Rotodynamic pump having a body defining a body cavity with a first and second housing portion defining a portion of an impeller cavity and disposed within the body cavity wherein the body cavity extends at least in part around the second housing portion and the housing portions defining an impeller clearance

Patent metadata

Field	Value
Publication number	US-11459958-B2
Application number	US-201916361819-A
Country	US
Kind code	B2
Filing date	Mar 22, 2019
Priority date	Mar 22, 2019
Publication date	Oct 4, 2022
Grant date	Oct 4, 2022

Abstract

A rotodynamic pump for pumping a fluid includes an impeller, a housing surrounding the impeller, and a pressure regulating mechanism. The pressure regulating mechanism is configured to adjust the clearance between the impeller and the impeller housing to regulate pressure of the fluid downstream of the impeller. A method of regulating the delivery pressure is also disclosed.

First claim

The invention claimed is:

1. A rotodynamic pump for pumping a fluid, the rotodynamic pump comprising:
a body defining a body cavity;
an impeller disposed within the body cavity;
a first housing portion disposed within the body cavity and defining at least in part an impeller cavity containing the impeller, and a second housing portion disposed within the body cavity and defining at least in part the impeller cavity, a portion of the body cavity defined between the second housing portion and the body, the portion of the body cavity fluidly sealed from the impeller cavity; and
a pressure regulating mechanism configured to adjust a clearance between the impeller and the second housing portion to regulate pressure of the fluid downstream of the impeller;
wherein the second housing portion is movable relative to the first housing portion during operation of the rotodynamic pump to vary the clearance, and the pressure regulating mechanism is configured to move the second housing portion relative to the first housing portion to vary the clearance and thereby regulate a delivery pressure of the fluid at an outlet of the pump; and
wherein the body extends at least in part around the second housing portion, wherein an inner surface of the body and an outer surface of the second housing portion at least partially define the portion of the body cavity, the portion of the body cavity being hydraulically isolated from an outer surface of the body.

2. The rotodynamic pump of claim 1 , comprising a fluid conduit hydraulically connecting the outlet of the pump to the portion of the body cavity to feed fluid from the outlet to the portion of the cavity to apply a force on the second housing portion.

3. The rotodynamic pump of claim 2 , comprising a biasing element biasing the second housing portion toward the first housing portion.

4. The rotodynamic pump of claim 3 , comprising a bellows, the bellows and the biasing element being movable by movement of the second housing portion relative to the first housing portion.

5. The rotodynamic pump of claim 3 , wherein the biasing element is a spring disposed between the second housing portion and the body, and the second housing portion is movable away from the first housing portion to compress the spring and the bellows.

6. The rotodynamic pump of claim 1 , wherein the impeller is rotatable about a rotation axis to pump the fluid from an inlet of the pump to the outlet, and the second housing portion is movable relative to the first housing portion in a direction parallel to the rotation axis.

7. A fuel system for an aircraft engine, comprising the rotodynamic pump of claim 1 , the rotodynamic pump when in use supplying fuel to the aircraft engine.

8. The rotodynamic pump of claim 1 , wherein the pressure regulating mechanism includes an actuator and a pressure sensor that are operatively connected to a controller, the pressure regulating mechanism regulating the delivery pressure toward at least one delivery pressure setpoint by operating the actuator by the controller to selectively displace the second housing portion relative to the first housing portion in response to a signal indicative of the delivery pressure.

9. The rotodynamic pump of claim 8 , wherein the actuator includes at least one of an electric motor, and a hydraulic actuator that is communicatively coupled to the controller.

10. The rotodynamic pump of claim 8 , comprising a pressure sensor communicatively coupled to the controller and being hydraulically connected to the outlet to generate the signal while the rotodynamic pump is in use.

11. The rotodynamic pump of claim 8 , wherein the at least one delivery pressure setpoint is a range of pressures.

12. The rotodynamic pump of claim 11 , wherein the controller includes a processor and a non-transient memory communicatively coupled to the processor, the non-transient memory storing processor-executable instructions which, when executed by the processor, cause the controller to execute a proportional-integral-derivative (PID) control algorithm to operate the actuator in response to the signal to regulate the delivery pressure toward the at least one delivery pressure setpoint.

13. The rotodynamic pump of claim 1 , wherein movement of the second housing portion relative to the first housing portion varies a size of the impeller cavity, and varies a size of the portion of the body cavity.

Assignees

• Pratt & Whitney Canada

Inventors

• Waddleton David
• Renaud Benjamin
• Bergeron Sebastien
• Plamondon Etienne
• Gauvreau Jean-Gabriel

Classifications

• B64D37/00

  Arrangements in connection with fuel supply for power plant (refuelling during flight B64D39/00) · CPC title

• F02C7/22

  Fuel supply systems · CPC title

• F04D5/008

  Details of the stator, e.g. channel shape · CPC title

• F04D15/005 Primary

  the pumps being of the circumferential flow type · CPC title

• F02C9/30

  characterised by variable fuel pump output · CPC title