Energy recovering flow control valves

Patent metadata

Field	Value
Publication number	US-10648588-B2
Application number	US-201615560071-A
Country	US
Kind code	B2
Filing date	Mar 30, 2016
Priority date	Mar 30, 2015
Publication date	May 12, 2020
Grant date	May 12, 2020

Abstract

A control valve for a fluid flow includes: a valve body that defines an inlet and an outlet for the fluid, an obstructer inserted in the valve body, and an actuator system configured for reversibly translating the obstructer between a first position, in which the obstructer allows the passage of the fluid between the inlet and the outlet, and a second position, in which the obstructer prevents the passage of the fluid between the inlet and the outlet; the control valve further includes a turbine rotor housed inside the valve body, wherein the rotor includes a plurality of blades and is configured for continuously rotating under the action of the fluid flowing between the inlet and the outlet, the rotor rotating about an axis of rotation substantially aligned with the direction of translation of the obstructer.

First claim

The invention claimed is:

1. A control valve for a fluid flow, comprising:
a valve body that defines an inlet and an outlet for said fluid, an obstructer inserted in said valve body;
an actuator system configured for reversibly translating said obstructer between a first position, in which said obstructer allows the passage of said fluid between said inlet and said outlet;
a second position, in which said obstructer prevents the passage of said fluid between said inlet and said outlet, wherein the control valve further comprises a turbine rotor housed inside said valve body, wherein said rotor comprises a plurality of blades and is configured for continuously rotating under the action of said fluid flowing between said inlet and said outlet;
said rotor rotating about an axis of rotation substantially aligned with the direction of translation of said obstructer;
wherein said valve body internally comprises walls which delimit a fluid inlet chamber having a substantially circular seat, and wherein said obstructer is substantially disc-like shaped, and wherein said obstructer is configured for at least partially unrestricting a passage section at said seat in said first position, and wherein said obstructer is further configured for translating into said second position, so as to abut on said seat, in order to occlude said passage section; and
wherein said rotor is so sized as to substantially engage the whole said passage section at said seat, and wherein said rotor is configured for an axial inflow of said fluid into it, and for a perimetrical outflow of said fluid from said rotor; and
wherein said rotor is configured for allowing at least a partial accommodation of said obstructer inside of it, so as to allow translation of said obstructor into said first position.

2. The control valve according to claim 1 , wherein said rotor is further configured for jointly translating with said obstructer, passing through said seat.

3. The control valve according to claim 1 , wherein said rotor is so sized as to substantially engage the whole said passage section at said seat, and wherein said rotor is configured for a perimetrical inflow of said fluid into it, and for an axial outflow of said fluid from said rotor, said rotor being positioned in said fluid inlet chamber.

4. The control valve according to claim 3 , wherein said valve body comprises, proximal to said inlet, a flow diverter configured for directing said fluid flow asymmetrically onto the perimeter of said rotor, so as to trigger the rotation of said rotor.

5. The control valve according to claim 1 , wherein said valve body internally comprises an ovoid element which is fixed with respect to the sidewalls of said valve body, wherein said ovoid element internally houses said obstructer, wherein said obstructer is shaped substantially like a cylinder, and wherein said obstructer is configured for at least partially unrestricting a passage section for said fluid downstream of said ovoid element in said first position, and wherein said obstructer is further configured for translating into said second position, so as to occlude said passage section by means of the lateral wall of said cylinder, in particular by means of a portion of said lateral wall without said slits.

6. The control valve according to claim 5 , wherein said rotor is so shaped as to mate with said ovoid element, and is so sized as to occupy substantially the whole free section around said ovoid element, and wherein said rotor is configured for an axial inflow of said fluid into it, and for an axial outflow of said fluid from said rotor.

7. The control valve according to claim 6 , wherein said rotor is located upstream of said ovoid element with respect to the direction of said fluid between said inlet and said outlet, and wherein said outflow from said rotor is diverging around said ovoid element.

8. The control valve according to claim 6 , wherein said rotor is located downstream of said ovoid element with respect to the direction of said fluid between said inlet and said outlet, and wherein said outflow from said rotor is converging for entering said outlet.

9. The control valve according to claim 8 , wherein said rotor comprises a central hole configured for allowing said obstructer to be housed therein, in both said first position and said second position.

10. The control valve according to claim 5 , wherein said obstructer comprises a plurality of slits.

11. The control valve according to claim 1 , wherein said turbine comprises said rotor, wherein said rotor is supported by rolling elements allowing it to rotate about said axis of rotation, and wherein said turbine further comprises a transmission adapted to rotate a shaft protruding from said valve body and configured for being connected to an external mechanical or electric utilizer.

12. The control valve according to claim 11 , wherein said transmission is a mechanical transmission.

13. The control valve according to claim 12 , wherein said mechanical transmission comprises a gear transmission having a predefined transmission ratio.

14. The control valve according to claim 11 , wherein said transmission is a magnetic drive transmission.

15. A control valve for a fluid flow, comprising:
a valve body that defines an inlet and an outlet for said fluid, an obstructer inserted in said valve body;
an actuator system configured for reversibly translating said obstructer between a first position, in which said obstructer allows the passage of said fluid between said inlet and said outlet;
a second position, in which said obstructer prevents the passage of said fluid between said inlet and said outlet, wherein the control valve further comprises a turbine rotor housed inside said valve body, wherein said rotor comprises a plurality of blades and is configured for continuously rotating under the action of said fluid flowing between said inlet and said outlet;
said rotor rotating about an axis of rotation substantially aligned with the direction of translation of said obstructer;
wherein said valve body internally comprises an ovoid element which is fixed with respect to the sidewalls of said valve body, wherein said ovoid element internally houses said obstructer, wherein said obstructer is shaped substantially like a cylinder, and wherein said obstructer is configured for at least partially unrestricting a passage section for said fluid downstream of said ovoid element in said first position, and wherein said obstructer is further configured for translating into said second position, so as to occlude said passage section by means of the lateral wall of said cylinder, in particular by means of a portion of said lateral wall without said slits.

16. A control valve for a fluid flow, comprising:
a valve body that defines an inlet and an outlet for said fluid, an obstructer inserted in said valve body;
an actuator system configured for reversibly translating said obstructer between a first position, in which said obstructer allows the passage of said fluid between said inlet and said outlet;
a second position, in which said obstructer prevents the passage of said fluid between said inlet and said outlet, wherein the control valve further comprises a turbine rotor housed inside said valve body, wherein said rotor comprises a plurality of blades and is configured for continuously rotating under the action of said fluid flowing between said inlet and said outlet;
said rotor rotating about an axis of rotation substantially aligned with the direction of translation of said obstructer;
wherein said turbine comprises said rotor, wherein said

Assignees

• Milano Politecnico

Inventors

• Malavasi Stefano

Classifications

• F16K1/00

  Lift valves {or globe valves}, i.e. cut-off apparatus with closure members having at least a component of their opening and closing motion perpendicular to the closing faces ({in combination with sliding valves F16K3/246, F16K3/267} ; diaphragm valves F16K7/00) · CPC title

• F01D1/06

  traversed by the working-fluid substantially radially · CPC title

• F16K1/12

  with streamlined valve member around which the fluid flows when the valve is opened · CPC title

• F16K47/08 Primary

  for decreasing pressure {or noise level} and having a throttling member separate from the closure member {, e.g. screens, slots, labyrinths} · CPC title

• F01D17/145

  by means of valves, e.g. for steam turbines (valves in general F16K) · CPC title