Jet pump

• US 9,239,063 B2
• Filed: 04/12/2013
• Issued: 01/19/2016
• Est. Priority Date: 07/29/2004
• Status: Active Grant

• Current Assignee: Pursuit Marine Drive Limited (Cellulac Limited)
• Original Assignee: Pursuit Marine Drive Limited (Cellulac Limited)
• Inventors: Fenton, Marcus Brian Mayhall, Wallis, Alexander Guy
• Primary Examiner(s): Freay, Charles
• Assistant Examiner(s): STIMPERT, PHILIP EARL
• Application Number:
  US13/862,207
• Publication Number:
  US 20140064988A1
• Time in Patent Office: 1,012 Days
• Field of Search: 417/151, 417/54, 417/76, 417/152, 417/165, 417/184, 417/185, 417187-189, 417/196, 417/198
• US Class Current: 1/1
• CPC Class Codes: F04F 5/14 the inducing fluid being elastic fluid
• CPC Class Codes: F04F 5/465 with supersonic flow mixing of supersonic fluids B01F25/20

Abstract

A fluid mover includes a hollow body with a straight-through passage of substantially constant cross-section with an inlet end an outlet end for the entry and discharge respectively of a working fluid. A nozzle substantially circumscribes and opens into the passage intermediate the inlet and outlet ends. An inlet communicates with the nozzle for the introduction of a transport fluid, and a mixing chamber is formed within the passage downstream of the nozzle. The nozzle internal geometry and the bore profile upstream of the nozzle exit optimize the energy transfer between the transport fluid and working fluid. Working fluids are atomized to form a dispersed vapor/droplet flow with locally supersonic conditions within a pseudo-vena contracta, resulting in the creation of a supersonic condensation shock wave within the downstream mixing chamber by the condensation of the transport fluid. Methods of moving and processing fluids using the fluid mover are also disclosed.

Claims

1. A fluid mover comprising:

a hollow body provided with a straight-through passage of substantially constant cross section with an inlet at one end of the passage and an outlet at the other end of the passage for the entry and discharge respectively of a working fluid;

a nozzle substantially circumscribing and opening into said passage intermediate the inlet and outlet ends thereof;

an inlet communicating with the nozzle for the introduction of a transport fluid;

a transport fluid source in communication with the transport fluid inlet, wherein the transport fluid source controls the pressure of the transport fluid at the inlet such that a momentum flux ratio (M) between the transport fluid and working fluid lies in the range 2≦

M≦

70; and

a mixing chamber being formed within the passage downstream of the nozzle;

wherein the nozzle internal geometry and the bore profile of the passage immediately upstream of the nozzle exit are so disposed and configured that in use through the introduction of transport fluid the working fluid or fluids are atomised to form a dispersed vapour/droplet flow regime-within a distance of 1.5D downstream of the nozzle exit where D is the nominal diameter of the bore through the center of the fluid mover.

2. The fluid mover according to claim 1, wherein the passage is a substantially circular passage and the nozzle is an annular nozzle substantially circumscribing the passage.

3. The fluid mover according to claim 1, wherein the nozzle is of a convergent-divergent geometry internally thereof.

4. The fluid mover according to claim 3, wherein the nozzle is configured to give the supersonic flow of transport fluid within the passage.

5. The fluid mover according to claim 1, wherein the bore profile of the passage immediately upstream of the nozzle is configured to encourage working fluid atomisation.

6. A method of moving a working fluid, the method comprising the steps of:

presenting a fluid mover to the working fluid, the mover having a straight-through passage of substantially constant cross section;

applying a substantially circumscribing stream of a transport fluid to the passage through an annular nozzle;

controlling the pressure of the transport fluid via a transport fluid source such that a momentum flux ratio (M) between the transport fluid and working fluid lies in the range 2≦

M≦

70;

atomising the working fluid to form a dispersed vapour and droplet flow regime with locally supersonic flow conditions within a distance of 1.5D downstream of the nozzle exit where D is the nominal diameter of the bore through the center of the fluid mover;

generating a supersonic condensation shock wave within the passage downstream of the nozzle by condensation of the transport fluid;

inducing flow of the working fluid through the passage from an inlet to an outlet thereof; and

modulating the condensation shock wave to vary the working fluid discharge from the outlet.

7. The method of claim 6, wherein the modulating step includes modulating the intensity of the condensation shock wave.

8. The method of claim 6, wherein the modulating step includes modulating the position of the condensation shock wave.

9. The method of claim 6, further comprising the step of introducing an instability in working fluid flow immediately upstream of the nozzle.

10. The method according to claim 6, wherein the transport fluid is steam.