Lubrication system with prolonged loss of lubricant operation

• US 8,459,413 B2
• Filed: 01/19/2007
• Issued: 06/11/2013
• Est. Priority Date: 01/19/2007
• Status: Active Grant

• Current Assignee: Sikorsky Aircraft Corporation (Martin Marietta Corporation)
• Original Assignee: Sirkorsky Aircraft Corporation
• Inventors: Gmirya, Yuriy, Gelfand, Mikhail
• Primary Examiner(s): Mansen, Michael
• Assistant Examiner(s): RIEGELMAN, MICHAEL A
• Application Number:
  US12/522,268
• Publication Number:
  US 20100025159A1
• Time in Patent Office: 2,335 Days
• Field of Search: 184/6.4, 184/6.2, 184/6.22
• US Class Current: 184/6.4
• CPC Class Codes: B64C 27/12 Rotor drives
• CPC Class Codes: F01M 11/10 Indicating devices; Other safety devices
• CPC Class Codes: F01M 13/0011 Breather valves
• CPC Class Codes: F01M 2011/0045 for controlling the oil temperature
• CPC Class Codes: F01M 5/00 Heating, cooling, or controlling temperature of lubricant arrangement of lubricant coolers in engine cooling system F01P11/08; Lubrication means facilitating engine starting
• CPC Class Codes: F01M 5/002 Cooling
• CPC Class Codes: F16N 17/00 Lubrication of machines or apparatus working under extreme conditions additives to lubricating oil or lubricating grease C10M
• CPC Class Codes: F16N 2210/08 Aircraft
• CPC Class Codes: F16N 39/02 by cooling heat-exchangers in general F28

Abstract

A lubrication system includes an external pump system which pumps air out of the housing and develop negative pressure therein in response to a loss of lubrication condition. The negative pressure operates as an air lock to minimize or prevent lubricating oil loss from the housing while an internal lubrication system continues to distribute lubricating oil—which although now increasing in temperature—still operates to lubricate the gearbox components. For further ballistic tolerance, the housing is a compound housing that reduces or closes the penetration and further minimizes lubricating oil and negative pressure loss. The housing may be still further hardened by an armor layer.

Claims

1. A lubrication system to lubricate moving components comprising:

a housing defining a hot oil sump and a cold oil sump;

a heat exchanger system;

an external lubrication communication system to communicate a lubricating oil from said hot oil sump to said cold oil sump though said heat exchanger system;

an internal lubrication communication system to communicate the lubricating oil from said cold oil sump to the moving components;

a breather valve in communication with said housing, said breather valve in communication with said housing and atmospheric pressure; and

a controller to selectively close said breather valve and seal said housing from atmospheric pressure in response to a loss of lubricant condition indicated by a pressure sensor such that said external lubrication communication system develops a negative pressure within said housing.

2. The system as recited in claim 1, wherein the lubricating oil within said cold oil sump is received and interchanged from said hot oil sump during a normal operational condition.

3. The system as recited in claim 1, wherein said external lubrication communication system includes an external pump system within said hot oil sump.

4. The system as recited in claim 3, wherein said external pump system includes an intake line within said hot oil sump.

5. The system as recited in claim 4, wherein said external pump system communicates lubricating oil from said hot oil sump to said heat exchanger system, through a hot communication line to extract thermal energy from said lubricating oil, then communicates said lower temperature lubricating oil into said cold oil sump through a cold communication line.

6. The system as recited in claim 1, wherein said internal lubrication communication system includes an internal pump system within said cold oil sump.

7. The system as recited in claim 6, wherein said internal pump system communicates the lubricating oil to a multiple of oil jets within the housing.

8. The system as recited in claim 1, wherein said controller is in communication with a heat exchanger valve system.

9. The system as recited in claim 8, wherein said controller is in communication with said breather valve.

10. The system as recited in claim 8, wherein the pressure sensor is within a hot communication line between an external pump system and a heat exchanger.

11. The system as recited in claim 1, wherein said housing includes an inner housing and an outer housing which defines a gap therebetween, said gap filled with a resilient material.

12. The system as recited in claim 1, wherein said housing includes an armor layer.

13. The system as recited in claim 12, wherein said armor layer is adjacent to a lower surface of said housing.

14. The system as recited in claim 1, wherein said hot oil sump is located above said cold oil sump relative the moving components.

15. The system as recited in claim 1, wherein said hot oil sump is separated from said cold oil sump by a divider.

16. The system as recited in claim 15, wherein said divider wall includes a separator.

17. The system as recited in claim 1, wherein said housing includes a common divider wall between said cold oil sump and said hot oil sump.

18. A lubrication system to lubricate moving components comprising:

a housing defining a hot oil sump and a cold oil sump;

a breather valve in communication with said housing and atmospheric pressure; and

a controller to selectively close said breather valve and seal said housing from atmospheric pressure in response to a loss of lubricant condition indicated by a pressure sensor such that a negative pressure within said housing is developed.

19. The system as recited in claim 18, wherein said hot oil sump is separated from said cold oil sump by a divider.

20. The system as recited in claim 19, wherein said hot oil sump is located between said cold oil sump and the moving components.

21. The system as recited in claim 18, wherein the moving components include a power transmission of a rotary wing aircraft.

22. The system as recited in claim 18, wherein the moving components drive a main rotor system of a rotary wing aircraft.

23. The system as recited in claim 18, including:

a heat exchanger system;

an external lubrication communication system to communicate a lubricating oil from said hot oil sump to said cold oil sump though said heat exchanger system; and

an internal lubrication communication system to communicate the lubricating oil from said cold oil sump to the moving components, said external lubrication communication system operable to develop the negative pressure within said housing.

24. The system as recited in claim 18, wherein said housing includes a common divider wall between said cold oil sump and said hot oil sump.