Rotating fluid pumping system

Patent metadata

Field	Value
Publication number	US-9260980-B2
Application number	US-201213365605-A
Country	US
Kind code	B2
Filing date	Feb 3, 2012
Priority date	Mar 17, 2011
Publication date	Feb 16, 2016
Grant date	Feb 16, 2016

Abstract

A mechanism such as a rotor of an open rotor gas turbine engine comprises a rotor assembly 100 rotatable about a rotational axis A. The rotor assembly 100 has a fluid pathway 110 including a pump 114 carried by the first rotor assembly 100 for driving fluid along the fluid pathway 110 . The fluid may be oil for lubricating components of the mechanism. The fluid is collected by an annular channel-shaped collector 111 and pumped through surface coolers 116 to an outlet pipe 119 . From the pipe 119 the fluid migrates along a path 500 under centrifugal force, returning to the collector 111.

First claim

The invention claimed is:

1. A gas turbine engine oil scavenge mechanism comprising a first rotor assembly rotatable about a rotational axis, the first rotor assembly having: a fluid pathway, and a pump for driving oil along the fluid pathway, wherein the fluid pathway and the pump are separate elements, the fluid pathway and the pump are in fluid communication, the fluid pathway and the pump are provided in the first rotor assembly and together form a cycle that allows the driving oil to be scavenged and returned, and the cycle resides entirely within the first rotor assembly and the cycle rotates entirely about the rotational axis with the first rotor assembly.

2. A gas turbine engine oil scavenge mechanism according to claim 1 in which the fluid pathway comprises a fluid collector, and in which the pump has an inlet communicating with the fluid collector, the fluid collector being situated away from the rotational axis of the first rotor assembly.

3. A gas turbine engine oil scavenge mechanism according to claim 2 in which the fluid collector is an annular radially inwardly opening channel centred on the rotational axis.

4. A gas turbine engine oil scavenge mechanism according to claim 2 in which there is a flow restrictor between the fluid collector and the pump.

5. A gas turbine engine oil scavenge mechanism according to claim 2 in which the pump has an outlet which communicates via a portion of the fluid pathway to a region of the mechanism situated radially inwardly of the collector.

6. A gas turbine engine oil scavenge mechanism according to claim 1 in which the fluid pathway comprises at least one surface cooler which is exposed at an external surface of the first rotor assembly.

7. A gas turbine engine oil scavenge mechanism according to claim 6 in which the at least one surface cooler is one of at least two surface coolers which are distributed about the rotational axis, the pump being disposed circumferentially between the surface coolers or between two adjacent surface coolers.

8. A gas turbine engine oil scavenge mechanism according to claim 1 wherein components of the fluid pathway are distributed about the rotational axis of the first rotor assembly to balance the first rotor assembly during rotation.

9. A gas turbine engine oil scavenge mechanism according to claim 1 further comprising a drive shaft mounted in the first rotor assembly for driving the pump, the drive shaft extending radially with respect to the rotational axis of the first rotor assembly.

10. A gas turbine engine oil scavenge mechanism according to claim 1 , further comprising a second rotor assembly, which is rotatable about the rotational axis.

11. A gas turbine engine oil scavenge mechanism according to claim 10 in which a drive shaft is driven by relative rotation between the first rotor assembly and the second rotor assembly.

12. A gas turbine engine oil scavenge mechanism as claimed in claim 10 , in which the first and second rotor assemblies are drivable by an epicyclic gear mechanism in which the first rotor assembly is mounted for rotation with an annulus gear of the epicyclic gear mechanism and the second rotor assembly is mounted for rotation in the opposite direction with a planet carrier of the epicyclic gear mechanism.

13. A gas turbine engine oil scavenge mechanism according to claim 12 , in which a drive shaft for driving the pump is drivingly connected to the planet carrier by a bevel gear arrangement.

14. A gas turbine engine oil scavenge mechanism according to claim 10 wherein the mechanism further comprises at least one weir mounted on either the first or second rotor assembly, the weir being arranged such that, when the rotor assemblies are rotating, the oil flows radially outwardly over the weir between the rotor assemblies.

15. A gas turbine engine comprising a propeller and an oil scavenge mechanism according to claim 1 .

Assignees

• Leese Robert E
• Rolls Royce Plc

Inventors

• Leese Robert E

Classifications

• F01D25/20 Primary

  using lubrication pumps · CPC title

• F02C7/14

  of fluids in the plant {, e.g. lubricant or fuel (F02C7/185 takes precedence)} · CPC title

• F01D25/18

  Lubricating arrangements (of machines or engines in general F01M) · CPC title

• Y02T50/675

  Cross-Sectional Technologies · mapped topic

• F02C3/067

  having counter-rotating rotors (F02C3/073 takes precedence) · CPC title