Turbine starter lubricant cooling

• US 8,910,463 B2
• Filed: 02/22/2010
• Issued: 12/16/2014
• Est. Priority Date: 02/22/2010
• Status: Active Grant

• Current Assignee: Hamilton Sundstrand Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Hamilton Sundstrand Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Telakowski, Robert
• Primary Examiner(s): Gartenberg, Ehud
• Assistant Examiner(s): Duger, Jason H
• Application Number:
  US12/709,961
• Publication Number:
  US 20110203249A1
• Time in Patent Office: 1,758 Days
• Field of Search: 60/390.8, 60/398.3, 607/86, 184/6.11, 184/6.3, 184/65, 310/54, 244/53.A
• US Class Current: 60/39.83
• CPC Class Codes: F01D 25/18 Lubricating arrangements of machines or engines in general F01M
• CPC Class Codes: F02C 7/14 of fluids in the plant , e.g. lubricant or fuel F02C7/185 takes precedence
• CPC Class Codes: F02C 7/277 the starter being a separate turbine
• CPC Class Codes: F05D 2260/205 Cooling fluid recirculation, i.e. after cooling one or more components is the cooling fluid recovered and used elsewhere for other purposes
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

A cooling system for turbine starter lubricant includes one or more outflow transfer passages (54) extending from the turbine starter (10) to a secondary component (40). At least one heat exchange passage (56) affixed at a first end to an end of an outflow transfer passage (54) of the one or more outflow transfer passages (54), is located in the secondary component (40) having a lower interior temperature than the turbine starter (10). One or more return transfer passages (60) are affixed to a second end of the at least one heat exchange passage (56) and extend from the secondary component (40) to the turbine starter (10). Flowing a volume of starter lubricant (42) through the one or more outflow transfer passages (54), the at least one heat exchange passage (56), and the one or more return transfer passages (60) removes thermal energy from the volume of starter lubricant (42) and returns the volume of starter lubricant (42) to the turbine starter (10).

Claims

1. A cooling system for turbine starter lubricant comprising:

one or more outflow transfer passages extending from a compressed gas driven turbine starter to a gearbox assembly;

at least one heat exchange passage extending through the gearbox assembly at least partially vertically, affixed at a first end to an end of an outflow transfer passage of the one or more outflow transfer passages, the gearbox assembly having a lower interior temperature than the turbine starter during operation;

one or more return transfer passages affixed to a second end of the at least one heat exchange passage and extending from the gearbox assembly to the turbine starter, whereby flowing a volume of starter lubricant through the one or more outflow transfer passages, the at least one heat exchange passage, and the one or more return transfer passages removes thermal energy from the volume of starter lubricant and returns the volume of starter lubricant to the turbine starter, the one or more return transfer passages are disposed inside the turbine starter at a higher elevation than the one or more outflow transfer passages; and

an internal pump disposed inside a turbine starter housing to circulate the volume of starter lubricant through the at least one heat exchange passage;

wherein thermal energy is removed from the starter lubricant via transfer from the starter lubricant flowing through the at least one heat exchange passage to a gearbox coolant circulating in the gearbox assembly at an exterior of the at least one heat exchange passage.

2. The cooling system of claim 1 wherein the at least one heat exchange passage includes a plurality of fins extending therefrom to increase heat transfer.

3. The cooling system of claim 1 wherein flow of the volume of starter lubricant through the cooling system is driven by gravitation forces.

4. The cooling system of claim 1 including at least one lubricant trough disposed at the one or more outflow passages to collect the volume of starter lubricant for cooling.

5. The cooling system of claim 1 wherein the turbine starter utilizes splash lubricant circulation.

6. A method of cooling lubricant comprising:

flowing a volume of starter lubricant from a compressed gas driven turbine starter to a gearbox assembly via one or more outlet transfer passages by operation of an internal pump disposed inside the turbine starter;

flowing the volume of starter lubricant through at least one heat exchange passage extending through the gearbox assembly at least partially vertically, the gearbox assembly having a lower interior temperature than the turbine starter during operation, thereby removing thermal energy from the volume of starter lubricant via thermal energy transfer from the starter lubricant flowing through the at least one heat exchange passage to a gearbox coolant circulating in the gearbox assembly at an exterior of the at least one heat exchange passage; and

returning the volume of starter lubricant to the turbine starter via one or more return transfer passages;

wherein the one or more return transfer passages are disposed inside the turbine starter at a higher elevation than the one or more outflow transfer passages.

7. The method of claim 6 including dissipating thermal energy from the volume of starter lubricant via a plurality of fins extending from the at least one heat exchange passage to increase heat transfer.

8. The method of claim 6 including impinging the gearbox coolant on the at least one heat exchange passage to remove thermal energy from the volume of starter lubricant.

9. The method of claim 6 including flowing the volume of starter lubricant through the cooling system via gravitational forces.

10. The method of claim 6 including collecting the volume of starter lubricant for cooling in at least one lubricant trough disposed at the one or more outflow transfer passages.

11. The method of claim 6 including circulating the volume of starter lubricant throughout the turbine starter via rotation of elements of the turbine starter.