Coupling and a method of using the same

Patent metadata

Field	Value
Publication number	US-2016102751-A1
Application number	US-201514848595-A
Country	US
Kind code	A1
Filing date	Sep 9, 2015
Priority date	Oct 9, 2014
Publication date	Apr 14, 2016
Grant date	—

Abstract

A fluid transfer coupling includes a first and second shaft assembly. The first shaft assembly includes a shaft and annular fin attached to shaft, annular fin having one or more internal passages extending therethrough. The or each internal passage connects a centre portion of shaft to a radially outwardly facing side of annular fin. The second shaft assembly includes a shaft and annular trough extending radially outwardly of shaft. The first shaft is concentrically accommodated within second shaft with annular fin being accommodated within annular trough. In use, first shaft assembly rotates at a first rotational speed and second shaft assembly rotates at a second rotational speed, with second rotational speed being greater than first rotational speed. The difference between second and first rotational speeds cause a fluid contained within annular trough to be driven radially inwardly through the or each internal passage to centre portion of first shaft.

First claim

What is claimed is:

1 . A fluid transfer coupling comprising:
a first shaft assembly; and a second shaft assembly, the first shaft assembly comprising: a first shaft; and an annular fin attached to the first shaft, the annular fin having one or more internal passages extending therethrough, the or each internal passage connecting a centre portion of the first shaft to a radially outwardly facing side of the annular fin, the second shaft assembly comprising: a second shaft; and an annular trough extending radially outwardly of the second shaft, wherein the first shaft is concentrically accommodated within the second shaft with the annular fin accommodated within the annular trough, and in use, the first shaft assembly rotates at a first rotational speed and the second shaft assembly rotates at a second rotational speed, the second rotational speed being greater than the first rotational speed, the difference between the second rotational speed and the first rotational speed causes a fluid contained within the annular trough to be driven radially inwardly through the or each internal passage to the centre portion of the first shaft.

2 . The fluid transfer coupling as claimed in claim 1 , wherein the or each passage comprises a single annular volume.

3 . The fluid transfer coupling as claimed in claim 1 , wherein the or each passage comprises a plurality of radially extending holes.

4 . The fluid transfer coupling as claimed in claim 1 , wherein the ratio of the second rotational speed to the first rotational speed is between approximately 6:1 and 2:1.

5 . The fluid transfer coupling as claimed in claim 1 , wherein the ratio of the second rotational speed to the first rotational speed is between approximately 5:1 and 3:1.

6 . The fluid transfer coupling as claimed in claim 1 , wherein the ratio of the second rotational speed to the first rotational speed is approximately 3:1.

7 . The hydraulic coupling as claimed in claim 1 , wherein the first shaft assembly rotates in an opposite direction to the second shaft assembly.

8 . The fluid transfer coupling as claimed in claim 1 , wherein the or each internal passage comprises one or more radially extending first vanes arranged within the respective passage.

9 . The fluid transfer coupling as claimed in claim 1 , wherein the annular trough comprises a plurality of radially extending second vanes projecting axially into a volume defined by the annular trough.

10 . The fluid transfer coupling as claimed in claim 1 , wherein the or each internal passage has an axial dimension of between approximately 0.5 mm and 3 mm.

11 . The fluid transfer coupling as claimed in claim 1 , wherein the or each internal passage has an axial dimension of between approximately 0.5 mm and 1.5 mm.

12 . A method of using a fluid transfer coupling, the fluid transfer coupling comprising a first shaft assembly and a second shaft assembly, the first shaft assembly comprising a first shaft and an annular fin attached to the first shaft, the annular fin having one or more internal passages extending therethrough, the or each internal passage connecting a centre portion of the first shaft to a radially outwardly facing side of the annular fin, the second shaft assembly comprising a second shaft and an annular trough extending radially outwardly of the second shaft, the method comprising the steps of:
(i) arranging the first shaft assembly concentrically within the second shaft assembly; (ii) driving the first shaft assembly at a first rotational speed and the second shaft assembly at a second rotational speed; (iii) introducing a supply of fluid to the annular trough; and (iv) the difference between the second rotational speed and the first rotational speed causing the fluid to be driven radially inwardly from the trough through the or each internal passage to the centre of the first shaft.

13 . The method as claimed in claim 12 , wherein step (ii) comprises the step of:
(ii)′ driving the first shaft assembly at a first rotational speed and the second shaft assembly at a second rotational speed, and the ratio of the second rotational speed to the first rotational speed is between approximately 6:1 and 2:1.

14 . The method as claimed in claim 12 , wherein step (ii) comprises the step of:
(ii)″ driving the first shaft assembly at a first rotational speed and the second shaft assembly at a second rotational speed, and the ratio of the second rotational speed to the first rotational speed is between approximately 5:1 and 3:1.

15 . The method as claimed in claim 12 , wherein step (ii) comprises the step of:
(ii)′″ driving the first shaft assembly at a first rotational speed and the second shaft assembly at a second rotational speed, and the ratio of the second rotational speed to the first rotational speed is approximately 4:1.

Assignees

• Rolls Royce Plc

Inventors

• Scothern David Peter

Classifications

• F16C2360/23

  Gas turbine engines · CPC title

• F04D1/003

  Having contrarotating parts · CPC title

• F04D1/02 Primary

  having non-centrifugal stages, e.g. centripetal · CPC title

• F16H57/0434 Primary

  relating to lubrication supply, e.g. pumps; Pressure control · CPC title

• F16H57/0471

  Bearing · CPC title