Turbine

Patent metadata

Field	Value
Publication number	US-9309768-B2
Application number	US-201213693266-A
Country	US
Kind code	B2
Filing date	Dec 4, 2012
Priority date	Dec 6, 2011
Publication date	Apr 12, 2016
Grant date	Apr 12, 2016

Abstract

A turbine includes a stator ( 10 ) and a rotor ( 20 ); a plurality of turbine stages ( 30 ) through which a flow path of an operating fluid extends; an axial thrust balancing piston ( 40 ) arranged at the rotor and a first piston chamber ( 41 ) connected to one of the turbine stages ( 30.1 ) so that the operating fluid can be conveyed into the first piston chamber with a first fluid pressure, and a second piston chamber ( 42 ) has a counterpressure so that an axial thrust opposed to a flow direction of the operating fluid can be exerted on the rotor; and a pressure control device ( 60 ) connected to the second piston chamber. The pressure control device constructed to vary the counterpressure by controlled removal of fluid from the second piston chamber so that the axial thrust of the axial thrust balancing piston can be varied.

First claim

We claim:

1. A turbine comprising:
a stator ( 10 );
a rotor ( 20 ) rotatably bearing-supported in said stator ( 10 );
a plurality of turbine stages ( 30 ) formed by said rotor ( 20 ) and said stator ( 10 ) and arranged successively along a longitudinal direction (LR) of said turbine and through which a flow path of an operating fluid extends for driving said rotor ( 20 ) in rotation;
an axial thrust balancing piston ( 40 ) arranged at said rotor ( 20 ), said axial thrust balancing piston ( 40 ) comprising on a first axial piston side a first piston chamber ( 41 ) connected to one of said turbine stages ( 30 . 1 ) via a first fluid line ( 51 ) so that the operating fluid can be conveyed from one turbine stage ( 30 . 1 ) into said first piston chamber ( 41 ) with a first fluid pressure and, on a second axial piston side remote of the first piston side, a second piston chamber ( 42 ) having a counterpressure that is lower than the first fluid pressure so that an axial thrust opposed to a flow direction of the operating fluid through said turbine stages ( 30 ) can be exerted on said rotor ( 20 ) by said axial thrust balancing piston ( 40 ); and
a pressure control device ( 60 ) connected to said second piston chamber ( 42 ) of said axial thrust balancing piston ( 40 ) for varying the counterpressure by controlled removal of fluid from said second piston chamber ( 42 ).

2. The turbine according to claim 1 , wherein said pressure control device ( 60 ) is constructed to vary the counterpressure by controlled suction of fluid from said second piston chamber ( 42 ).

3. The turbine according to claim 1 , wherein said pressure control device ( 60 ) is constructed as a fluid pump comprising a suction side ( 61 ) connected to said second piston chamber ( 42 ) by a second fluid line ( 52 ).

4. The turbine according to claim 3 , wherein said pressure control device ( 60 ) comprises a delivery side ( 62 ) connected by a third fluid line ( 53 ) to the flow path of the operating fluid at a further one of said turbine stage ( 30 . 2 ) of said turbine stages ( 30 ) situated downstream of said one of said turbine stage ( 30 . 1 ) in the flow path; and wherein said further turbine stage ( 30 . 2 ) has a second fluid pressure of operating fluid which is lower than the first fluid pressure.

5. The turbine according to claim 3 , wherein said pressure control device ( 60 ) is constructed as a steam jet ejector having a motive side ( 63 ) connected to the flow path of the operating fluid by a fourth fluid line ( 54 ) so that the operating fluid can be supplied to the motive side ( 63 ) for driving the steam jet ejector.

6. The turbine according to claim 5 , wherein the fourth fluid line ( 54 ) is connected to the first fluid line ( 51 ) so that the operating fluid can be supplied to the motive side ( 63 ) of the steam jet ejector from the first fluid line ( 51 ).

7. The turbine according to claim 5 , additionally comprising a servo valve ( 70 ) arranged in the fourth fluid line ( 54 ) for varying an amount of operating fluid that can be supplied to the motive side ( 63 ) of said pressure control device ( 60 ).

8. The turbine according to claim 7 , wherein said pressure control device ( 60 ) is configured so that an amount of fluid removed from the second piston chamber ( 42 ) is approximately twice the amount of operating fluid supplied to the motive side ( 63 ) of said pressure control device ( 60 ).

9. The turbine according to claim 7 additionally comprising a sensor device ( 90 ), a signal output ( 82 ) and a second control device ( 80 ) having at least one signal input ( 81 ) connected to said sensor device ( 90 ) sensing at least one state parameter of the said turbine; said signal output ( 82 ) connected to said servo valve ( 70 ), and wherein said control device ( 80 ) constructed to control via said signal output ( 82 ) a degree of opening of said servo valve ( 70 ) depending on the at least one state parameter of the said turbine.

10. The turbine according to claim 9 , wherein said sensor device ( 90 ) comprises a temperature sensor ( 91 ) for sensing the temperature of a thrust bearing of said rotor ( 20 ), and wherein said control device ( 80 ) is constructed to control the degree of opening of said servo valve ( 70 ) depending on a the temperature of a thrust bearing of said rotor ( 20 ).

11. The turbine according to claim 2 , wherein said pressure control device ( 60 ) is constructed to vary the counterpressure by controlled suction of fluid from said second piston chamber ( 42 ).

12. The turbine according to claim 4 , wherein said pressure control device ( 60 ) comprises a delivery side ( 62 ) connected by a third fluid line ( 53 ) to the flow path of the operating fluid at a further one of said turbine stage ( 30 . 2 ) of said turbine stages ( 30 ) situated downstream of said one of said turbine stage ( 30 . 1 ) in the flow path; and wherein said further turbine stage ( 30 . 2 ) has a second fluid pressure of operating fluid which is lower than the first fluid pressure.

13. The turbine according to claim 6 , additionally comprising a servo valve ( 70 ) arranged in the fourth fluid line ( 54 ) for varying an amount of operating fluid that can be supplied to the motive side ( 63 ) of said pressure control device ( 60 ).

14. The turbine according to claim 8 additionally comprising a sensor device ( 90 ), a signal output ( 82 ) and a second control device ( 80 ) having at least one signal input ( 81 ) connected to said sensor device ( 90 ) sensing at least one state parameter of the said turbine; said signal output ( 82 ) connected to said servo valve ( 70 ), and wherein said control device ( 80 ) constructed to control via said signal output ( 82 ) a degree of opening of said servo valve ( 70 ) depending on the at least one state parameter of the said turbine.

Assignees

• Man Diesel & Turbo Se

Inventors

• Reinhold Björn
• Schaake Thomas

Classifications

• F01D3/04 Primary

  axial thrust being compensated by thrust-balancing dummy piston or the like · CPC title