IP Library › Granted Patent US 10,415,693
Granted Patent B2
US 10,415,693 · App. 15/384,179 · Granted Sep 17, 2019

Oil transfer assembly for supplying oil into a rotating and translating tube

Inventor: Paolo Altamura (Brindisi, IT)
Assignee: General Electric Company
F16H57/0486B64C11/38F01D25/18F02C7/36F02K3/02F16C3/023F16H57/043F05D2260/40311F05D2260/98F16H1/28
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 10,415,693
App. No.
15/384,179
Granted
Sep 17, 2019
Kind
B2
Abstract

An oil transfer assembly supplies oil into a moving, rotating tube extending along an axis. The assembly is provided with a support plate transversal to the axis and a sleeve, which is angularly fixed with respect to the support plate, it is configured to be coupled in a sliding and watertight way to a terminal section of the inlet of said tube and has at least one chamber for transferring oil into said terminal section of the inlet. The assembly is also equipped with at least two tubular bodies, which project axially from the support plate, define between them an annular channel communicating with the chamber and join the sleeve to the support plate in a watertight manner and with clearances so as to leave freedom of orientation of the sleeve around any direction orthogonal to the axis.

Claims (37)

1. An oil transfer assembly for supplying oil into a rotating and translating tube extending along an axis; the assembly comprising:

a support plate transverse to said axis and defined by a planet-carrier of an epicycloidal transmission;

a sleeve angularly fixed with respect to said support plate about said axis, wherein the sleeve is configured to be coupled in a sliding and fluid-tight manner to an end inlet portion of said tube, and defines at least one chamber for transferring oil into said end inlet portion; and

at least a first and a second tubular body which project axially from said support plate, delimit between each other an annular channel communicating with said chamber, and couple said sleeve to said support plate in a fluid-tight manner and with coupling clearances so as to leave freedom of orientation to said sleeve about any direction orthogonal to said axis.

2. An assembly according to claim 1 , wherein said coupling clearances are provided:

between said first tubular body and an axial end of said sleeve; and

between a first end portion of said second tubular body and said support plate.

3. An assembly according to claim 2 , wherein said first tubular body is fixed to said support plate.

4. An assembly according to claim 3 , wherein said first tubular body comprises a first shoulder arranged about a second end portion of said second tubular body and defining a rest, in radial direction, for said second end portion.

5. An assembly according to claim 3 , wherein said first tubular body comprises a second shoulder axially facing a second end portion of said second tubular body for axially retaining said second tubular body.

6. An assembly according to claim 2 , further comprising an axial stop element facing axially said first tubular body and fixed to said first tubular body so as to axially retain said axial end with axial clearance.

7. An assembly according to claim 6 , wherein said axial end comprises an external flange which is axially bound, with said axial clearance, between said first tubular body and said axial stop element.

8. An assembly according to claim 6 , further comprising an anti-rotation device acting between said sleeve and said first tubular body.

9. A turbo-propeller engine comprising:

an epicycloidal transmission;

a drive shaft extending along an axis and driven by said epicycloidal transmission to rotate about said axis;

a propeller supported and actuated by said drive shaft to rotate about said axis and having a rotating and translating tube, which extends along said axis and comprises an end inlet portion arranged in said drive shaft; and

an oil transfer assembly as defined in claim 1 .

10. An oil transfer assembly for supplying oil into a rotating and translating tube extending along an axis; the assembly comprising:

a support plate transverse to said axis;

a sleeve angularly fixed with respect to said support plate about said axis, wherein the sleeve is configured to be coupled in a sliding and fluid-tight manner to an end inlet portion of said tube, and defines at least one chamber for transferring oil into said end inlet portion; and

at least a first and a second tubular body which project axially from said support plate, delimit between each other an annular channel communicating with said chamber, and couple said sleeve to said support plate in a fluid-tight manner and with coupling clearances so as to leave freedom of orientation to said sleeve about any direction orthogonal to said axis, said coupling clearances being provided between said first tubular body and an axial end of said sleeve and between a first end portion of said second tubular body and said support plate, and said first tubular body being fixed to said support plate and comprising a first shoulder arranged about a second end portion of said second tubular body and defining a rest, in radial direction, for said second end portion.

11. An assembly according to claim 10 , wherein said support plate is defined by a planet-carrier of an epicycloidal transmission.

12. An assembly according to claim 10 , wherein said first tubular body comprises a second shoulder axially facing a second end portion of said second tubular body for axially retaining said second tubular body.

13. An assembly according to claim 10 , further comprising an axial stop element facing axially said first tubular body and fixed to said first tubular body so as to axially retain said axial end with axial clearance.

14. An assembly according to claim 13 , wherein said axial end comprises an external flange which is axially bound, with said axial clearance, between said first tubular body and said axial stop element.

15. An assembly according to claim 10 , further comprising an anti-rotation device acting between said sleeve and said first tubular body.

16. An oil transfer assembly for supplying oil into a rotating and translating tube extending along an axis; the assembly comprising:

a support plate transverse to said axis;

a sleeve angularly fixed with respect to said support plate about said axis, wherein the sleeve is configured to be coupled in a sliding and fluid-tight manner to an end inlet portion of said tube, and defines at least one chamber for transferring oil into said end inlet portion; and

at least a first and a second tubular body which project axially from said support plate, delimit between each other an annular channel communicating with said chamber, and couple said sleeve to said support plate in a fluid-tight manner and with coupling clearances so as to leave freedom of orientation to said sleeve about any direction orthogonal to said axis, said coupling clearances being provided between said first tubular body and an axial end of said sleeve and between a first end portion of said second tubular body and said support plate;

an axial stop element facing axially said first tubular body and fixed to said first tubular body so as to axially retain said axial end with axial clearance; and

an anti-rotation device acting between said sleeve and said first tubular body.

17. An assembly according to claim 16 , wherein said first tubular body is fixed to said support plate.

18. An assembly according to claim 17 , wherein said first tubular body comprises a first shoulder arranged about a second end portion of said second tubular body and defining a rest, in radial direction, for said second end portion.

19. An assembly according to claim 16 , wherein said axial end comprises an external flange which is axially bound, with said axial clearance, between said first tubular body and said axial stop element.

20. An assembly according to claim 16 , wherein said support plate is defined by a planet-carrier of an epicycloidal transmission.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 19, 2016
From: ALTAMURA, PAOLO
To: GE AVIO S.R.L.
Reel/Frame 040676/0078 →
Priority Claims (1)
IT 102015000086684 · Dec 22, 2015 · national
Continuity (1)
Related Publication 20170175877A1 · Jun 22, 2017
Cited By (1)
US 12,747,670