Supplemental lubrication pressurized by component or reservoir rotation

Patent metadata

Field	Value
Publication number	US-10697586-B2
Application number	US-201715684920-A
Country	US
Kind code	B2
Filing date	Aug 23, 2017
Priority date	Aug 23, 2017
Publication date	Jun 30, 2020
Grant date	Jun 30, 2020

Abstract

An example lubrication system for a rotating component has a primary lubrication system providing continuous lubrication during normal operation of the rotating component and secondary lubrication system with a reservoir co-rotating with the component. The reservoir is continuously replenished from the primary lubrication system during normal operation of the rotating system, with the lubricant being forced through a discharge orifice by the centrifugal force generated by the rotation toward, for example, a bearing or a gear. When the primary pressurized lubrication system fails, lubrication will continue to be provided by the lubricant in the supplemental lubricant reservoir while the rotation speed or power supplied to the shaft is controllably decreased in an emergency.

First claim

What is claimed is:

1. A lubrication system for a substantially vertically installed rotating component constructed as a hollow shaft, comprising:
a primary lubrication system comprising a lubricant pump and continuously supplying a lubricant to the rotating component independent of rotation of the rotating component; and
a secondary lubrication system arranged inside the rotating component and comprising a lubricant reservoir having an outer wall of the rotating component and an inner wall and a closed bottom and defining an enclosed volume, wherein the lubricant reservoir co-rotates with the rotating component about a substantially vertical axis and receives lubricant from the primary lubrication system at a top opening and discharges a metered quantity of the lubricant through an orifice disposed proximate to the bottom of the lubricant reservoir, wherein
when the primary lubrication system fails to supply the lubricant to the rotating component, a centrifugal force generated by rotation of the rotating component and acting on the lubricant in the co-rotating lubricant reservoir pushes the metered quantity through the orifice and supplies the metered quantity of the lubricant to the rotating component while the rotation of the rotating component is controllably decreased and ultimately stopped.

2. The lubrication system of claim 1 , wherein the lubricant reservoir of the secondary lubrication system is sized so as to supply the metered quantity of the lubricant to the rotating component while the rotation speed of the shaft is controllably decreased.

3. The lubrication system of claim 1 , wherein the rotating component is supported for rotation by a bearing comprising an inner race connected to the rotating component and an outer race connected to a housing, with the metered quantity of the lubricant being conveyed to the inner race through the orifice.

4. The lubrication system of claim 1 , wherein the rotating component is supported for rotation in a housing by at least one bearing.

5. The lubrication system of claim 4 , wherein the housing is closed off at a housing bottom forming an oil pan or a sump.

6. The lubrication system of claim 5 , wherein the lubricant pump draws lubricant from the oil pan or sump.

7. The lubrication system of claim 4 , wherein the lubricant pump is arranged inside the housing.

8. The lubrication system of claim 5 , wherein the lubricant is continuously supplied to the lubricant reservoir from the oil pan or sump through a supplemental feed line which keeps the lubricant reservoir filled during normal operation.

9. A method for lubricating a substantially vertically installed rotating component constructed as a hollow shaft, the method comprising:
supplying a lubricant to the rotating component from a primary lubrication system comprising a lubricant pump independent of rotation of the rotating component; and
discharging a metered quantity of the lubricant through an orifice disposed proximate to a closed bottom of in a lubricant reservoir defined by an outer wall of the rotating component and an inner wall and the closed bottom of a secondary lubrication system, wherein the lubricant reservoir is arranged inside the rotating component and co-rotates with the rotating component about a substantially vertical axis and receives lubricant from the primary lubrication system at a top opening and, wherein
when the primary lubrication system fails to supply the lubricant to the rotating component, a centrifugal force generated by rotation of the rotating component and acting on the lubricant in the co-rotating lubricant reservoir pushes the metered quantity through the orifice and supplies the metered quantity of the lubricant to the rotating component while the rotation of the rotating component is controllably decreased and ultimately stopped.

10. The method of claim 9 , wherein the lubricant reservoir of the secondary lubrication system is sized so as to supply the metered quantity of the lubricant to the rotating component while the rotation speed of the shaft is controllably decreased.

11. The method of claim 9 , wherein the rotating component is supported for rotation by a bearing comprising an inner race connected to the rotating component and an outer race connected to a housing, with the metered quantity of the lubricant being conveyed to the inner race through the orifice.

12. The method of claim 9 , wherein the rotating component is supported for rotation in a housing by at least one bearing.

13. The method of claim 12 , wherein the housing is closed off at a housing bottom forming an oil pan or a sump.

14. The method of claim 13 , wherein the lubricant pump draws lubricant from the oil pan or sump.

15. The method of claim 12 , wherein the lubricant pump is arranged inside the housing.

16. The method of claim 13 , wherein the lubricant is continuously supplied to the lubricant reservoir from the oil pan or sump through a supplemental feed line which keeps the lubricant reservoir filled during normal operation.

17. A rotorcraft comprising:
at least one substantially vertically installed rotating component constructed as a hollow shaft,
a primary lubrication system comprising a lubricant pump and continuously supplying a lubricant to the at least one rotating component independent of rotation of the at least one rotating component; and
a secondary lubrication system arranged inside the rotating component and comprising a lubricant reservoir defined by an outer wall of the rotating component and an inner wall and a closed bottom, wherein the lubricant reservoir co-rotates with the rotating component about a substantially vertical axis and receives lubricant from the primary lubrication system at a top opening and discharges a metered quantity of the lubricant through an orifice disposed proximate to the bottom of the lubricant reservoir, wherein
when the primary lubrication system fails to supply the lubricant to the rotating component, a centrifugal force generated by rotation of the rotating component and acting on the lubricant in the co-rotating lubricant reservoir pushes the metered quantity through the orifice and supplies the metered quantity of the lubricant to the rotating component while the rotation of the rotating component is controllably decreased and ultimately stopped.

18. The rotorcraft of claim 17 , wherein the lubricant reservoir of the secondary lubrication system is sized so as to supply the metered quantity of the lubricant to the rotating component while the rotation speed of the shaft is controllably decreased.

19. The rotor craft of claim 17 , wherein the rotating component is supported for rotation in a housing by at least one bearing.

20. The rotor craft of claim 17 , wherein the lubricant is continuously supplied to the lubricant reservoir from the oil pan or sump, keeping the lubricant reservoir filled during normal operation.

Assignees

• Bell Helicopter Textron Inc

Inventors

• Poster Scott David

Classifications

• F02C7/36 Primary

  Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user ({F02C3/107 - F02C3/13 and} F02C7/32 take precedence; couplings for transmitting rotation F16D; gearing in general F16H) · CPC title

• F16H57/0442

  for supply in case of failure, i.e. auxiliary supply · CPC title

• F16H57/0482

  Gearings with gears having orbital motion · CPC title

• F16H57/045

  Lubricant storage reservoirs, e.g. reservoirs in addition to a gear sump for collecting lubricant in the upper part of a gear case · CPC title

• F16H57/0427

  on rotary parts, e.g. using baffles for collecting lubricant by centrifugal force · CPC title