Device and method for fuel injection using swirl burst injector

Patent metadata

Field	Value
Publication number	US-11020758-B2
Application number	US-201715656456-A
Country	US
Kind code	B2
Filing date	Jul 21, 2017
Priority date	Jul 21, 2016
Publication date	Jun 1, 2021
Grant date	Jun 1, 2021

Abstract

Flow blurring injection utilizes a two-phase concept to generate fine sprays immediately at the interior exit, rather than a typical jet which gradually disintegrates into ligaments and then finer droplets for a conventional injector. Therefore, clean combustion is achieved with the FB injection for fuels with distinct properties without fuel preheating or hardware modification. However, in addition to the droplets, the FB injection also produces ligaments for highly viscous liquids and relatively larger droplets at spray edge, resulting in difficulty in sustaining the flame and performs incomplete combustion and higher emissions close to the combustor all. The disclosed swirl burst injector and method utilizes the advantages of FB injection and swirl atomization to further improve atomization, and overcomes the limitations of FB injection, providing a sustainable way to use both conventional and alternative fuels with improved efficiency and minimized emissions. The fine atomization of the present invention can be also used in various applications where fine sprays are needed.

First claim

I claim:

1. A swirl burst fuel injector comprising:
(a) an internal liquid tubing, comprising a liquid tip end with chamfered outside wall;
(b) an injector head;
(c) a chamfered injector exit;
(d) a bubble generation zone;
(e) one or more swirling paths;
(f) at least two swirling vanes;
(g) an atomizing gas channel;
(h) an injector orifice;
wherein a gap is present between the injector orifice and the liquid tip end, wherein gas bifurcation occurs wherein a portion of a gas flows into the bubble generation zone and a remaining portion of said gas exits through the chamfered injector exit;
wherein bubbles are formed in the portion of the gas flowing into the bubble generation zone;
wherein the at least two swirling vanes are contained in each swirling path; and
wherein at least one of the swirling paths delivers gas into the bubble generation zone in a swirling mode;
wherein a mixing of the gas and the liquid occurs prior to its arrival at the chamfered injector exit;
wherein said bubbles undergo a pressure drop while passing through the chamfered injector exit; and
wherein said pressure drop causes said bubbles to burst into fine droplets upon exiting the chamfered injector exit.

2. The swirl burst fuel injector of claim 1 , wherein the size of the gap between the injector orifice and the liquid tip end is equal to or less than one-fourth the size of the diameter of the internal liquid tubing.

3. The swirl burst fuel injector of claim 1 , wherein at least one of the swirling paths delivers gas outside of the injector through the injector exit in swirling mode.

4. The swirl burst fuel injector of claim 1 , wherein the swirling vanes are angled; and wherein said angle and vane dimension are identified as the swirl number.

5. The swirl burst fuel injector of claim 4 , wherein the swirl number is at least 1.5.

6. The swirl burst fuel injector of claim 1 , wherein at least two of the swirling vanes are located on the chamfered outer wall of the injector orifice and that of the liquid tube tip; and
wherein at least two of the swirling vanes on the injector orifice and the liquid tube tip operate in the same direction.

7. The swirl burst fuel injector of claim 1 , wherein at least two of the swirling vanes are located on the injector orifice and the liquid tube tip; and
wherein at least two of the swirling vanes on the injector orifice and the liquid tube tip operate in different directions.

8. The swirl burst fuel injector of claim 1 , wherein during operation of the swirl burst fuel injector, a gas and a liquid pass through said injector; and wherein a ratio of the gas' mass and the liquid's mass is 4.0.

9. The swirl burst fuel injector of claim 1 , wherein at least one of the swirling paths also delivers gas into a spray field of the injector exit in a swirling mode.

10. The swirl burst fuel injector of claim 1 , wherein the internal liquid tubing's inside diameter is equal to the injector orifice's diameter.

11. The swirl burst fuel injector of claim 1 , wherein the liquid tip is located upstream of the injector orifice.

12. The swirl burst fuel injector of claim 1 , wherein the injector head comprises an orifice located in the injector head's center, and where the chamfered injector exit is constructed around the orifice on the orifice's outer wall.

Assignees

• Univ Louisiana At Lafayette

Inventors

• Jiang Lulin

Classifications

• B05B1/3405 Primary

  to produce swirl · CPC title

• F23D11/383

  with swirl means · CPC title

• F23D11/007

  combination of means covered by sub-groups F23D11/10 and F23D11/24 · CPC title

• F23C2900/99009

  Combustion process using vegetable derived fuels, e.g. from rapes · CPC title

• F23D11/12

  characterised by the shape or arrangement of the outlets from the nozzle · CPC title