Fuel pump systems

Patent metadata

Field	Value
Publication number	US-11629643-B1
Application number	US-202217571055-A
Country	US
Kind code	B1
Filing date	Jan 7, 2022
Priority date	Jan 7, 2022
Publication date	Apr 18, 2023
Grant date	Apr 18, 2023

Abstract

A fuel pump system, comprising an inlet line and a motorized pump, a first selector valve in fluid communication with an inlet line at a first inlet port and in fluid communication with the motorized pump outlet via a first outlet branch at a second inlet port to receive fuel from the motorized pump outlet. The system can also include a main fuel pump in fluid communication with the first selector valve and a second selector valve, wherein the second selector valve can be in fluid communication with the main fuel pump and in fluid communication with the motorized pump outlet.

First claim

What is claimed is:

1. A fuel pump system, comprising:
an inlet line;
a motorized pump having a motorized pump inlet in fluid communication with the inlet line to receive fuel from the inlet line, and a motorized pump outlet configured to output flow from the motorized pump;
a first selector valve in fluid communication with the inlet line at a first inlet port, wherein the first selector valve is in fluid communication with the motorized pump outlet via a first outlet branch at a second inlet port to receive fuel from the motorized pump outlet, wherein the first selector valve is configured to selectively communicate the first inlet port to an outlet port, and to selectively communicate the second inlet port to the outlet port;
a main fuel pump having a main fuel pump inlet in fluid communication with the first selector valve to be downstream of the first selector valve, and having a main fuel pump outlet; and
a second selector valve in fluid communication with the main fuel pump outlet at a first input port, wherein the second selector valve is in fluid communication with the motorized pump outlet via a second outlet branch at a second input port to receive fuel from the motorized pump outlet, wherein the second selector valve is configured to selectively communicate the first input port to an output port, and to selectively communicate the second input port to the output port, wherein the output port is in fluid communication with an outlet line.

2. The system of claim 1 , wherein the first selector valve is actively controlled.

3. The system of claim 2 , wherein the first selector valve is a solenoid valve.

4. The system of claim 2 , wherein the second selector valve is a passive valve such that the second selector valve is configured to selectively communicate the first input port to an output port when a pressure from the main fuel pump exceeds a pressure from the motorized fuel pump or exceeds a set threshold.

5. The system of claim 1 , wherein each selector valve is a three-way valve.

6. The system of claim 1 , further comprising a controller configured to control a motor connected to the motorized pump to drive the motorized pump.

7. The system of claim 6 , wherein the controller is configured to operate the first selector valve to select whether the first inlet port is in communication with the outlet port, or whether the second inlet port is in communication with the outlet port.

8. The system of claim 7 , wherein the controller is configured to operate the motor and the first selector valve to provide a low flow mode wherein only the motorized pump provides flow to the outlet line, a mid-flow mode wherein only the main fuel pump provides flow to the outlet line, and a high flow mode wherein both the motorized pump and the main fuel pump are operated in series to provide flow to the outlet line.

9. The system of claim 1 , wherein the main fuel pump is a centrifugal pump.

10. The system of claim 9 , wherein the motorized pump is a centrifugal pump.

11. An aircraft, comprising:
a fuel pump system, comprising:
an inlet line;
a motorized pump having a motorized pump inlet in fluid communication with the inlet line to receive fuel from the inlet line, and a motorized pump outlet configured to output flow from the motorized pump;
a first selector valve in fluid communication with the inlet line at a first inlet port, wherein the first selector valve is in fluid communication with the motorized pump outlet via a first outlet branch at a second inlet port to receive fuel from the motorized pump outlet, wherein the first selector valve is configured to selectively communicate the first inlet port to an outlet port, and to selectively communicate the second inlet port to the outlet port;
a main fuel pump having a main fuel pump inlet in fluid communication with the first selector valve to be downstream of the first selector valve, and having a main fuel pump outlet; and
a second selector valve in fluid communication with the main fuel pump outlet at a first input port, wherein the second selector valve is in fluid communication with the motorized pump outlet via a second outlet branch at a second input port to receive fuel from the motorized pump outlet, wherein the second selector valve is configured to selectively communicate the first input port to an output port, and to selectively communicate the second input port to the output port, wherein the output port is in fluid communication with an outlet line.

12. The aircraft of claim 11 , wherein the first selector valve is actively controlled.

13. The aircraft of claim 12 , wherein the first selector valve is a solenoid valve.

14. The aircraft of claim 12 , wherein the second selector valve is a passive valve such that the second selector valve is configured to selectively communicate the first input port to an output port when a pressure from the main fuel pump exceeds a pressure from the motorized fuel pump or exceeds a set threshold.

15. The aircraft of claim 11 , wherein each selector valve is a three-way valve.

16. The aircraft of claim 11 , further comprising a controller configured to control a motor connected to the motorized pump to drive the motorized pump.

17. The aircraft of claim 16 , wherein the controller is configured to operate the first selector valve to select whether the first inlet port is in communication with the outlet port, or whether the second inlet port is in communication with the outlet port.

18. The aircraft of claim 17 , wherein the controller is configured to operate the motor and the first selector valve to provide a low flow mode wherein only the motorized pump provides flow to the outlet line, a mid-flow mode wherein only the main fuel pump provides flow to the outlet line, and a high flow mode wherein both the motorized pump and the main fuel pump are operated in series to provide flow to the outlet line.

19. The aircraft of claim 11 , wherein the main fuel pump is a centrifugal pump.

20. A fuel pump system, comprising:
an inlet line;
a motorized pump having a motorized pump inlet in fluid communication with the inlet line to receive fuel from the inlet line, and a motorized pump outlet configured to output flow from the motorized pump;
a first selector valve in fluid communication with the inlet line at a first inlet port, wherein the first selector valve is in fluid communication with the motorized pump outlet via a first outlet branch at a second inlet port to receive fuel from the motorized pump outlet, wherein the first selector valve is configured to selectively communicate the first inlet port to an outlet port, and to selectively communicate the second inlet port to the outlet port;
a main fuel pump having a main fuel pump inlet in fluid communication with the first selector valve to be downstream of the first selector valve, and having a main fuel pump outlet; and
a second selector valve in direct fluid communication with the main fuel pump outlet at a first input port, wherein the second selector valve is in fluid communication with the motorized pump outlet via a second outlet branch at a second input port to receive fuel from the motorized pump outlet, wherein the second selector valve is configured to selectively communicate the first input port to an output port, and to selectively communicate the second input port to the output port, wherein the output port is in fluid communication with an outlet line,
wherein the first and second selector valves are configured to allow flow through only the motorized pump

Assignees

• Hamilton Sundstrand Corp

Inventors

• Susca Ryan

Classifications

• F02M2037/087

  Controlling fuel pressure valve · CPC title

• F02M37/18

  characterised by provision of main and auxiliary pumps · CPC title

• F02M37/08

  electrically driven · CPC title

• F02M37/0047

  Layout or arrangement of systems for feeding fuel (fuel injection apparatus characterised by their conduits and venting means F02M55/00; fuel injection apparatus having a common rail F02M63/0225; arrangement of fuel conduits of low pressure fuel injection apparatus F02M69/462) · CPC title

• F02M37/0029

  Pressure regulator in the low pressure fuel system (pressure regulator in low-pressure injection apparatus F02M69/54) · CPC title