Patent Application
20210293408
The present invention relates to an apparatus and method for injectors for use in combustion systems. This technology is considered for systems requiring the introduction of combinations of fuel-fuel, fuel-inert, oxidizer-inert, or oxidizer-oxidizer into the combustion chamber. Inert, in this case, includes the classic definition plus complete combustion product species such as water/steam and carbon dioxide. Supercritical CO2 combustion systems are the primary application for this technology but it can be employed in any system employing multiple gas streams.
Supercritical CO2 systems are unique from any other traditional combustion system in that they have large amounts of combustion product gas (CO2) which is typically recirculated from the exhaust back into the inlet of the combustor. Combustion product gases are essentially inert in nature which, when introduced into the combustion chamber in proximity of the fuel or oxidizer, can inhibit reactions. This is of particular interest when the combustion process has high flame speeds, very short ignition delay times, or are in an autoignition condition. These considerations apply to supercritcal CO2 systems, but also to many other combustion systems.
The following description is merely exemplary in nature and is in no way intended to limit the invention, its application, or uses. While the description is designed to permit one of ordinary skill in the art to make and use the invention, and specific examples are provided to that end, they should in no way be considered limiting. It will be apparent to one of ordinary skill in the art that various modifications to the following will fall within the scope of the appended claims. The present invention should not be considered limited to the presently disclosed embodiments, whether provided in the examples or elsewhere herein.
The present invention relates to an apparatus and method to inject reactants into a combustion chamber in such a way that combustion is locally inhibited. Delaying the reaction moves the high temperature combustion species and reactions away from the injectors and other combustion chamber hardware improving durability and survivability of such hardware.
An injector in one preferred embodiment of the invention, comprises an outer cylindrical tube comprising an inner diameter and a first end and a second end, wherein said first end is connected to a source of a first non-solid and said second end comprises an annular or circular exit; and an inner cylindrical tube positioned within said outer cylindrical tube, wherein said inner cylindrical tube comprises an inner diameter and a first end and a second end wherein said first end is connected to a source of a second non-solid and said second end comprises an annular or circular exit; and wherein said second end of said inner cylindrical tube is positioned relative to said outer cylindrical tube such that said second end of said inner cylindrical tube is located an axial distance away from said second end of said outer cylindrical tube; and wherein said inner diameter of said outer cylindrical tube is configured to swirl said first non-solid and said inner diameter of said second cylindrical tube is configured to swirl said second non-solid such that said first non-solid and said second non-solid remain swirled and stratified into separate layers of flow for each gas as they flow through the exits of the inner and outer tubes. Swirl is defined as any component of velocity not aligned with the tube axis and includes zero. In preferred embodiments, the first non-solid may comprise supercritical CO2 and the second non-solid may comprise CH4.
A method of injecting an inert into a combustion chamber comprising at least one injector comprising an outer tube and an inner tube positioned within said outer tube, in one preferred embodiment, comprises the steps of: flowing an inert into said outer tube of said at least one injector; swirling the inert as it flows through said outer tube; flowing a non-solid into said inner tube of said at least one injector; swirling the non-solid as it flows through said inner tube; injecting the swirled inert and swirled non-solid from said outer and inner tubes into said combustion chamber such that the swirled inert delays the mixing of swirled non-solid in said combustion chamber thereby preventing reactions for some distance beyond the point of injection of said at least one injector. In preferred embodiments, the non-solid may comprise fuel (e.g. CH4), oxidizer and the inert may comprise supercritical CO2 or steam.
A method of injecting a non-solid into a combustion chamber comprising at least one injector comprising an outer tube and an inner tube positioned within said outer tube, in one preferred embodiment of the invention, comprises the steps of: flowing the non-solid into said outer tube of said at least one injector to form an outer stream of the non-solid; flowing the non-solid into said inner tube of said at least one injector to form an inner stream of the non-solid; injecting the non-solid from said outer and inner tubes into said combustion chamber such that the inner and outer streams enter into said combustion chamber with enhanced turbulence caused by the inner and outer streams experiencing high shear forces due to either a difference in axial velocity, a difference in swirl velocity or direction or a combination of these effects, downstream of said at least one injector.
