Journal bearing with oil pocket
A journal shaft for a journal bearing assembly of an aircraft engine includes a shaft body extending along a longitudinal axis. The shaft body has a radially outer surface and a radially inner surface radially spaced apart from the longitudinal axis to define an inner cavity. An oil pocket is defined in the radially outer surface. One or more passages extend through the shaft body from the radially inner surface to the oil pocket to provide fluid communication between the inner cavity and the oil pocket. The oil pocket includes a radially inner base surface and interconnecting transition surfaces extending between the radially inner base surface of the oil pocket and the radially outer surface of the shaft body. The interconnecting transition surfaces form a fluid-dynamically smooth and edgeless transition to the radially outer surface of the journal shaft.
1. A journal shaft for a journal bearing assembly of an aircraft engine, comprising:
a shaft body extending along a longitudinal axis, the shaft body having a radially outer surface and a radially inner surface radially spaced apart from the longitudinal axis to define an inner cavity; and
an oil pocket defined in the radially outer surface, one or more passages extending through the shaft body from the radially inner surface to the oil pocket to provide fluid communication between the inner cavity and the oil pocket, the oil pocket including a radially inner base surface and interconnecting transition surfaces extending between the radially inner base surface of the oil pocket and the radially outer surface of the shaft body, wherein the interconnecting transition surfaces form a fluid-dynamically smooth and edgeless transition to the radially outer surface of the journal shaft;
wherein each of the interconnecting transition surfaces defines a tangent line relative to the longitudinal axis with a maximum angle of about six degrees.
2. The journal shaft as defined in claim 1 , wherein an axial length of each of the interconnecting transition surfaces occupies about ten to thirty percent of an overall axial length of the radially inner base surface.
3. The journal shaft as defined in claim 1 , wherein the maximum angle of tangent line is about one to four degrees.
4. The journal shaft as defined in claim 1 , wherein the oil pocket is axially symmetric about a longitudinal center of the shaft body.
5. The journal shaft as defined in claim 1 , wherein an axial profile of each of the interconnecting transition surfaces is defined by a linear function.
6. The journal shaft as defined in claim 1 , wherein an axial profile of each of the interconnecting transition surfaces is defined by a sinusoidal function.
7. The journal shaft as defined in claim 1 , wherein an axial profile of each of the interconnecting transition surfaces is defined by a double radius curve.
8. The journal shaft as defined in claim 1 , wherein the inner cavity defines a pin-receiving inner cavity, and the radially inner surface includes at least one circumferential oil chamber in fluid communication with the one or more passages.
9. The journal shaft as defined in claim 1 , wherein the one or more passages extending through the shaft body extend through the shaft body in a direction normal to the longitudinal axis.
10. A journal bearing assembly for an aircraft engine, comprising:
a bearing sleeve defining a bore; and
a journal shaft rotatable within the bore of the bearing sleeve, the journal shaft having a shaft body extending along a longitudinal axis, the shaft body having a radially outer surface and a radially inner surface radially spaced apart from the longitudinal axis to define an inner cavity, and an oil pocket defined in the radially outer surface, one or more passages extending through the shaft body from the radially inner surface to the oil pocket to provide fluid communication between the inner cavity and the oil pocket, the oil pocket including a radially inner base surface and interconnecting transition surfaces extending between the radially inner base surface of the oil pocket and the radially outer surface of the shaft body, wherein the interconnecting transition surfaces form a fluid-dynamically smooth and edgeless transition to the radially outer surface of the journal shaft.
11. The journal bearing assembly as defined in claim 10 , further comprising a pin disposed in the inner cavity of the journal shaft, the pin having a pin inner cavity in fluid communication with the inner cavity of the journal shaft via one or more pin radial passages.
12. The journal bearing assembly as defined in claim 11 , wherein the inner cavity of the journal shaft includes one or more circumferential oil chambers in fluid communication with the one or more pin radial passages and the one or more passages extending through the shaft body.
13. The journal bearing assembly as defined in claim 10 , wherein the oil pocket is axially symmetric about a longitudinal center of the shaft body.
14. The journal bearing assembly as defined in claim 10 , wherein an axial profile of each of the interconnecting transition surfaces is defined by one of a linear function, a polynomial function, a sinusoidal function or a double radius curve.
15. The journal bearing assembly as defined in claim 10 , wherein an axial length of each of the interconnecting transition surfaces occupies about ten to thirty percent of an overall axial length of the radially inner base surface.
16. The journal bearing assembly as defined in claim 10 , wherein each of the interconnecting transition surfaces defines a tangent line relative to the longitudinal axis with a maximum angle of about six degrees.
17. The journal bearing assembly as defined in claim 16 , wherein the maximum angle of the is about one to four degrees.
18. The journal bearing assembly as defined in claim 10 , wherein the one or more passages extending through the shaft body extend through the shaft body in a direction normal to the longitudinal axis.