Oil tank filling system

Patent metadata

Field	Value
Publication number	US-11174755-B2
Application number	US-201916387836-A
Country	US
Kind code	B2
Filing date	Apr 18, 2019
Priority date	May 2, 2018
Publication date	Nov 16, 2021
Grant date	Nov 16, 2021

Abstract

An oil tank filling system for filling the oil tank of a gas turbine engine. The system includes an oil tank located within the core of the engine, an engine oil filling port located on a bifurcation below the core of the engine, and an oil tank filling pipe that leads from the engine oil filling port to a tank filling port on the oil tank. The engine oil filling port is detachably connectable to an off-engine oil pump that when connected to the engine oil filling port and supplied with oil pumps oil into the engine oil filling port and through the oil tank filling pipe to the tank filling port to fill the oil tank. A method of filling the oil tank of a gas turbine engine and a gas turbine engine that includes the oil tank filling system are also disclosed.

First claim

We claim:

1. An oil tank filling system for filling an oil tank of a gas turbine engine, the system comprises:
an oil tank located within a core of the engine;
an engine oil filling port located on a bifurcation below the core of the engine; and
an oil tank filling pipe that leads from the engine oil filling port to a tank filling port on the oil tank;
wherein the engine oil filling port is detachably connectable to an off-engine oil pump that when connected to the engine oil filling port and supplied with oil pumps oil into the engine oil filling port and through the oil tank filling pipe to the tank filling port to fill the oil tank.

2. The oil tank filling system of claim 1 wherein the oil tank has an oil tank top and an oil tank bottom and the tank filling port is located on or adjacent the oil tank top.

3. The oil tank filling system of claim 2 wherein the oil tank top is located directly beneath an outlet guide vane of the gas turbine engine, and the oil tank bottom is located directly above another outlet guide vane of the gas turbine engine.

4. The oil tank filling system of claim 1 wherein the oil tank is shaped to curve around one or both sides of the engine within the core of the engine.

5. The oil tank filling system of claim 1 wherein the oil tank is located between opposing outlet guide vanes.

6. The oil tank filling system of claim 1 wherein the bifurcation has a bifurcation base that is attached to a fan case, which is covered by a fan nacelle, and the engine oil filling port is located on the bifurcation base and accessed through an opening in the fan nacelle.

7. The oil tank filling system of claim 1 wherein one or more temperature and/or pressure sensors are provided alongside one or more sections of the oil tank filling pipe and communicate with a controller to provide an alert should the oil tank filling pipe burst or become blocked.

8. A gas turbine engine that includes the oil tank filling system of claim 1 .

9. The gas turbine engine of claim 8 for an aircraft wherein the gas turbine engine comprises an engine core comprising a turbine, a compressor, and a core shaft connecting the turbine to the compressor; a fan located upstream of the engine core, the fan comprising a plurality of fan blades and a gearbox that receives an input from the core shaft and outputs drive to the fan so as to drive the fan at a lower rotational speed than the core shaft.

10. A method of filling an oil tank of a gas turbine engine that is located within a core of the engine, the method comprising the steps of:
connecting an off-engine oil pump to an engine oil filling port located on a bifurcation below the core of the engine; and
pumping oil from the off-engine oil pump into the engine oil filling port and through an oil tank filling pipe that leads from the engine oil filling port to a tank filling port on the oil tank that is located within the core of the engine.

Assignees

• Rolls Royce Plc

Inventors

• White Samuel W
• Malewicz William A
• Ray Sebastian
• Diaz Garcia Cristina

Classifications

• F02C7/20

  Mounting or supporting of plant; Accommodating heat expansion or creep · CPC title

• F16N2210/02

  Turbines · CPC title

• F01D9/065

  Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids (see also F01D25/16, F01D25/24 and F01D25/26) · CPC title

• F05D2230/72

  Maintenance · CPC title

• B64D37/16

  Filling systems (ground installations for fuelling aircraft B64F1/28) · CPC title