Sealing system, turbomachine with a sealing system and method for cleaning the same

1. A sealing system of a turbomachine configured to seal a rotor of the turbomachine relative to a stator of the turbomachine, having a rotor-side component rotating together with the rotor and at least one stator-side component that is stationary together with the stator, comprising:

at least one dry gas seal, which comprises:

a rotor-side sealing component;

a stator-side sealing component, wherein a sealing gap is formed between the rotor-side sealing component and the stator-side sealing component;

a spring element configured to compress the rotor-side sealing component and the stator-side sealing component forming sealing gap; and

a cleaning device comprising a detergent feeding duct arranged in part in the stator and the at least one-stator-side component of the turbomachine and configured to conduct detergent in a direction of

the spring element for cleaning the spring element;

a detergent discharge duct arranged in the stator-side component that is stationary together with the stator and configured to conduct detergent away from the spring element; and

a sealing gas feeding duct configured to conduct sealing gas in the direction of the sealing gap;

wherein radially inner section of the detergent feeding duct is arranged radially outward of the spring element to discharge the detergent into a spring space of the spring element, and

wherein the detergent feeding duct is axially spaced apart from the sealing gas feeding duct.

2. The sealing system according to claim 1 , further comprising:

a sealing gas discharge duct configured to conduct the sealing gas away from the sealing gap,

wherein the sealing gas feeding duct and the sealing gas discharge duct are provided in the stator and into the at least one stator-side component that is stationary together with the stator.

3. The sealing system according to claim 2 , further comprising:

a radially outer section of the sealing gas feeding duct arranged in the stator;

multiple radially inner sections of the sealing gas feeding duct are arranged in the stator-side component; and

a first annular gap connecting the radially outer section and a radially inner section formed between the stator and the stator-side component.

4. The sealing system according to claim 3 , further comprising:

a radially outer section of the sealing gas discharge duct arranged in the stator;

multiple radially inner sections of the sealing gas discharge duct are arranged in the stator-side component; and

an annular gap connecting the radially outer section and the multiple radially inner sections formed between the stator and the stator-side component.

5. The sealing system according to claim 4 , wherein the detergent feeding duct is introduced into the stator-side component that is stationary together with the stator and configured to conduct detergent to the spring element.

6. The sealing system according to claim 5 , wherein

a radially outer section of the detergent feeding duct and of the detergent discharge duct are introduced into the stator, and

the radially inner section of the detergent feeding duct and a radially inner section of the detergent discharge duct are introduced into the stator.

7. The sealing system according to claim 6 , wherein detergent feeding duct is configured to conduct the detergent in the direction of the sealing gap and via the sealing gas discharge duct away from the sealing gap.

8. The sealing system according to claim 7 , wherein the sealing gas feeding duct and the sealing gas discharge duct are formed spaced apart from one another in an axial direction and at a same circumferential position with respect to an axis of rotation of the rotor.

9. The sealing system according to claim 8 , wherein the detergent feeding duct and the detergent discharge duct are formed spaced apart from one another in a circumferential direction and at a same axial position.

10. The sealing system according to claim 9 , wherein the detergent feeding duct is formed in the axial direction between the sealing gas feeding duct and the sealing gas discharge duct and in the same circumferential position as the sealing gas feeding duct and the sealing gas discharge duct.

11. The sealing system according to claim 5 , wherein the detergent feeding duct receives the detergent from a detergent dosing system at a defined detergent pressure.

12. The sealing system according to claim 1 , further comprising:

a heating device configured to heat detergent utilized for cleaning the dry gas seal.

13. A turbomachine for compressing a process gas with an integrated cleaning device, comprising:

a stator having a stator-side component;

a rotor, and

a sealing system comprising at least one dry gas seal, which comprises:

a rotor-side sealing component;

a stator-side sealing component, wherein a sealing gap is formed between the rotor-side sealing component and the stator-side sealing component;

a spring element configured to compress the rotor-side sealing component and the stator-side sealing component forming the sealing gap; and

the integrated cleaning device comprising a detergent feeding duct arranged in part in the stator and stator-side component of the turbomachine and configured to conduct detergent in a direction of

the spring element for cleaning the spring element; and

a detergent discharge duct arranged in the stator-side component that is stationary together with the stator and configured to conduct detergent away from the spring element; and

a sealing gas feeding duct configured to conduct sealing gas in the direction of the sealing gap,

wherein radially inner section of the detergent feeding duct is arranged radially outward of the spring element to discharge the detergent into a spring space of the spring element, and

wherein the detergent feeding duct is axially spaced apart from the sealing gas feeding duct.

14. The sealing system according to claim 1 , wherein the cleaning device conducts the detergent during a running of the turbomachine.

15. The sealing system according to claim 1 , wherein at least one sealing gas feeding duct of the cleaning device is integrated into the stator.

16. The sealing system according to claim 1 , wherein at least one sealing gas discharge duct of the cleaning device is integrated into the stator.

17. The turbomachine for compressing a process gas with an integrated cleaning device, according to claim 13 , wherein the detergent feeding duct and the detergent discharge duct are offset relative to one another in a circumferential direction and formed in a same axial position.

18. The turbomachine for compressing a process gas with an integrated cleaning device, according to claim 17 , wherein the detergent feeding duct, seen in the axial direction is formed between a sealing gas feeding duct and a sealing gas discharge duct.