Liquid swirler flow control

Patent metadata

Field	Value
Publication number	US-9310073-B2
Application number	US-201213481411-A
Country	US
Kind code	B2
Filing date	May 25, 2012
Priority date	Mar 10, 2011
Publication date	Apr 12, 2016
Grant date	Apr 12, 2016

Abstract

A flow directing device for imparting swirl on a fluid includes a flow directing body having a first surface and opposed second surface. A flow channel is defined in the first surface of the flow directing body for conducting fluids flowing through the flow directing body. The flow channel includes a channel surface set in from the first surface. A swirl bore extends though the flow directing body from the channel surface to the second surface of the flow directing body at an oblique angle relative to the channel surface for imparting a tangential swirl component onto fluids flowing through the swirl bore. Having an asymmetrical terminus portion of the channel surface, and positioning of the swirl bore within the terminus portion, allow control of the swirl direction for flow within the terminus portion and swirl bore.

First claim

What is claimed is:

1. An injector for producing an atomized spray of liquid comprising:
a) an annular injector body;
b) an annular first flow directing body mounted inboard of the injector body, the first flow directing body including an inboard surface and opposed outboard surface,
wherein a plurality of flow channels are defined in the outboard surface of the first flow directing body for conducting fluids flowing through the first flow directing body,
wherein each flow channel includes a channel floor and a sidewall extending from the channel floor to the outboard surface of the first flow directing body, and
wherein a swirl bore extends through the first flow directing body from each channel floor to the inboard surface of the first flow directing body at an oblique angle relative to the channel floor for imparting a tangential swirl component onto fluids flowing through the swirl bore; and

c) an annular second flow directing body mounted radially inboard of the first flow directing body and including an outboard surface with an annular swirl chamber defined therein for receiving liquid from the swirl bores of the first flow directing body to form a swirling sheet of liquid for atomization downstream of the second flow directing body;
wherein a terminus section of each flow channel defines a dogleg with respect to the flow channel upstream of the terminus section;
wherein the dogleg is angled relative to the flow channel upstream of the dogleg;
wherein the swirl bore of each flow channel defines a swirl bore radius, wherein the terminus section of each flow channel defines a semi-circular pad in the channel floor having a radius between about two to about five times the swirl bore radius.

2. The injector as recited in claim 1 , wherein the flow channel upstream of each dogleg defines a respective first axis, wherein each respective dogleg defines a second axis angled relative to the first axis, and wherein the swirl bore opening in each channel floor has a center that is offset from a radial center point defined by the semi-circular pad in a direction perpendicular to the second axis by about one swirl bore radius or more and about two times the swirl bore radius or less.

3. The injector as recited in claim 1 , wherein the flow channel upstream of each dogleg defines a respective first axis, wherein each respective dogleg defines a second axis angled relative to the first axis, and wherein the swirl bore opening in each channel floor has a center that is offset from a radial center point defined by the semi-circular pad in a direction perpendicular to the second axis by zero or more times the swirl bore radius downstream relative to the flow channel.

4. The injector as recited in claim 1 , wherein the flow channel upstream of each dogleg defines a respective first axis, and wherein the swirl bore opening in each channel floor has a center that is offset from a radial center point defined by the semi-circular pad in a direction along a second axis that is angled relative to the first axis by about one swirl bore radius or less.

Assignees

• Buelow Philip E O
• Siders Randall Duane
• Bretz David H
• Thomson Neal A
• Rolls Royce Plc

Inventors

• Buelow Philip E O
• Siders Randall Duane
• Bretz David H
• Thomson Neal A

Classifications

• F23D11/107 Primary

  at least one of both being subjected to a swirling motion · 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

• F23R3/28

  characterised by the fuel supply (burners F23D) · CPC title

• F23D2900/11101

  Pulverising gas flow impinging on fuel from pre-filming surface, e.g. lip atomizers · CPC title