US20200041130A1

Movatterモバイル変換

Info

Publication number: US20200041130A1
Application number: US16/051,168
Authority: US
Inventors: Benjamin J. Boyce; Michael T. Abbott
Original assignee: Hotstart Inc
Current assignee: Hotstart Inc
Priority date: 2018-07-31
Filing date: 2018-07-31
Publication date: 2020-02-06
Also published as: US20200040762A1; US20200041131A1; US11168888B2

Abstract

An engine heater system for heating a diesel engine of a vehicle. The engine heater system including a gas turbine. A heat exchanger communicatively coupled to an exhaust of the gas turbine. An electric generator including connection members to couple to a battery of the vehicle, and a shaft rotatably attached between the gas turbine and the electric generator. The heat exchanger utilizes the exhaust of the gas turbine to keep the diesel engine of the vehicle within a desired temperature range, and the electric generator charges the battery when the gas turbine rotates the shaft.

Description

This application claims the benefit of priority to provisional U.S. Patent Application Ser. No. 62/712,716, filed on Jul. 31, 2018 and entitled “Engine Heaters, Combustor Systems, and Rotary Atomizers”, which is herein incorporated by reference in its entirety.

BACKGROUND

Engine heaters maintain a temperature of an internal combustion engine. For example, fuel fired heaters exist which are used onboard vehicles, such as locomotives, trucks, automobiles, ships, etc. in order to maintain the combustion engines within a desired temperature range.

In some onboard applications, fuel fired heaters may employ a fan and a combustor in order to maintain the combustion engines within a desired temperature range. The fan may be employed by the fuel fired heaters to provide air to the combustor. However, the fan may be a parasitic load on a battery of the vehicle. For example, the fan of the fuel fired heater may be powered by the battery of the vehicle, reducing a charge of the battery of the vehicle.

Moreover, the fuel fired heaters may employ a pump in order to maintain the combustion engines within a desired temperature range. The pump may be employed by the fuel fired heaters to provide for pumping an engine oil or an engine coolant. However, the pump may also be a parasitic load on the battery of the vehicle. For example, the pump of the fuel fired heater may be powered by the battery of the vehicle, again reducing a charge of the battery of the vehicle.

Thus, there remains a need to develop new fuel fired heaters that are more efficient and not a parasitic load on the vehicle the fuel fired heaters are maintaining within a desired temperature range.

SUMMARY

This summary is provided to introduce simplified concepts for systems, devices, and components of the disclosure which are further described below in the Detailed Description. This summary is not intended to identify essential features of the claimed subject matter, nor is it intended for use in determining the scope of the claimed subject matter.

In an embodiment, an engine heater system may provide for heating a diesel engine of a vehicle (e.g., a locomotive, a ship, or a truck, etc.). The engine heater system may be located onboard of the vehicle and may include a heat exchanger communicatively coupled to an exhaust of a gas turbine. The heat exchanger may utilize the exhaust of the gas turbine to keep the diesel engine of the vehicle within a desired temperature range. A shaft may be rotatably attached between the gas turbine and an electric generator, and the generator may charge the battery when the gas turbine rotates the shaft.

In an embodiment, an engine heater system may include a heat exchanger communicatively coupled to an exhaust of a gas turbine. The heat exchanger may utilize the exhaust of the gas turbine to keep the diesel engine of the vehicle within a desired temperature range.

In an embodiment, a shaft may be rotatably attached between a gas turbine and an electric generator. When the gas turbine rotates the shaft, the generator charges a battery of the vehicle.

In an embodiment, a combustor system may include a toroidal-shaped combustion zone having an outside perimeter opposite a central hole. An airflow channel may interface with the outside perimeter of the toroidal-shaped combustion zone. The airflow channel may provide for delivering air to the toroidal-shaped combustion zone. An atomizer component may be fixed to a portion of a shaft extending into the central hole of the toroidal-shaped combustion zone. The atomizer component may provide for atomizing a liquid fuel into the toroidal-shaped combustion zone when the shaft is rotated.

In an embodiment, a combustor system may include a toroidal-shaped combustion zone having an outside perimeter opposite a central hole. An atomizer component may be fixed to a portion of a shaft extending into the central hole of the toroidal-shaped combustion zone. The atomizer component may provide for atomizing a liquid fuel into the toroidal-shaped combustion zone when the shaft is rotated.

