Air turbine starter with fluid flow control

• US 6,681,579 B2
• Filed: 02/07/2002
• Issued: 01/27/2004
• Est. Priority Date: 02/07/2002
• Status: Expired due to Term

• Current Assignee: Honeywell International Inc., Seagate Technology LLC (Seagate Technology Holdings Plc)
• Original Assignee: Honeywell International Inc.
• Inventors: Geck, Kellan, Lane, Glenn H., Farnsworth, Gary A., Schroeder, Gerhard
• Primary Examiner(s): Richter, Sheldon J.
• Application Number:
  US10/071,175
• Publication Number:
  US 20030145602A1
• Time in Patent Office: 719 Days
• Field of Search: 607/88, 607/87, 607/78, 60/390.91
• US Class Current: 60/787
• CPC Class Codes: F01D 25/18 Lubricating arrangements of machines or engines in general F01M
• CPC Class Codes: F02C 7/277 the starter being a separate turbine
• CPC Class Codes: F05D 2260/85 Starting
• CPC Class Codes: F05D 2300/2283 of silicon
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

An improved air turbine starter that includes fluid flow control devices. The devices may be check valves, for example normally open check valves. The check valves may be located in fluid flow paths between the starter and the gearbox to which it is mounted. The starter may also include a ring seal about the output shaft to restrict fluid flow over the shaft.

Claims

1. A gas turbine engine combination comprising:

an air turbine starter including a cover plate and at least one passageway through the cover plate;

a gas turbine engine;

a gearbox adjacent the cover plate and between the air turbine starter and the gas turbine engine; and

a normally open valve in the at least one passageway through the cover plate.

2. The combination of claim 1 wherein the normally open valve is positioned in an oil return passage between the starter and the gearbox.

3. The combination of claim 1 wherein the valve includes a spring biased ball.

4. The combination of claim 1 wherein the valve includes a valve housing having a valve seat formed by a chamfer surface.

5. The combination of claim 1 wherein the first valve includes a valve ball within a valve housing having internal lands and grooves.

6. The combination of claim 5 wherein the first valve housing includes a chamfer surface forming a valve seat.

7. The combination of claim 1 further comprising a second normally open valve between the gearbox and the air turbine starter.

8. The combination of claim 7 wherein the second valve is positioned in a vent hole between the starter and the gearbox.

9. The combination of claim 8 wherein the first-recited valve is positioned in an oil return passage between the starter and the gearbox.

10. The combination of claim 1 wherein the valve includes a spring biased ball and a retaining element.

11. The combination of claim 10 wherein the retaining element includes a perforated wall.

12. The combination of claim 10 wherein the retaining element includes an annulus.

13. The combination of claim 12 wherein the valve includes a housing having a housing wall surrounding the ball wherein the housing wall includes at least one wall defining an opening.

14. An air turbine starter comprising:

an air turbine starter housing;

an output shaft extending from the air turbine starter housing;

a wall adjacent the turbine output shaft; and

a pressure valve in at least one of the air turbine starter housing and the wall wherein the valve is normally open under normal operating conditions for the turbine housing.

15. The air turbine starter of claim 14 wherein the air turbine starter has a normal internal operating pressure and the valve is configured to close when the internal operating pressure decreases below a given pressure.

16. The air turbine starter of claim 14 wherein the valve includes a plastic stopper.

17. The air turbine starter of claim 14 wherein the air turbine starter housing includes an oil return channel and wherein the valve is positioned adjacent the oil return channel.

18. The air turbine starter of claim 14 wherein the turbine housing includes an oil vent between the air turbine starter housing and a transmission housing and wherein the valve is positioned adjacent the oil vent.

19. The air turbine starter of claim 14 wherein the valve includes a spring biased ball.

20. The air turbine starter of claim 14 wherein the valve includes a valve housing having a perforated end wall.

21. The air turbine starter of claim 14 wherein the valve includes a valve housing having a perforated side wall.

22. The air turbine starter of claim 14 wherein the valve is placed in the housing of the air turbine starter.

23. The air turbine starter of claim 22 wherein the valve is placed in the a rear portion of the air turbine starter.

24. The air turbine starter of claim 23 wherein the valve is placed in the housing adjacent the a transmission housing.

25. The air turbine starter of claim 14 wherein the valve is normally biased open.

26. The air turbine starter of claim 25 wherein the valve includes a bias element having a threshold for closing the valve and wherein the threshold is at least about 12 inches of water.

27. The air turbine starter of claim 26 wherein the valve is positioned in an oil return channel of the air turbine starter and wherein the valve is a poppet valve.

28. A kit for configuring an air turbine starter to have a valve, the kit comprising:

a cover plate for mounting on an air turbine starter between the air turbine starter and a gearbox, the cover plate having a wall defining an opening for receiving a valve, the cover plate further including an engagement surface; and

a normally open valve including a valve housing for engaging the opening in the cover plate and further including a complementary engagement surface for engaging the engagement surface on the cover plate so that the valve when installed on the cover plate is normally open during normal operation of an air turbine starter mounted on a gearbox.

29. The kit of claim 28 further comprising a second valve and wherein the cover plate includes a second wall defining a second opening for receiving the second valve.

30. The kit of claim 28 wherein the cover plate further includes a ring seal for sealing about an output shaft of an air turbine starter.

31. The kit of claim 30 further comprising a second valve and wherein the cover plate includes a second wall defining a second opening for receiving the second valve.

32. A method of operating an air turbine starter, the method comprising the steps of:

operating an air turbine starter;

allowing air transfer between the air turbine starter and a gearbox;

keeping a fluid valve in the air turbine housing open under normal operating pressures inside an air turbine housing; and

closing the fluid valve when the air pressure in the housing decreases below a defined pressure.

33. The method of claim 32 wherein the step of closing the fluid valve includes the step of reducing air flow between the air turbine starter and the gearbox.

34. The method of claim 32 wherein the step of keeping the fluid valve open includes the step of allowing air flow through the valve between the air turbine starter and the gearbox.

35. The method of claim 32 wherein the fluid valve is an air valve and the step of closing the fluid valve includes the step of closing the air valve.

36. An air turbine starter comprising an air turbine starter housing having a wall defining a first opening allowing oil to pass through the opening, an output shaft extending from the housing, a cover plate adjacent the output shaft and including a wall in the cover plate defining a second opening, a first normally open valve in the first opening, a second normally open valve in the second opening and wherein the first and second normally open valves are configured to be actuated by a pressure change across the valve.