System and method for controlling the working line position in a gas turbine engine compressor

• US 7,762,084 B2
• Filed: 11/11/2005
• Issued: 07/27/2010
• Est. Priority Date: 11/12/2004
• Status: Active Grant

• Current Assignee: Industrial Turbine Company (UK) Limited (Siemens AG)
• Original Assignee: Rolls-Royce Canada Ltd (Rolls-Royce Holdings Plc)
• Inventors: Martis, Dan, Rowe, Arthur
• Primary Examiner(s): RODRIGUEZ, WILLIAM H
• Application Number:
  US11/271,413
• Publication Number:
  US 20060101826A1
• Time in Patent Office: 1,719 Days
• Field of Search: 607/79, 607/82, 607/85, 60/390.91, 607/92, 607/95, 415/145, 415/160
• US Class Current: 60/792
• CPC Class Codes: F01D 15/10 Adaptations for driving, or combinations with, electric generators
• CPC Class Codes: F01D 17/162 for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line F01D17/167 takes precedence
• CPC Class Codes: F02C 9/20 by throttling; by adjusting vanes
• CPC Class Codes: F04D 27/0246 by varying geometry within the pumps, e.g. by adjusting vanes
• CPC Class Codes: F05D 2270/101 Compressor surge or stall

Abstract

A system for actively controlling the working line location within a low pressure compressor. The system includes a plurality of variable inlet guide vanes that are adjusted to maintain the working line at a constant level as the low pressure compressor rotates at a constant speed.

Claims

1. An apparatus, comprising:

an electric generator;

a first compressor including a plurality of variable inlet guide vanes;

a first turbine coupled to said first compressor and said electrical generator, said first turbine driving said first compressor and said electrical generator at a substantially constant speed;

a second compressor;

a second turbine coupled to said second compressor and operable to drive said second compressor; and

said first compressor has a working line maintained at a constant level by closed loop control of said plurality of variable inlet guide vanes.

2. The apparatus of claim 1, wherein the control of said plurality of variable inlet guide vanes is independent of output power.

3. The apparatus of claim 1, wherein said first compressor is a low-pressure compressor;

wherein said first turbine is a low-pressure turbine;

wherein said second compressor is a higher pressure compressor than said low-pressure compressor;

wherein said second turbine is a higher pressure turbine than said low pressure turbine;

wherein said plurality of variable inlet guide vanes are joined by a ring; and

which further includes an actuator coupled with said ring and operable to move all of said plurality of variable inlet guide vanes in unison.

4. The apparatus of claim 1, which further includes a plurality of bleed off valves in fluid communication with said first compressor, said plurality of bleed valves being operable to control the working line level up to a bleed off valve closing point;

and

wherein said first compressor working line is maintained at a constant level by said plurality of variable inlet guide vanes after said plurality of bleed off valves are closed.

5. The apparatus of claim 1 wherein said first compressor is an axial flow compressor including an inlet and an outlet;

which further includes a first sensor at said inlet operable to determine total pressure and a second sensor aft of said outlet to determine a static pressure downstream of said outlet; and

wherein a ratio of said static pressure to said total pressure is utilized in the closed loop control of said plurality of variable inlet guide vanes.

6. The apparatus of claim 1, wherein said working line level is maintained at a constant level over the life of the engine.

7. The apparatus of claim 1, which further includes means for controlling the maintenance of said working line at a constant level.

8. The apparatus of claim 1, wherein the control of said plurality of variable inlet guide vanes is independent of output power;

wherein said first compressor is an axial flow low-pressure compressor;

wherein said first turbine is a low-pressure turbine;

wherein said second compressor is an axial flow higher pressure compressor than said low-pressure compressor;

wherein said second turbine is a higher pressure turbine than said low pressure turbine;

wherein said plurality of variable inlet guide vanes are joined by a ring;

which further includes an actuator coupled with said ring and operable to move all of said plurality of variable inlet guide vanes in unison;

which further includes a plurality of bleed off values in fluid communication with said low-pressure compressor, said plurality of bleed valves being operable to control the working line level up to a bleed off valve closing point;

wherein said low-pressure compressor working line is maintained at a constant level by said plurality of variable inlet guide vanes after said plurality of bleed off valves are closed;

wherein said low-pressure compressor including an inlet and an outlet;

which further includes a first sensor at said inlet of the low-pressure compressor and being operable to determine a total pressure and a second sensor aft of said outlet of the low-pressure compressor and being operable to determine a static pressure downstream of said outlet; and

wherein a ratio of said static pressure to said total pressure is utilized in the closed loop control of said plurality of variable inlet guide vanes.

9. An apparatus, comprising:

an electric generator;

a low-pressure compressor including a plurality of variable inlet guide vanes and a plurality of bleed off valves;

a high-pressure compressor;

a high-pressure turbine coupled to said high-pressure compressor and operable to drive said high-pressure compressor;

a low-pressure turbine coupled to said low-pressure compressor and said electrical generator, said low-pressure turbine driving said low-pressure compressor and said electrical generator at a constant rotational speed; and

said low-pressure compressor has a working line controlled by operation of said plurality of bleed off valves up to a bleed off valve closing point, at said bleed off valve closing point said plurality of bleed off valves are closed, and control of said working line above said bleed off valve closing point is through the operation of said plurality of variable inlet guide vanes to maintain said working line at a constant level independent of engine output power.

10. The apparatus of claim 9, wherein said plurality of variable inlet guide vanes are joined by a connecting member;

which further includes an actuator coupled with said connecting member and being operable to move all of said plurality of variable inlet guide vanes in unison; and

wherein the control of the plurality of variable inlet guide vanes is in closed loop.

11. The apparatus of claim 9, wherein said low-pressure compressor is an axial flow compressor including an inlet and an outlet;

which further includes a first sensor at said inlet operable to determine a total pressure and a second sensor aft of said outlet to determine a static pressure downstream of said outlet; and

wherein a feedback pressure ratio of said static pressure to said total pressure is utilized in the control of said plurality of variable inlet guide vanes.

12. The apparatus of claim 9, wherein said working line is maintained at a constant level over the life of the engine.

13. The apparatus of claim 9, which further includes control means for controlling the maintenance of said working line at a constant level.

14. The apparatus of claim 9, wherein the control of said plurality of variable inlet guide vanes is independent of output power;

wherein said plurality of variable inlet guide vanes are joined by a connecting member;

which further includes an actuator coupled with said connecting member and being operable to move all of said plurality of variable inlet guide vanes in unison;

wherein said low-pressure compressor is an axial flow compressor including an inlet and an outlet;

which further includes a first sensor at said inlet operable to determine total pressure and a second sensor aft of said outlet to determine a static pressure downstream of said outlet;

wherein a feedback pressure ratio of said static pressure to said total pressure is utilized in the control of said plurality of variable inlet guide vanes;

wherein the control of the plurality of variable inlet guide vanes is in closed loop; and

wherein said working line is maintained at a constant level over the life of the engine.

15. An apparatus, comprising:

an electric generator; and

a multi-spool gas turbine engine comprising;

a first compressor having a working line level;

a first turbine coupled to said first compressor and said electrical generator, said first turbine driving said first compressor and said electrical generator at a substantially constant speed;

a second compressor;

a second turbine coupled to said second compressor and operable to drive said second compressor; and

means for maintaining said working line of said first compressor at a constant level.