In an embodiment, a combustor system may include a toroidal-shaped combustion zone having an outside perimeter opposite a central hole. An airflow channel may interface with the outside perimeter of the toroidal-shaped combustion zone. The airflow channel may provide for delivering air to the toroidal-shaped combustion zone.

In an embodiment, a rotary atomizer may include an atomizer component fixable to a shaft having a longitudinal axis. The atomizer component may include a plate and a wall extending from a perimeter of the plate. The wall may have a height varying curvilinearly along the perimeter of the plate. The plate may extend transversely to the longitudinal axis of the shaft, and the wall may extend from the plate in a direction of extension of the longitudinal axis of the shaft. When the shaft is rotated and a liquid is introduced to the plate of the atomizer component, the varying height of the wall causes the liquid to atomize away from the atomizer component.

In an embodiment, an atomizer component may include a plate and a wall extending from a perimeter of the plate. The wall may have a height varying curvilinearly along the perimeter of the plate. When the atomizer component is rotated and a liquid is introduced to the plate of the atomizer component, the height of the wall varying curvilinearly along the perimeter of the plate atomizes the liquid away from the atomizer component.

In an embodiment, an atomizer component may include a plate and a wall extending from a perimeter of the plate. The wall may have a plurality of peaks interspersed by a plurality of troughs along the perimeter of the plate. When the atomizer component is rotated, the plurality of peaks interspersed by the plurality of troughs along the perimeter of the plate atomizes a liquid away from the atomizer component.

BRIEF DESCRIPTION OF THE DRAWINGS

The detailed description is described with reference to the accompanying figures. The use of the same reference numbers in different figures indicates similar or identical items.

FIG. 1 illustrates an example engine heater system for heating a diesel engine of a vehicle according to an embodiment of the instant disclosure.

FIG. 2 illustrates a section view of an example combustor system according to an embodiment of the instant disclosure.

FIG. 3 illustrates a perspective view of an example atomizer component according to an embodiment of the instant disclosure.

FIG. 4 illustrates a section view of another example combustor system according to an embodiment of the instant disclosure.

DETAILED DESCRIPTIONOverview

As noted above, engine heaters may employ fans and/or pumps that are parasitic loads on batteries of the vehicles the engine heaters are maintaining within a desired temperature range. This disclosure is directed to engine heater systems, for heating a diesel engine of a vehicle for example, that are not a parasitic load on the vehicles, and therefore are more efficient. In an embodiment of the instant application, the engine heater systems include a heat exchanger communicatively coupled to an exhaust of a gas turbine and a shaft rotatably attached between the gas turbine and an electric generator. The heat exchanger utilizing the exhaust of the gas turbine to keep the diesel engine of the vehicle within a desired temperature range, and the generator charging the battery of the vehicle when the gas turbine rotates the shaft.

Traditional engine heaters have been installed onboard of vehicles and arranged to keep the diesel engine within a desired temperature range via a fan receiving electric power from the battery of the vehicle. For example, an electric fan powered by a battery of the vehicle may be employed with a combustor in order to maintain the diesel engine within a desired temperature range. Moreover, traditional engine heaters may be configured to use an electric pump also powered by a battery of the vehicle to maintain the diesel engine within a desired temperature range. Because traditional engine heaters utilize a battery of the vehicle to power fans and/or pumps, they are parasitic to the vehicle and inefficient at maintaining the diesel engine of the vehicle with a desired temperature range. Having fans and/or pumps that are not powered by a battery of the vehicle to keep an engine with in a desired temperature range, may allow for optimizing a vehicle's operation and reduce power consumption costs.

Accordingly, this disclosure describes engine heater systems that may result in a more efficient operation of the vehicle. In an embodiment, a heat exchanger may be communicatively coupled to an exhaust of a gas turbine, the heat exchanger utilizing the exhaust of the gas turbine to keep the engine of the vehicle within a desired temperature. Further, an electric generator charges a battery of the vehicle when the gas turbine rotates a shaft rotatably attached between the gas turbine and the electric generator.

While this application describes implementations that are described in the context of an onboard engine heater system for maintaining a diesel engine of a vehicle within a desired temperature, the implementations described herein may be used in other environments and are applicable to other contexts. For example, the engine heater systems may be located at any desired location, including with a generator (e.g., backup generator) located at a server farm, a hospital, a high-rise building, remote cell tower site, an urban cell tower site, an oil site, a gas site, etc.

