Multiphase fuel injector

Patent metadata

Field	Value
Publication number	US-12331933-B2
Application number	US-202318170932-A
Country	US
Kind code	B2
Filing date	Feb 17, 2023
Priority date	Feb 18, 2022
Publication date	Jun 17, 2025
Grant date	Jun 17, 2025

Abstract

A multiphase fuel injector has an injector body with a fuel inlet at a first end and a fuel outlet at a second end opposite the first end. A primary circuit disposed proximate the fuel inlet extends into a central portion of the injector body. The primary circuit is configured to receive a first flow of pressurized fuel from the fuel inlet that discharges into a spin chamber in the injector body downstream from the fuel inlet. The primary circuit is configured to impart a swirling action to the first flow of pressurized fuel. A secondary circuit is located in the injector body radially outward from the primary circuit. The secondary circuit is configured to receive a second flow of pressurized fuel from the fuel inlet that discharges into the fuel outlet. The secondary circuit is configured to impart a swirling action to the second flow of pressurized fuel.

First claim

What is claimed is:

1. A method of making a multiphase fuel injector, the method comprising the steps of:
additively manufacturing an injector body, wherein the injector body includes:
a fuel inlet at a first end of the injector body and a fuel outlet at a second end of the injector body opposite the first end;
a primary circuit disposed within the injector body proximate the fuel inlet and extending into a central portion of the injector body, the primary circuit having a fuel swirler disposed in an opening within the injector body, the fuel swirler configured to receive a first flow of pressurized fuel from the fuel inlet, direct the first flow of pressurized fuel to a spin chamber located in the injector body downstream from the fuel inlet, and impart a swirling motion to the first flow of pressurized fuel; and
a secondary circuit located within the injector body and positioned radially outward from the primary circuit, the secondary circuit configured to receive a second flow of pressurized fuel from the fuel inlet, the secondary circuit having one or more helical secondary openings formed in the injector body, the one or more helical secondary openings configured to direct the second flow of pressurized fuel toward the fuel outlet and to impart a swirling motion to the second flow of pressurized fuel,
wherein the primary circuit includes a flow plate attached to a biasing spring, wherein the flow plate blocks fuel from flowing into the secondary circuit when the biasing spring is fully extended, and allows fuel to flow into the secondary circuit when the biasing spring is compressed.

2. The method of claim 1 , wherein the fuel swirler is cylindrical with helical grooves formed in an exterior surface of the fuel swirler.

3. A method of making a multiphase fuel injector, the method comprising the steps of:
additively manufacturing an injector body, wherein the injector body includes:
a fuel inlet at a first end of the injector body and a fuel outlet at a second end of the injector body opposite the first end;
a primary circuit disposed within the injector body proximate the fuel inlet and extending into a central portion of the injector body, the primary circuit configured to receive a first flow of pressurized fuel from the fuel inlet, the primary circuit having one or more helical primary openings formed in the injector body, the one or more helical primary openings configured to direct the first flow of pressurized fuel to a spin chamber located in the injector body downstream from the fuel inlet, the one or more helical primary openings further configured to impart a swirling motion to the first flow of pressurized fuel; and
a secondary circuit located within the injector body and positioned radially outward from the primary circuit, the secondary circuit configured to receive a second flow of pressurized fuel from the fuel inlet, the secondary circuit having one or more helical secondary openings formed in the injector body, the one or more helical secondary openings configured to direct the second flow of pressurized fuel toward the fuel outlet and to impart a swirling motion to the second flow of pressurized fuel,
wherein the primary circuit includes a flow plate attached to a biasing spring, wherein the flow plate blocks fuel from flowing into the secondary circuit when the biasing spring is fully extended, and allows fuel to flow into the secondary circuit when the biasing spring is compressed.

4. The method of claim 3 , wherein the flow plate and spring are inserted into an opening within the injector.

5. A multiphase fuel injector, comprising:
an injector body having a fuel inlet at a first end of the injector body and a fuel outlet at a second end of the injector body opposite the first end;
a primary circuit disposed proximate the fuel inlet and extending into a central portion of the injector body, the primary circuit configured to receive a first flow of pressurized fuel from the fuel inlet and discharge the fuel into a spin chamber located in the injector body downstream from the fuel inlet, the primary circuit configured to impart a swirling motion to the first flow of pressurized fuel;
a secondary circuit located in the injector body radially outward from the primary circuit, the secondary circuit configured to receive a second flow of pressurized fuel from the fuel inlet and discharge the fuel into the fuel outlet, the secondary circuit configured to impart a swirling motion to the second flow of pressurized fuel,
wherein the primary circuit includes a flow plate attached to a biasing spring, wherein the flow plate blocks fuel from flowing into the secondary circuit when the biasing spring is fully extended, and allows fuel to flow into the secondary circuit when the biasing spring is compressed.

6. The multiphase fuel injector of claim 5 , wherein the biasing spring, flow plate, and primary circuit are configured to facilitate ignition of fuel at a flow rate of less than 50 pounds per hour (PPH).

7. The multiphase fuel injector of claim 5 , wherein the biasing spring, flow plate, primary circuit, and secondary circuit are together configured to facilitate a maximum fuel flow rate greater than 6,000 pounds per hour (PPH).

8. The multiphase fuel injector of claim 5 , wherein the primary circuit includes one or more helical primary openings formed in the injector body, the one or more helical primary openings configured to direct the first flow of pressurized fuel in the primary circuit to the spin chamber and to impart the swirling motion to the first flow of pressurized fuel.

9. The multiphase fuel injector of claim 8 , wherein the secondary circuit includes one or more helical secondary openings formed in the injector body, the one or more helical secondary openings configured to direct the second flow of pressurized fuel to the fuel outlet and to impart the swirling motion to the second flow of pressurized fuel.

10. The multiphase fuel injector of claim 9 , wherein the one or more helical secondary openings are located radially outward from the one or more helical primary openings.

11. The multiphase fuel injector of claim 5 , wherein the primary circuit includes a fuel swirler inserted into an opening in the injector body, the fuel swirler having one or more helical grooves in an exterior surface of the fuel swirler, the fuel swirler being configured to impart the swirling motion to fuel flowing through the primary circuit.

Assignees

• Dam Bidhan
• Crosby Mowgli
• Sarker Sudipa
• Woodward Inc

Inventors

• Dam Bidhan
• Crosby Mowgli
• Sarker Sudipa

Classifications

• F16K17/04

  spring-loaded · CPC title

• F16K21/04

  Self-closing valves, i.e. closing automatically after operation {(pneumatic tools B25B9/00)} · CPC title

• F02C7/232

  Fuel valves {(control of fuel supply by means of fuel metering valves F02C9/263)}; Draining valves or systems (valves in general F16K) · CPC title

• F23R3/343

  Pilot flames, i.e. fuel nozzles or injectors using only a very small proportion of the total fuel to insure continuous combustion (ignition in gas-turbine plants F02C7/264; pilot flame igniters F23Q9/00) · CPC title

• F23R3/283

  Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances · CPC title