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An air bearing shaft has a first cylindrical portion with a relatively small outer diameter, and a ramped surface extending at an angle that is non-perpendicular and non-parallel to a central axis of a shaft body. The ramped surface leads into a second cylindrical portion of the shaft has a large ou

An air bearing shaft has a first cylindrical portion with a relatively small outer diameter, and a ramped surface extending at an angle that is non-perpendicular and non-parallel to a central axis of a shaft body. The ramped surface leads into a second cylindrical portion of the shaft has a large outer diameter that is greater than the diameter of the first cylindrical portion. There are twelve air holes formed to extend into an interior of the second cylindrical portion. A bore diameter is defined to an inner periphery of the second cylindrical portion at the location of the air holes. A ratio of the bore diameter to a diameter of the air holes is between 6.30 and 6.54. In addition, a bearing assembly, a compressor, and a method of incorporating an air bearing shaft into a compressor are all disclosed and claimed.

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1. An air bearing shaft comprising: a shaft body having a first cylindrical portion with a relatively small outer diameter, and a ramped surface that extends at an angle that is non-perpendicular and non-parallel to a central axis of the shaft body, said ramped surface leading into a second cylindri

1. An air bearing shaft comprising: a shaft body having a first cylindrical portion with a relatively small outer diameter, and a ramped surface that extends at an angle that is non-perpendicular and non-parallel to a central axis of the shaft body, said ramped surface leading into a second cylindrical portion with a diameter greater than the diameter of said first cylindrical portion;twelve air holes formed in said shaft body, and extending into an interior of said second cylindrical portion, a bore diameter being defined to an inner periphery of said second cylindrical portion at said air holes, and a ratio of said bore diameter to a diameter of said air holes is between 6.30 and 6.54;a distance defined from an axial end of said second cylindrical portion remote from said ramped portion, and a ratio of said distance to said diameter of said air holes is between 10.80 and 11.21; andsaid twelve holes being equally spaced about a circumference of said second cylindrical portion. 2. An air bearing assembly comprising: a journal bearing having air flow passages; an air bearing shaft having a shaft body with a first cylindrical portion having a relatively small outer diameter, and a ramped surface that extends at an angle that is non-perpendicular and non-parallel to a central axis of the shaft body, said ramped surface leading into a second cylindrical portion that has a diameter that is greater than the diameter of said first cylindrical portion, and twelve air holes formed in said shaft body, and extending into an interior of said second cylindrical portion, a bore diameter being defined to an inner periphery of said second cylindrical portion at said air holes, and a ratio of said bore diameter to a diameter of said air holes is between 6.30 and 6.54; and a distance defined from an axial end of said second cylindrical portion remote from said ramped portion, and a ratio of said distance to said diameter of said air holes is between 10.80 and 11.21. 3. The air bearing assembly as set forth in claim 2, wherein said twelve holes are equally spaced about a circumference of said second cylindrical portion. 4. The air bearing assembly as set forth in claim 2, wherein said journal bearing has a plurality of corrugations to form air passages. 5. An air compressor for supplying air to an aircraft cabin comprising: a motor driving a main shaft, said main shaft driving a compressor rotor;an air bearing system, including an air supply for supplying a source of air into a housing for housing said motor, said main shaft and said compressor rotor, an air bearing positioned to be radially outward of an air bearing shaft, and a central axis defined by said main shaft, said air bearing being positioned axially between said motor and said rotor;the air bearing shaft having a shaft body with a first cylindrical portion having a relatively small outer diameter, and a ramped surface that extends at an angle that is non-perpendicular and non-parallel to a central axis of the shaft body, said ramped surface leading into a second cylindrical portion that has a diameter greater than the diameter of said first cylindrical portion, and twelve air holes formed in said shaft body, and extending into an interior of said second cylindrical portion, a bore diameter being defined to an inner periphery of said second cylindrical portion at said air holes, and a ratio of said bore diameter to a diameter of said air holes is between 6.30 and 6.54;the first cylindrical portion secured on an outer periphery of a rotor for said motor, and an end of said second cylindrical portion remote from said ramped portion being secured on a surface of said compressor rotor, with said main shaft being a tie-rod extending through said rotor, said air bearing shaft, and said motor rotor, and securing the components together to rotate as one; andwherein a distance is defined from an axial end of said second cylindrical portion remote from said ramped portion, and a ratio of said distance to said diameter of said air holes is between 10.80 and 11.21. 6. The air compressor as set forth in claim 5, wherein said twelve holes are equally spaced about a circumference of said second cylindrical portion. 7. The air compressor as set forth in claim 5, wherein said air bearing includes a plurality of corrugations to define air passages. 8. The air compressor as set forth in claim 5, wherein an airflow path includes air passing along thrust bearing surfaces and between an outer periphery of a thrust bearing shaft, along thrust bearing surfaces, and between an outer periphery of the thrust bearing shaft, and journal bearings, and then a portion of the air flowing through said holes into the interior of said air bearing shaft. 9. A method of installing an air bearing shaft in a compressor comprising the steps of: (a) providing an air bearing shaft having a shaft body including a first cylindrical portion with a relatively small outer diameter, and a ramped surface that extends at an angle that is non-perpendicular and non-parallel to a central axis of the shaft body, said ramped surface leading into a second cylindrical portion that has a diameter greater than the diameter of said first cylindrical portion, twelve air holes formed in said shaft body, and extending into an interior of said second cylindrical portion, a bore diameter being defined to an inner periphery of said second cylindrical portion at said air holes, and a ratio of said bore diameter to a diameter of said air holes is between 6.30 and 6.54, a distance defined from an axial end of said second cylindrical portion remote from said ramped portion, and a ratio of said distance to said diameter of said air holes is between 10.80 and 11.21, said twelve holes being equally spaced about a circumference of said second cylindrical portion;(b) securing said air bearing shaft to a motor rotor, and to a compressor rotor;(c) securing said compressor rotor, said air bearing shaft, and said motor rotor together with a tie-rod which is tightened to secure the components to rotate as one; and(d) positioning said air bearing shaft disk between opposed housing surfaces, with said opposed housing surfaces defining thrust bearing surfaces.