In an embodiment, the engine heater systems may include a trapped vortex combustor. For example, a gas turbine of the engine heater system may be communicatively coupled to a trapped vortex combustor. The trapped vortex combustor may include a toroidal-shaped combustion zone having an outside perimeter opposite a central hole. An airflow channel may interface with the outside perimeter of the toroidal-shaped combustion zone for delivering air to the toroidal-shaped combustion zone. An atomizer component may be fixed to a portion of a shaft of the engine heater system. The atomizer component may provide for atomizing a liquid fuel into the toroidal-shaped combustion zone when the gas turbine rotates the shaft.

In an embodiment, a trapped vortex combustor may include an atomizer component including a plate and a wall extending from a perimeter of the plate. The wall may have a height varying curvilinearly along the perimeter of the plate. When the shaft is rotated and a liquid is introduced to the plate of the atomizer component, the varying height of the wall causes the liquid to atomize away from the atomizer component.

Example Engine Heaters

FIG. 1 illustrates an exampleengine heater system100 for heating a diesel engine of avehicle102. WhileFIG. 1 illustrates thevehicle102 is a locomotive (e.g., a diesel electric locomotive), thevehicle102 may be a ship, a truck, a car, etc. Theengine heater system100 may be onboard of thevehicle102. For example, theengine heater system100 may be arranged on thevehicle102 for heating the diesel engine of thevehicle102.

Theengine heater system100 may include agas turbine104. Aheat exchanger106 may be communicatively coupled to anexhaust108 of thegas turbine104. Anelectric generator110 includingconnection members112 may be coupled to abattery114 of thevehicle102. Thebattery114 may be a battery bank of a diesel electric locomotive. Ashaft116 may be rotatably attached between thegas turbine104 and theelectric generator110. Acombustor system118 may be communicatively coupled to thegas turbine104. Thecombustor system118 may be a trapped vortex combustor (discussed in more detail below with regard toFIG. 2). Thecombustor system118 may provide for heating air. The heated air then acts on the blades of thegas turbine104 to rotate thegas turbine104. The rotatinggas turbine104 rotates theshaft116. When thegas turbine104 rotates theshaft116, theelectric generator110 charges thebattery114. Moreover, theheat exchanger106 utilizes theexhaust108 of thegas turbine104 to keep the diesel engine of thevehicle102 within a desired temperature range.

In one example, theheat exchanger106 may utilize theexhaust108 of thegas turbine104 to heat an engine coolant of the diesel engine of thevehicle102 to keep the diesel engine within the desired temperature range. In another example, theheat exchanger106 may utilize theexhaust108 of thegas turbine104 to heat an engine oil of the diesel engine of thevehicle102 to keep the diesel engine within the desired temperature range. In another example, theheat exchanger106 may utilize theexhaust108 of thegas turbine104 to heat an engine coolant of the diesel engine of thevehicle102 to keep a cab of thevehicle102 at a desired temperature.

FIG. 1 illustrates theengine heater system100 may include acompressor120. Thecompressor120 may be attached to theshaft116. Thecompressor120 may forceair122 to thecombustor system118. When thegas turbine104 rotates theshaft116, theshaft116 rotates thecompressor120 to force theair122 to thecombustor system118.

Theconnection members112 may further coupleelectric generator110 to anelectric motor124 of acoolant pump126. When thegas turbine104 rotates theshaft116, theelectric generator110 may power theelectric motor124 of the-coolant pump126. Thecoolant pump126 may forceengine coolant128 through theheat exchanger106. Theexhaust108 of thegas turbine104 may then heat theengine coolant128 forced through theheat exchanger106 by thecoolant pump126. Theheated engine coolant128 may be used to keep the diesel engine within the desired temperature range. WhileFIG. 1 illustrates ancoolant pump126 for forcingengine coolant128 through theheat exchanger106, an oil pump (not shown) may be powered by theelectric generator110 to force engine oil through theheat exchanger106. In such an embodiment, theexhaust108 of thegas turbine104 may heat the engine oil forced through theheat exchanger106 by the oil pump. The heated engine oil may be used to keep the diesel engine within the desired temperature range. Theheat exchanger106 may be further communicatively coupled to anexhaust pipe130 for venting the exhaust. WhileFIG. 1 illustrates theexhaust108 of thegas turbine104 heating an engine oil, theexhaust108 of thegas turbine104 may heat a hydraulic oil, a fuel (e.g., diesel fuel), etc.

