less than 0.175. 3. A rotor assembly for use in an air cycle machine comprising: a pair of turbine rotors rotating with a shaft, a compressor rotor rotating with said shaft, and a fan rotor rotating with said shaft and a seal shaft positioned intermediate one of said turbine rotors and said compressor rotor;said seal shaft including a body centered on a central axis, said body defining an inner bore and an outer surface including radially outwardly extending ledges at each of two axial edges, and a radially inner surface at an outer peripheral surface, with radially outwardly extending features axially spaced on an opposed side of said radially inner surface relative to said outwardly extending ledges and a plurality of air holes extending from said outer peripheral surface to said inner bore, an axial distance measured between contact faces on said axial edges, a tolerance to said axial distance, and a greatest variation maintained between said axial distance at a plurality of spaced locations on said contact faces, with a ratio of said greatest variation to said tolerance being less than 0.2; andwherein said axial distance is 0.770 in (1.95 cm), said tolerance is 0.002 in (0.005 cm) and said greatest variation is 0.0003 in (0.762 cm). 4. The rotor assembly as set forth in claim 3, wherein said ratio is less than 0.175. 5. An air cycle machine comprising: a housing receiving a rotor assembly, the rotor assembly including a pair of turbine rotors rotating with a shaft, a compressor rotor rotating with said shaft, and a fan rotor rotating with said shaft and a seal shaft positioned intermediate one of said turbine rotors and said compressor rotor;said seal shaft including a body centered on a central axis, said body defining an inner bore and an outer surface including radially outwardly extending ledges at each of two axial edges, and a radially inner surface at an outer peripheral surface, with radially outwardly extending features axially spaced on an opposed side of said radially inner surface relative to said outwardly extending ledges and a plurality of air holes extending from said outer peripheral surface to said inner bore, an axial distance measured between contact faces on said axial edges, a tolerance to said axial distance, and a greatest variation maintained between said axial distance at a plurality of spaced locations on said contact faces, with a ratio of said greatest variation to said tolerance being less than 0.2 , andwherein said axial distance is 0.770 in (1.95 cm), said tolerance is 0.002 in (0.005 cm) and said greatest variation is 0.0003 in (0.762 cm). 6. The air cycle machine as set forth in claim 5, wherein said ratio is less than 0.175. 7. A method of replacing a seal shaft in an air cycle machine comprising the steps of: removing a seal shaft from a housing from a location intermediate a turbine rotor and a compressor rotor and replacing a new seal shaft;said new seal shaft including a body centered on a central axis, said body defining an inner bore and an outer surface including radially outwardly extending ledges at each of two axial edges, and a radially inner surface at an outer peripheral surface, with radially outwardly extending features axially spaced on an opposed side of said radially inner surface relative to said outwardly extending ledges and a plurality of air holes extending from said outer peripheral surface to said inner bore, an axial distance measured between contact faces on said axial edges, a tolerance to said axial distance, and a greatest variation maintained between said axial distance at a plurality of spaced locations on said contact faces, with a ratio of said greatest variation to said tolerance being less than 0.2; andwherein said axial distance is 0.770 in (1.95 cm), said tolerance is 0.002 in (0.005 cm) and said greatest variation is 0.0003 in (0.762 cm). 8. The method as set forth in claim 7, wherein said ratio is less than 0.175. 9. The method as set forth in claim 7, wherein the replacement of the new seal shaft includes establishing a press-fit between the new seal shaft, and the turbine and compressor rotors.