Energy recovering flow control valve

• US 9,599,252 B2
• Filed: 02/14/2013
• Issued: 03/21/2017
• Est. Priority Date: 02/16/2012
• Status: Active Grant

• Current Assignee: Politecnico di Milano
• Original Assignee: Politecnico di Milano
• Inventors: Malavasi, Stefano
• Primary Examiner(s): TIETJEN, MARINA ANNETTE
• Application Number:
  US14/376,113
• Publication Number:
  US 20150041002A1
• Time in Patent Office: 1,496 Days
• Field of Search: 137/15.17, 137/551, 137/798
• US Class Current: 1/1
• CPC Class Codes: F16K 47/045 and the closure member being rotatable
• CPC Class Codes: F16K 5/0605 with particular plug arrangements, e.g. particular shape or built-in means
• CPC Class Codes: Y10T 137/8376 Combined

Abstract

A fluid flow control valve (101, 601) includes a housing (106) and a spherical obstructer (107) having a through hole (108), wherein the spherical obstructer (107) is inserted in the housing (106) and is adapted to rotate therein (106) about an axis of rotation (110) between a first position, in which the through hole (108) is substantially coaxial to the control valve to allow the passage of a fluid, and a second position, in which the through hole (108) is substantially transversal to the control valve to prevent the passage of a fluid. The control valve further includes a rotor (111) within the through hole (108), wherein the rotor is adapted to rotate in a continuous manner under the action of a fluid flowing through the control valve, rotating about a second axis of rotation (112) substantially coinciding with the axis of rotation of the spherical obstructer.

Claims

1. A fluid flow control valve, comprising:

a housing; and

a spherical obstructer comprising;

a through hole,

wherein said spherical obstructer is inserted in said housing, and

wherein said spherical obstructer is adapted to rotate therein about a first axis of rotation between a first position, in which said through hole is substantially coaxial to said control valve to allow the passage of a fluid, and a second position, in which said through hole is substantially transversal to said control valve to prevent the passage of the fluid, and

wherein said control valve further comprises a rotor within said through hole,

wherein said rotor comprises a shaft and a plurality of blades which are secured to said shaft,

wherein said rotor is adapted to rotate in a continuous manner under the action of the fluid flowing through said control valve, said rotor rotating about said shaft having a second axis of rotation substantially coinciding with said first axis of rotation of said spherical obstructer.

2. The control valve according to claim 1, wherein said plurality of blades are substantially transversal to a flow of said passing fluid, and wherein said second axis of rotation of said shaft substantially coincides with said first axis of rotation.

3. The control valve according to claim 2, wherein said blades are twisted in a direction substantially parallel to the flow of said passing fluid.

4. The control valve according to claim 2, wherein said blades are sized such as to occupy, for some rotation positions of said rotor, substantially the whole free cross-section of said through hole of said spherical obstructer.

5. The control valve according to claim 2, wherein said blades comprise holes on their surface.

6. The control valve according to claim 2, wherein at least one end of said shaft protrudes from said spherical obstructer and is connected to a mechanical unit or to an electric generator.

7. The control valve according to claim 6, further comprising an actuator adapted to rotate said spherical obstructer, wherein said actuator is positioned on one side of said valve opposite to said mechanical unit or said electric generator along said first axis of rotation.

8. The control valve according to claim 1, further comprising a deflecting element positioned upstream of said rotor and adapted to fluid-dynamically interact with a flow of said passing fluid.

9. The control valve according to claim 8, wherein said deflecting element is positioned asymmetrically in said valve relative to said first axis of rotation.

10. The control valve according to claim 1, wherein said first axis of rotation is substantially transversal to said fluid flow through said valve.

11. The control valve according to claim 8, wherein the deflecting element has an aero-fluid-dynamic shape.