Because theengine heater system100 includes thegas turbine104 that rotates thecompressor120, charges thebattery114, and powers thecoolant pump126, rather than drawing power from thebattery114, theengine heater system100 is not a parasitic load on thebattery114 of thevehicle102 and is more efficient. For example, because thegas turbine104 rotates thecompressor120 and powers thecoolant pump126, theengine heater system100 does not require power from thebattery114 to run thecompressor120 or thecoolant pump126, and instead charges thebattery114 making theengine heater system100 more efficient.

Example Combustor Systems

FIG. 2 illustrates asection view200 of anexample combustor system202. Thecombustor system202 may be implemented in theengine heater system100 ofFIG. 1. Thecombustor system202 may be the same as thecombustor system118 discussed above.

FIG. 2 illustrates thecombustor system202 may include a toroidal-shapedcombustion zone204. The toroidal-shapedcombustion zone204 may have anoutside perimeter206 opposite acentral hole208. Anairflow channel210 may interface with theoutside perimeter206 of the toroidal-shapedcombustion zone204 for delivering theair122 to the toroidal-shapedcombustion zone204. For example, thecompressor120 may force theair122 through theairflow channel210 for delivering theair122 to the toroidal-shapedcombustion zone204. Thecompressor120 may force an amount of air that is dependent on theengine heater system100 output and fuel burned. In one example, theengine heater system100 may be a 15 kW (kilowatt) heater and thecompressor120 may force about 14 cfm (cubic feet per minute) through theairflow channel210. In another example, theengine heater system100 may be a 30 kW heater and thecompressor120 may force about 28 cfm through theairflow channel210. The toroidal-shapedcombustion zone204 may heat theair122. For example, the toroidal-shapedcombustion zone204 may contain aflame vortex212 that heats theair122 delivered by theairflow channel210. Theairflow channel210 may deliver theheated air122 to thegas turbine104.

At least aportion214 of theshaft116 may extend into thecentral hole208 of the toroidal-shapedcombustion zone204. Anatomizer component216 may be fixed to theportion214 of theshaft116. Theatomizer component216 may provide for atomizing218 aliquid fuel220 into the toroidal-shapedcombustion zone204 when theshaft116 is rotated. For example, when theshaft116 is rotated by thegas turbine104, theshaft116 rotates the theatomizer component216 and theliquid fuel220 that is introduced to therotating atomizer component216 is atomized218 into the toroidal-shapedcombustion zone204. When theshaft116 is rotated, theshaft116 may rotate at about 6000 revolutions per minute (rpm).

Thegas turbine104 may be communicatively coupled to the toroidal-shapedcombustion zone204. As discussed above, theheat exchanger106 may be communicatively coupled to an exhaust of thegas turbine104. Theportion214 of theshaft116 extending into thecentral hole208 of the toroidal-shapedcombustion zone204 may be a first portion of theshaft116, and a second portion of theshaft116 may be attached to thegas turbine104.

At least aportion222 of atube224 may be arranged in thecentral hole208 of the toroidal-shapedcombustion zone204. Thetube224 may provide for introducing theliquid fuel220 to theatomizer component216. For example, thetube224 may have anend226 arranged proximate to theatomizer component216 for dispensing theliquid fuel220 onto theatomizer component216. Thetube224 may have an inside diameter of about 0.09 inch, and theliquid fuel220 may be pressurized, inside of thetube224, at about 30 pounds per square inch (psi) for introducing theliquid fuel220 to theatomizer component216.

In an embodiment, theatomizer component216 may include aplate228 fixed to theportion214 of theshaft116. The breadth of theplate228 may extend in a direction transversely to a direction of extension of thelongitudinal axis230 of theshaft116. Awall232 may extend from an outer perimeter of theplate228. Thewall232 may extend from theplate228 in the direction of extension of thelongitudinal axis230 of theshaft116. Thewall232 may have a varying height that causes theliquid fuel220 to atomize218 away from theatomizer component216 when therotateable shaft116 is rotated (discussed in more detail below with regard toFIGS. 2 and 3).

