Lubrication system for gas turbine engines

• US 10,107,197 B2
• Filed: 11/30/2012
• Issued: 10/23/2018
• Est. Priority Date: 11/30/2012
• Status: Active Grant

• Current Assignee: Rtx Corporation
• Original Assignee: United Technologies Corporation (Rtx Corporation)
• Inventors: Parnin, Francis, Dolman, Paul H., Daley, David M., James, Denman H., Clark, Richard W.
• Primary Examiner(s): Rodriguez, William H
• Assistant Examiner(s): Duger, Jason H
• Application Number:
  US13/690,767
• Publication Number:
  US 20140150439A1
• Time in Patent Office: 2,153 Days
• Field of Search: 60 3908, 184 611
• CPC Class Codes: F01D 25/20 using lubrication pumps
• CPC Class Codes: F02C 7/06 Arrangements of bearings bearings F16C; Lubricating of turbo machines F01D25/18; of machines or engines in general F01M
• CPC Class Codes: F05D 2270/301 Pressure
• CPC Class Codes: F05D 2270/304 Spool rotational speed
• CPC Class Codes: F05D 2270/331 Mechanical loads
• CPC Class Codes: F05D 2270/332 Maximum loads or fatigue criteria
• CPC Class Codes: F05D 2270/335 Output power or torque
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

A lubrication system is provided. The lubrication system may be used in conjunction with a gas turbine engine for generating power or lift. The lubrication system utilized a flow scheduling valve which reduces lubricant flow to at least one component based on an engine load. The lubrication system may further include a main pump which may be regulated by an engine speed. Thus, a lubrication system which provides a lubricant to engine components based on the load and speed of the engine is possible. The system may improve efficiency of the engine by reducing the power previously spent in churning excess lubricant by at least one engine component as well as reducing the energy used by a lubricant cooler in cooling the excess lubricant. The lubricant cooler size may also be minimized to reduce weight and air drag due to the reduced lubricant flow.

Claims

1. A lubrication system for a gas turbine engine having a fan and a combustor, the system comprising:

a main pump, a flow scheduling valve, and a main conduit fluidly connecting the main pump and the flow scheduling valve, the main pump moving a lubricant through the main conduit from a lubricant tank to the flow scheduling valve,

a first engine component fluidly connected by a first primary conduit to the flow scheduling valve, a second engine component fluidly connected by a second primary conduit to the flow scheduling valve, wherein the main pump moves the lubricant to the flow scheduling valve; and

a processor connected to each of the main pump, the flow scheduling valve and at least one sensor that provides at least one measured value,

the processor configured to;

receive the at least one measured value from the at least one sensor,

calculate an engine load based on the at least one measured value,

regulate the main pump to selectively control the moving of the lubricant to the flow scheduling valve according to an operational speed of the engine,

selectively control the flow scheduling valve to proportionally reduce flow of the lubricant to both the first engine component and the second engine component in response to detecting a reduced value of the calculated engine load, and

wherein the at least one sensor includes a pressure sensor providing a measured pressure of the combustor and a speed sensor providing a measured speed of the fan, and wherein the at least one measured value includes the measured pressure and the measured speed.

2. The lubrication system of claim 1, further comprising a lubricant cooler connected to the main conduit.

3. The lubrication system of claim 2, wherein the lubricant cooler is positioned between the main pump and the flow scheduling valve.

4. The lubrication system of claim 1, further comprising a fixed flow metering orifice allowing the lubricant to bypass the first engine component and the second engine component via a bypass conduit and to return to the lubricant tank.

5. The lubrication system of claim 1, further comprising a manifold positioned in the main conduit between the main pump and the flow scheduling valve, the manifold being connected to a third engine component via a side conduit to allow the third engine component to receive a portion of the lubricant not reduced by the flow scheduling valve.

6. The lubrication system of claim 1 further comprising a first scavenge conduit fluidly connecting the first engine component and the second engine component to each other and to the lubricant tank.

7. A gas turbine engine comprising:

a fan and a combustor,

and

a lubrication system, the lubrication system comprising;

a lubrication tank;

a main conduit in fluid communication with the lubrication tank;

a main pump, a flow scheduling valve, and the main conduit fluidly connecting the main pump and the flow scheduling valve, the main pump moving a lubricant through the main conduit from the lubricant tank to the flow scheduling valve,

a first engine component fluidly connected by a first primary conduit to the flow scheduling valve, a second engine component fluidly connected by a second primary conduit to the flow scheduling valve; and

a processor connected to each of the main pump, the flow scheduling valve and at least one sensor that provides at least one measured value, the processor configured to;

receive the at least one measured value from the at least one sensor,

calculate an engine load based on the at least one measured value,

regulate the main pump to selectively control the moving of the lubricant to the flow scheduling valve according to an operational speed of the engine, and

selectively control the flow scheduling valve to proportionally reduce flow of the lubricant both the first engine component and the second engine component in response to detecting a reduced value of the calculated engine load, and

wherein the at least one sensor includes a pressure sensor providing a measured pressure of the combustor and a speed sensor providing a measured speed of the fan, and wherein the at least one measured value includes the measured pressure and the measured speed.

8. The gas turbine engine of claim 7, wherein the main pump is driven by a drivetrain.

9. The gas turbine engine of claim 7, further comprising a lubricant cooler connected to the main conduit.

10. The gas turbine engine of claim 7, further comprising a manifold positioned in the main conduit between the lubricant tank and the flow scheduling valve and connected to a third engine component via a side conduit, the manifold allowing the third engine component to receive a portion of the lubricant not reduced by the flow scheduling valve.

14. The gas turbine engine of claim 7 further comprising a first scavenge conduit fluidly connecting the first engine component and the second engine component to each other and to the lubricant tank.

11. A method of lubricating a first component and a second component of a gas turbine engine, the gas turbine engine having a fan and a combustor, comprising:

moving a lubricant through a main conduit from a lubricant tank to a flow scheduling valve by a main pump, the main conduit fluidly connecting the main pump and the flow scheduling valve,

fluidly connecting the first component to the flow scheduling valve with a first primary conduit,

fluidly connecting the second component to the flow scheduling valve with a second primary conduit,

moving the lubricant to the flow scheduling valve with the main pump, and

providing at least one measured value from at least one sensor to a processor, the processor connected to each of the main pump, the flow scheduling valve, and the at least one sensor,

calculating an engine load with the processor based on the at least one measured value,

regulating the main pump with the processor to selectively control the moving of the lubricant through the main conduit from the lubricant tank to the flow scheduling valve according to an operational speed of the gas turbine engine,

selectively controlling the flow scheduling valve with the processor to proportionally reduce flow of the lubricant to both the first component and the second component in response to detecting a reduced value of the calculated engine load with the processor, and

wherein the at least one sensor includes a pressure sensor providing a measured pressure of the combustor and a speed sensor providing a measured speed of the fan, and wherein the at least one measured value includes the measured pressure and the measured speed.

12. The method of claim 11, further comprising directing an excess portion of the lubricant through a return conduit to the lubricant tank.

13. The method of claim 11, further comprising redirecting a portion of the lubricant from the main conduit through a bypass conduit to the lubricant tank.