METHOD FOR BALANCING THRUST, TURBINE AND TURBINE ENGINE

• US 20150330220A1
• Filed: 12/16/2013
• Published: 11/19/2015
• Est. Priority Date: 12/20/2012
• Status: Abandoned Application

• Current Assignee: Nuovo Pignone SPA (Nuovo Pignone International SRL)
• Original Assignee: Nuovo Pignone SPA (Nuovo Pignone International SRL)
• Inventors: D'ERCOLE, Michele, ASTI, Antonio, LANDI, Giacomo, CEI, Stefano, CECCHERINI, Alberto
• Application Number:
  US14/652,605
• Publication Number:
  US 20150330220A1
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: F01D 25/16 Arrangement of bearings; Supporting or mounting bearings in casings bearings per se F16C
• CPC Class Codes: F01D 25/24 Casings modified for heating or cooling F01D25/14; Casing parts, e.g. diaphragms, casing fastenings casings for rotary machines or engines in general F16M ; special arrangements in stators dealing with breaking-off of part of rotor F01D21/045
• CPC Class Codes: F01D 3/00 Machines or engines with axial-thrust balancing effected by working-fluid
• CPC Class Codes: F01D 3/02 characterised by having one fluid flow in one axial direction and another fluid flow in the opposite direction
• CPC Class Codes: F01D 3/04 axial thrust being compensated by thrust-balancing dummy piston or the like
• CPC Class Codes: F01D 5/02 Blade-carrying members, e.g. rotors rotors of non-bladed type F01D1/34; stators F01D9/00 ; selecting particular materials F01D5/28
• CPC Class Codes: F05D 2220/30 in turbines
• CPC Class Codes: F05D 2240/54 Radial bearings

Abstract

A turbine comprising a rotatable rotor and a pressure chamber; a wall of the pressure chamber is arranged to act on the rotor so that to balance thrust exerted by the rotor when it rotates; a conduit connects the pressure chamber and arranged to a pressure source; a valve associated to the conduit may open and close the conduit; the valve is arranged to open automatically when the pressure upstream of the valve exceeds a first predetermined threshold value; in this way, when the load of the turbine is high excessive thrust is balanced because of the higher pressure in the pressure chamber.

Claims

1. A method for balancing thrust in a turbine provided with a rotatable rotor, the method comprising:

providing a first pressure source outside of said turbine;

providing a pressure chamber inside of said turbine, wherein a wall of said pressure chamber acts on said rotor so that to balance thrust exerted by said rotor when it rotates;

connecting said first pressure source to said pressure chamber via a first conduit; and

associating a first valve to said first conduit, said first valve being arranged to open and close said first conduit,

wherein said first valve is arranged to open automatically when the pressure upstream of said first valve exceeds a first predetermined threshold value.

2. The method of claim 1, wherein said first valve is configured to be completely closed when the pressure upstream of said first valve is smaller than said first predetermined threshold value, and to be completely opened when the pressure upstream of said first valve is greater than said first predetermined threshold value.

3. The method of claim 1, further comprising:

associating a first orifice to said first conduit to choke said first conduit,

wherein said first orifice is sized to establish a choked flow inside said first conduit.

4. The method of claim 1, further comprising:

providing a second pressure source outside of said turbine;

connecting said second pressure source to said pressure chamber via a second conduit;

associating a second valve to said second conduit, said second valve being arranged to open and close said second conduit; and

associating a second orifice to said second conduit to choke said second conduit,

wherein said second valve is arranged to open automatically when the pressure upstream of said second valve exceeds a second predetermined threshold value; and

wherein said second orifice is sized to establish a choked flow inside said second conduit.

5. The method of claim 1, further comprising:

providing a third pressure source outside of said turbine; and

connecting said third pressure source to said pressure chamber via a third conduit.

14. The method of claim 2, further comprising:

associating a first orifice to said first conduit to choke said first conduit,

wherein said first orifice is sized to establish a choked flow inside said first conduit.

15. The method of claim 14, further comprising:

providing a second pressure source outside of said turbine;

connecting said second pressure source to said pressure chamber via a second conduit;

associating a second valve to said second conduit, said second valve being arranged to open and close said second conduit; and

associating a second orifice to said second conduit to choke said second conduit,

wherein said second valve is arranged to open automatically when the pressure upstream of said second valve exceeds a second predetermined threshold value; and

wherein said second orifice is sized to establish a choked flow inside said second conduit.

16. The method of claim 15, further comprising:

providing a third pressure source outside of said turbine; and

connecting said third pressure source to said pressure chamber via a third conduit.

6. A turbine comprising:

a rotatable rotor;

a pressure chamber, wherein a wall of said pressure chamber is arranged to act on said rotor to balance thrust exerted by said rotor when it rotates;

a first conduit connected to said pressure chamber and arranged to be connected to a first pressure source; and

a first valve associated to said first conduit and arranged to open and close said first conduit,

wherein said first valve is arranged to open automatically when the pressure upstream of said first valve exceeds a first predetermined threshold value.

7. The turbine of claim 6, further comprising:

a first orifice associated to said first conduit to choke said first conduit,

wherein said first orifice is sized to establish a choked flow inside said first conduit.

8. The turbine of claim 6, wherein said first automatic valve comprises:

a mechanical valve comprising a mechanical control member for its opening/closing; and

a hydraulic actuator comprising a mechanical actuation member, wherein said hydraulic actuator is hydraulically connected to said first conduit and said mechanical actuation member is mechanically connected to said mechanical control member.

9. The turbine of claim 6, further comprising a bearing, in particular a ball bearing, and wherein part of said thrust exerted by said rotor when it rotates is balanced by said bearing.

10. The turbine of claim 6, further comprising a plurality of cascaded stages, and wherein said thrust bearing is located downstream of the last stage of said plurality of cascaded stages.

11. The turbine of claim 6, wherein said first conduit passes through an exhaust of said turbine and is externally aerodynamically shaped.

17. The turbine of claim 7, wherein said first automatic valve comprises:

a mechanical valve comprising a mechanical control member for its opening/closing; and

a hydraulic actuator comprising a mechanical actuation member, wherein said hydraulic actuator is hydraulically connected to said first conduit and said mechanical actuation member is mechanically connected to said mechanical control member.

18. The turbine of claim 17, further comprising a bearing, in particular a ball bearing, and wherein part of said thrust exerted by said rotor when it rotates is balanced by said bearing.

19. The turbine of claim 18, further comprising a plurality of cascaded stages, and wherein said thrust bearing is located downstream of the last stage of said plurality of cascaded stages.

20. The turbine of claim 19, wherein said first conduit passes through an exhaust of said turbine and is externally aerodynamically shaped.

12. A turbine engine comprising:

a cascade connection of a compressor; and

a turbine downstream of said compressor, wherein said turbine comprises;

a rotatable rotor;

a pressure chamber, wherein a wall of said pressure chamber is arranged to act on said rotor to balance thrust exerted by said rotor when it rotates;

a first conduit connected to said pressure chamber and arranged to be connected to a first pressure source; and

a first valve associated to said first conduit and arranged to open and close said first conduit,

wherein said first valve is arranged to open automatically when the pressure upstream of said first valve exceeds a first predetermined threshold value,

wherein said compressor is used as a pressure source for balancing thrust in said turbine.

13. The turbine engine of claim 12, wherein said compressor comprises a plurality of cascaded stages, and wherein the outlet of a stage of said plurality of stages is used as a pressure source for balancing thrust in said turbine.