Because thecombustor system202 includes thelarge tube224 for dispensing theliquid fuel220 to theatomizer component216, thecombustor system202 is well-suited suited for use with dirty liquid fuel (e.g., liquid fuel having debris), less susceptible to thetube224 becoming clogged, and incurs relatively less maintenance as compared to a plurality of smaller nozzles having smaller orifices that may atomize theliquid fuel220 into the toroidal-shapedcombustion zone204. For at least these reasons, thecombustor system202 is more efficient than combustor systems employing a plurality of smaller nozzles to atomize the liquid fuel.

While this application describes thecombustor system202 being implemented in theengine heater system100 ofFIG. 1, thecombustor system202 described herein may be used in other environments and is applicable to other contexts. For example, thecombustor system202 may be implemented in a gas-powered generator, including with a gas-powered generator located on an airplane, on a ship, in a submarine, in a generator (e.g., backup generator) located at a server farm, a hospital, a high-rise building, remote cell tower site, an urban cell tower site, an oil site, a gas site, etc.

Example Atomizer Components

FIG. 3 illustrates aperspective view300 of anexample atomizer component302. Theatomizer component302 may be implemented in thecombustor system202 ofFIG. 2. Theatomizer component302 may be the same as theatomizer component216 discussed above.

FIG. 3 illustrates theatomizer component302 may include aplate304. Awall306 may extend from aperimeter308 of theplate304. Theperimeter308 of theplate304 may have a curvilinear shape. In an example embodiment, an outside diameter of theplate304 may be about 3 inches. However, the size of the diameter may vary according to the specific and varying needs of different implementations of theatomizer component302. Thewall306 may have aheight310 varying curvilinearly 312 along theperimeter308 of theplate304. For example, thewall306 may have a plurality ofpeaks314 interspersed by a plurality oftroughs316 along the upper end (edge318) of thewall306 as it extends around theperimeter308 of theplate304. Stated otherwise, a profile of thewall306 may have a plurality of teeth spaced consecutively along a length of thewall306. The varyingheight310 of thewall306 may have a difference of about 0.2 inches between a first height of the varyingheight310 of thewall306 and a second height of the varyingheight310 of thewall306. For example, a peak of the plurality ofpeaks314 and a trough of the plurality oftroughs316 may have a difference in height of about 0.2 inches. Adjacent peaks of the plurality ofpeaks314 may be separated a distance of about 0.6 inches. Likewise, adjacent troughs of the plurality oftroughs316 may be separated a distance of about 0.6 inches. Accordingly, each peak of the plurality ofpeaks314 may be separated by a distance of about 0.3 inches from an adjacent trough of the plurality oftroughs316. In an embodiment, each peak of the plurality ofpeaks314 and each trough of the plurality oftroughs316 may have a radius of about 0.2 inches. In an alternative embodiment (not shown), the radius may vary from peak to peak, either uniformly or selectively.Side profile view322 illustrates the profile of thewall306 may have a plurality of teeth spaced consecutively along a length of thewall306.

The varyingheight310 of thewall306 defines theedge318 of thewall306. For example, the plurality ofpeaks314 interspersed by the plurality oftroughs316 along theperimeter308 of theplate304 may define theedge318 of thewall306. In an example embodiment, theedge318 of thewall306 may have a perimeter length of about 11 inches, a thickness of about 0.1 inch, and an overall height of about 0.5 inch. Theedge318 of thewall306 may be a sharp edge to enhance the atomization of the fluid. However, the sizes of the perimeter, thickness, and overall height may vary according to the specific and varying needs of different implementations of theatomizer component302.

WhileFIG. 3 illustrates the varyingheight310 of thewall306 having a smooth repetitive oscillational shape (e.g., sinusoidal shape), the varyingheight310 of thewall306 may have other shapes. For example, the varyingheight310 of thewall306 may have a sharp repetitive oscillational shape, a smooth irregular (e.g., non-repetitive) oscillational shape, a sharp irregular oscillational shape, etc. For the purposes of this disclosure, a “sharp” shape may refer to the change in direction of the wall height going into or out of a trough as being non-curvilinear or non-radial, and instead the change in direction is abruptly transverse.

