IP Library Granted Patent US 10,753,456
Granted Patent B2
US 10,753,456 · App. 15/492,045 · Granted Aug 25, 2020

Oil transfer unit for transferring oil between a stationary part and a rotating part

Inventors: Lorenzo Cipolla (Rivalta di Torino, IT); Michele Gravina (Rivalta di Torino, IT)
Assignee: GE Avio S.r.l.
F16H57/0424F01D25/166F01D25/18F02C7/06F02C7/36F16H57/043F16H57/0479
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Quick Facts
Patent No.
US 10,753,456
App. No.
15/492,045
Granted
Aug 25, 2020
Kind
B2
Abstract

An oil transfer unit has a rotating part extending along an axis, a stationary part provided with an oil mouth, and a floating part coupled to the stationary part; the floating part is provided with a cylindrical surface fitted onto an outer cylindrical surface of the rotating part in a non-contact configuration, with an annular groove therebetween to put the oil mouth into communication with an inner chamber of the rotating part; both sides of the groove are sealed by oil films at a radial gap between the cylindrical surfaces of the floating and rotating parts; the unit has a plurality of recesses, which are delimited outwardly by the floating part and inwardly by the rotating part, are arranged on the opposite axial sides of the groove so as to locally enlarge the radial distance with respect to the radial gap and are inwardly closed by the rotating part.

Claims (40)

1. An oil transfer unit comprising:

a stationary part comprising an oil mouth;

a rotating part having an inner chamber and an outer cylindrical surface extending along an axis;

a floating part having a cylindrical surface, the cylindrical surface of the floating part corresponding to the outer cylindrical surface with a radial gap therebetween defining a non-contact configuration, and the floating part having opposed axial ends with opposing edges;

the floating part being positioned about said axis and connected to said stationary part with a defined freedom of movement with respect to the stationary part;

an annular groove defined by said rotating part and said floating part and in permanent fluid communication with said oil mouth and with said inner chamber; said radial gap defining, in use, an oil film sealing located on each side of said groove; and

a plurality of recesses, which are delimited outwardly by said floating part and inwardly by said rotating part, are arranged on opposite axial sides of and remote from said groove so as to locally enlarge the radial distance between said floating part and said rotating part and are inwardly closed by said rotating part.

2. The oil transfer unit according to claim 1 , wherein said recesses are axially spaced apart from said groove and from said edges.

3. The oil transfer unit according to claim 1 , wherein said recesses are symmetric with respect to a mid-plane of said groove.

4. The oil transfer unit according to claim 3 , wherein said recesses are aligned along two annular rows, each arranged on a corresponding side of said groove.

5. The oil transfer unit according to claim 1 , wherein, on each side of said groove, said recesses are spaced apart from each other.

6. The oil transfer unit according to claim 5 , wherein, on each side of said groove, said recesses are angularly spaced apart from each other.

7. The oil transfer unit according to claim 1 , wherein said recesses are radially defined outwardly by respective pockets made into said cylindrical surface and inwardly by said outer cylindrical surface.

8. The oil transfer unit according to claim 1 , wherein said floating part has:

an annular channel in permanent fluid communication with said oil mouth;

at least one radial hole, that puts said channel in permanent fluid communication with said groove;

a plurality of passages, that put said channel in permanent fluid communication with said recesses and are distinct from said at least one radial hole.

9. The oil transfer unit according to claim 8 , wherein said recesses comprise respective arc portions, elongated along a circumferential direction about said axis, and respective axial branches, which axially extend from said arc portions towards said groove; said passages being defined by further radial holes.

10. The oil transfer unit according to claim 8 , wherein said recesses comprise respective arc portions, elongated along a circumferential direction about said axis, and respective recesses, made on an axial side of the arc portions towards said groove; said passages being defined by holes inclined with respect to radial and axial directions.

11. An oil transfer unit comprising:

a stationary part comprising an oil mouth;

a rotating part having an inner chamber and an outer cylindrical surface extending along an axis;

a floating part having a cylindrical surface, the cylindrical surface of the floating part corresponding to the outer cylindrical surface with a radial gap therebetween defining a non-contact configuration, and the floating part having opposed axial ends with opposing edges;

the floating part being positioned about said axis and connected to said stationary part with a defined freedom of movement with respect to the stationary part;

an annular groove defined by said rotating part and said floating part and in permanent fluid communication with said oil mouth and with said inner chamber; said radial gap defining, in use, an oil film sealing located on each side of said groove; and

a plurality of recesses, which are delimited outwardly by said floating part and inwardly by said rotating part, are arranged on opposite axial sides of said groove so as to locally enlarge the radial distance between said floating part and said rotating part and are inwardly closed by said rotating part;

wherein said floating part has:

an annular channel in permanent fluid communication with said oil mouth;

at least one radial hole, that puts said channel in permanent fluid communication with said groove; and

a plurality of passages, that put said channel in permanent fluid communication with said recesses and are distinct from said at least one radial hole; and

wherein said recesses comprise respective arc portions, elongated along a circumferential direction about said axis, and respective recesses, made on an axial side of the arc portions towards said groove; said passages being defined by holes inclined with respect to radial and axial directions.

12. The oil transfer unit according to claim 11 , wherein said recesses are axially spaced apart from said groove and from said edges.

13. The oil transfer unit according to claim 11 , wherein said recesses are symmetric with respect to a mid-plane of said groove.

14. The oil transfer unit according to claim 13 , wherein said recesses are aligned along two annular rows, each arranged on a corresponding side of said groove.

15. The oil transfer unit according to claim 11 , wherein, on each side of said groove, said recesses are spaced apart from each other.

16. The oil transfer unit according to claim 15 , wherein, on each side of said groove, said recesses are angularly spaced apart from each other.

17. The oil transfer unit according to claim 11 , wherein said recesses are radially defined outwardly by respective pockets made into said cylindrical surface and inwardly by said outer cylindrical surface.

18. The oil transfer unit according to claim 11 , wherein said recesses are axially spaced apart from said edges.

19. The oil transfer unit according to claim 11 , wherein said recesses are radially defined outwardly by respective pockets made into said cylindrical surface.

20. The oil transfer unit according to claim 11 , wherein said recesses are radially defined inwardly by said outer cylindrical surface.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 20, 2017
From: CIPOLLA, LORENZO; GRAVINA, MICHELE
To: GE AVIO S.R.L.
Reel/Frame 042073/0437 →
Priority Claims (1)
IT 102016000040539 · Apr 20, 2016 · national
Continuity (1)
Related Publication 20170307062A1 · Oct 26, 2017