The non-solid may comprise a fuel or an oxidizer in preferred embodiments. Optionally, preferred methods may further comprise swirling the non-solid as it flows through said outer tube, or swirling the non-solid as it flows through the inner tube, or swirling the non-solid as it flows through both the inner and the outer tube. In other preferred embodiments two different fuels or two different oxidizers may be flowed, and optionally swirled as they flow, through the inner and outer tubes wherein one fuel or oxidizer is flowed through the outer tube and a different fuel or oxidizer is flowed through the inner tube.
The present design provides a small delay to the combustion process while being highly effective at mixing the reactants. This can be accomplished by using the weights of the non-solids or gases along with swirling the non-solids or gases to keep reactants stratified. Large numbers of discrete injection elements or injectors can also be utilized. Both the fuel and oxidizer can be stratified: fuel#1-fuel#2, fuel-inert, oxidizer-inert, or oxidizer#1-oxidizer#2. The present injectors can be used in any non-premixed combustor designs.
Swirling can be initiated by tangential entry, rifling, or helical ribbon inserts. Unlike typical injectors, the present injectors comprise an outer tube forming an exit of the injector, and an inner tube located within the outer tube that includes its own exit that stops short of the exit of the outer tube of the injector. In one preferred embodiment, the inner and outer tubes can be cylindrical. The exits of the inner cylindrical tubes are designed to minimize the mixing between the two streams. As the two fluids continue in the outer tube, the mixing of the streams is minimized by proper selection of the temperature, density, velocity, and swirl of the streams. In one preferred embodiment, the exits of the inner and outer tubes can be the annular ends of the cylindrical tubes. One of ordinary skill in the art would appreciate that other configurations for the tubes and exits could be incorporated in the design.
In one preferred embodiment, stratification can be accomplished by using temperature differential to effect the densities so as to aid in stratification.
In one preferred embodiment of the invention, supercritical CO2 and CH4 can be swirled the same amount in an injector comprising an outer tube forming an exit of the injector, and an inner tube that stops short of the exit of the injector. The CH4 can be introduced into the combustion chamber through the inner tube of the injectors and the supercritical CO2 can be introduced through the outer tube of the injector. The supercritical CO2 and CH4 can be swirled in the injector by tangential entry of the supercritical CO2 and CH4 into the injector tubes, rifling on the inner surface of the inner and outer injector tubes, helical ribbon inserts within the inner and outer injector tubes, or a combination of such elements. The supercritical CO2 and CH4 can be supplied to the injector from separate sources of supply operably connected to the inner and outer tubes respectively.
According to the present design, a plurality of injectors can be utilized within a combustion chamber, or such that the exits of the injectors flows gases into the combustion chamber.
With reference to
In preferred embodiments, said first gas may be an oxidizer or a fuel, and said second gas may be inert (non-participating). In the preferred embodiment depicted in
In one preferred embodiment, as depicted in
With reference to
While the present invention has been described in terms of the above examples and detailed description, those of ordinary skill will understand that alterations may be made within the spirit of the invention. It is to be understood that the invention may assume various alternative variations and step sequences, except where expressly specified to the contrary. It is also to be understood that the specific devices and processes illustrated in the attached drawings and described in the specification are simply exemplary embodiments or aspects of the invention. Although the invention has been described in detail for the purpose of illustration based on what is currently considered to be the most practical and preferred embodiments or aspects, it is to be understood that such detail is solely for that purpose and that the invention is not limited to the disclosed embodiments or aspects, but, on the contrary, is intended to cover modifications and equivalent arrangements that are within the spirit and scope thereof. For example, it is to be understood that the present invention contemplates that to the extent possible, one or more features of any embodiment or aspect can be combined with one or more features of any other embodiment or aspect.
The present application claims priority to U.S. Provisional Patent Application No. 62/991,362, filed on Mar. 18, 2020, the disclosure of which is hereby incorporated by reference in its entirety.
| Number | Date | Country | |
|---|---|---|---|
| 62991362 | Mar 2020 | US |
