Method for nozzle clamping force control

• US 4,502,836 A
• Filed: 09/30/1982
• Issued: 03/05/1985
• Est. Priority Date: 07/02/1982
• Status: Expired due to Term

• Current Assignee: Rotoflow Corporation
• Original Assignee: Judson S. Swearingen
• Inventors: Swearingen, Judson S.
• Primary Examiner(s): Garrett, Robert E.
• Assistant Examiner(s): Pitko, Joseph M.
• Application Number:
  US06/430,349
• Time in Patent Office: 887 Days
• Field of Search: 415/26, 415/156, 415/160-164, 415/148, 415/150, 415/151, 415/154, 415/155, 91/44, 92/27, 92/28, 60/594, 416/165
• US Class Current: 415/150
• CPC Class Codes: F01D 17/165 for radial flow, i.e. the vanes turning around axes which are essentially parallel to the rotor centre line F01D17/167 takes precedence

Abstract

A system for pressurizing cavities arranged laterally of pivotal vanes of a variable primary nozzle system in a radial turbine. The cavities are supplied with fluid of increased or reduced pressure to resist the clamping forces of the mounting rings. The fluid may conveniently be influent pressure or nozzle discharge pressure as may be appropriate. Pressure to the cavities is controlled as responsive to the pressure in the actuator system for adjusting the nozzles.

Claims

1. A method for controlling clamping forces in a variable primary nozzle system of a radial turbine having primary nozzles formed by pivotal nozzle vanes clamped between mounting rings having relative axial movement therebetween, comprising the steps of:

sensing the force required to vary the primary nozzles;

opening a source of pressure when said sensed force exceeds a preselected value;

directing flow from the opened source of pressure to the nozzle vanes adjacent the mounting rings.

2. The method of claim 1 wherein the nozzle system includes a fluid pressure driven actuator system for varying said nozzles and said step of sensing the force includes sensing the pressure applied to the actuator system.

3. The method of claim 2 wherein said step of opening a source of pressure includes directing pressure from the actuator system as applied to vary nozzles to a pressure actuated valving system controlling flow from the source of pressure.

4. The method of claim 1 wherein said step of opening a source of pressure includes restricting the resulting flow to allow a minimum pressure bleed off from between the vanes and the rings.

5. The method of claim 1 wherein said step of directing flow includes receiving flow from the influent to the radial turbine as the source of pressure.

6. A nozzle clamping force control for a variable primary nozzle system on a radial turbine having mounting rings mounted for relative axial movement therebetween, nozzle vanes clamped between the mounting rings, and an actuator for pivoting said nozzle vanes, comprising

cavities in the nozzle vane surfaces adjacent the rings;

passages extending to said cavities;

a source of pressure in communication with said passages;

valve means for controlling flow from said source of pressure through said passages;

valve control means for opening said valve means responsive to actuator force.

7. The control of claim 6 wherein said passages extending to said cavities include a first passage extending through a ring to a first said cavity and a second passage extending from said first cavity to a second said cavity.

8. The control of claim 6 wherein said source of pressure is the influent to the radial turbine.

9. A nozzle clamping force control for a variable primary nozzle system on a radial turbine having mounting rings mounted for relative axial movement therebetween, nozzle vanes clamped between the mounting rings and a fluid pressure driven actuator for pivoting said nozzle vanes, comprising

cavities in the nozzle vane surfaces adjacent the rings;

passages extending to said cavities;

a source of pressure in communication with said passages;

valve means for controlling flow from said source of pressure through said passages;

a valve actuator operatively coupled with said valve means; and

a pressure line from the fluid pressure driven actuator to said valve actuator, said valve actuator being fluid pressure actuated and having a preselected actuation pressure.

10. A method for controlling clamping forces in a variable primary nozzle system of a radial turbine having primary nozzles formed by pivotal nozzle vanes clamped between mounting rings having relative axial movement therebetween, comprising the steps of:

sensing the force required to vary the primary nozzles;

opening a source of pressure when said sensed force exceeds a preselected value;

directing pressure from the opened source of pressure to at least one cavity laterally positioned to the nozzle vanes.

11. The method of claim 10 wherein the nozzle system includes a fluid pressure driven actuator system for varying said nozzles and said step of sensing the force includes sensing the pressure applied to the actuator system.

12. The method of claim 11 wherein said step of opening a source of pressure includes directing pressure from the actuator system as applied to vary nozzles to a pressure actuated valving system controlling flow from the source of pressure.

13. The method of claim 10 wherein said step of directing pressure includes receiving pressure from the influent to the radial turbine as the source of pressure.

14. The method of claim 10 wherein said step of directing flow includes receiving reduced pressure from the nozzle discharge area of the turbine as the source of pressure.

15. A nozzle clamping force control for a variable primary nozzle system on a radial turbine having mounting rings mounted for relative axial movement therebetween, nozzle vanes clamped between the mounting rings, and an actuator for pivoting said nozzle vanes, comprising

at least one cavity laterally positioned to the nozzle vanes;

a passage extending to said cavity;

a source of pressure in communication with said passage;

valve means for controlling pressure from said source of pressure through said passage;

valve control means for opening said valve means responsive to actuator force.

16. The control of claim 15 wherein said cavity is on an opposite side of one of the mounting rings to the nozzle vanes.

17. The control of claim 16 further including a vent port extending through the clamping ring from the cavity to adjacent at least one nozzle vane.

18. The control of claim 17 further including a passageway through at least one nozzle vane in alignment with said vent port.

19. The control of claim 16, 17 or 18 wherein said source of pressure is an area of reduced pressure in the turbine.

20. The control of claim 19 wherein said area of reduced pressure is the nozzle discharge.

21. The control of claim 15 wherein said source of pressure is the influent to the radial turbine.

22. A nozzle clamping force control for a variable primary nozzle system on a radial turbine having mounting rings mounted for relative axial movement therebetween, nozzle vanes clamped between the mounting rings and a fluid pressure driven actuator for pivoting said nozzle vanes, comprising

a cavity laterally positioned adjacent a mounting ring on a side opposite from the nozzle vanes;

a passage extending to said cavity;

a source of pressure in communication with said passage;

a valve means for controlling flow from said source of pressure through said passage;

a valve actuator operatively coupled with said valve means; and

a pressure line from the fluid pressure driven actuator to said valve actuator, said valve actuator being fluid pressure actuated and having a preselected actuation pressure.