Theatomizer component302 may be fixed to a shaft (e.g., shaft116) via a mountingportion320 arranged with theplate304. In an example, the mountingmember320 may simply include an opening through theplate304, where the opening is sized to receive at least a portion of the shaft. In another example, the mountingportion320 may further include a coupler (not shown) to couple with a mating coupler attached to at least a portion of the shaft. In another example, the mountingmember320 may further include a collar (not shown) to receive at least a portion of the shaft. In another example, the mountingmember320 may further include a fastener (e.g., a threaded fastener, a snap-fit fastener, a press-fit fastener, a friction-fit fastener, etc.) (not shown) to fasten to a mating fastener attached to at least a portion of the shaft. In an example embodiment, the mountingmember320 may have an inside diameter of about 0.4 inch to receive at least a portion of the shaft. However, the size of the inside diameter may vary according to the specific and varying needs of different implementations of theatomizer component302.

WhileFIG. 3 illustrates theatomizer component302 may be fixed to a shaft via a mountingmember320, theatomizer component302 may be fixed to a shaft via any other desired means. For example, theatomizer component302 may be fixed to a shaft via welding. In another example, theatomizer component302 and the shaft may be formed of a single piece (e.g., a single unit) of material (e.g., metal, plastic, composite, etc.).

When compared to a conventional atomizer component, because theatomizer component302 of the instant disclosure has a varyingheight310, theatomizer component302 has a perimeter length longer than a perimeter length of a conventional atomizer component that has a constant height along the perimeter thereof. For the purposes of the instant disclosure, “perimeter length” refers to the measurable length of the extension of thewall edge318 beginning and ending at a reference point on thewall306, from which the length is measured along theedge318 as it varies up and down in height. For example, theatomizer component302 having the varyingheight310 may have a perimeter length of about 11 inches, while a conventional atomizer component having a constant wall height and a plate with the same diameter as theatomizer component302, may have a perimeter length of about 9 inches. Because theatomizer component302 has a longer perimeter length than a perimeter length of a conventional atomizer component having a constant height along a perimeter of the atomizer component, the linear speed of theatomizer component302 is greater than the linear speed of the conventional atomizer component. For example, theatomizer component302 may have a linear speed of about 1060 inches per second, while the conventional atomizer component having the same diameter as theatomizer component302 and having a constant height, may have linear speed of about 900 inches per second when rotated at the same speed of about 6,000 revolutions per minute.

Further, when compared to a conventional atomizer component, because theatomizer component302 of the instant disclosure has a varyingheight310, theatomizer component302 distributes droplets of the atomized liquid fuel over a wider area. The wider area permits more air to be interspersed between the droplets, which accelerates evaporation. The accelerated evaporation then results in a higher efficiency of combustion than the conventional atomizer component. The droplet area may be a result of a depth of the varyingheight310. For example, the droplet area may be a result of a distance from peak to trough of the varyingheight310. Because the atomizer component has the varyingheight310, the varyingheight310 produces a wider droplet area (e.g., particle distribution) than atomizer components not having a varying height, but rather have holes or knife edges. For example, because the atomizer component has the varyingheight310, the varyingheight310 produces a wide droplet area of about 0.15 inches as compared to a thin band droplet area of about 0.01 inches produced by the atomizer components having holes or knife edges.

While this application describes theatomizer component302 being implemented in thecombustor system202 ofFIG. 2, theatomizer component302 described herein may be used in other environments and is applicable to other contexts. For example, theatomizer component302 may be implemented in a turbine engine, including with a turbine engine located on an airplane, a helicopter, a boat, a submarine, etc. Further, theatomizer component302 may be implemented in a sprayer, including with a paint sprayer, a snow cannon (e.g., snow gun), an airbrush, an insecticide sprayer, a pressure washer, etc.

Another Example Combustor Systems

FIG. 4 illustrates asection view400 of anotherexample combustor system402 that may be implemented in theengine heater system100 ofFIG. 1. Thecombustor system402 may be the same as thecombustor system118 discussed above. Inasmuch asFIG. 4 depicts thecombustor system402 implementable in theengine heater system100 ofFIG. 1, while referring to the same elements and features of thecombustor system402, the following discussion of specific features may refer interchangeably to any ofFIG. 1, 2, or3 except where explicitly indicated. In particular,FIG. 4 illustrates an embodiment of thecombustor system402, including the toroidal-shapedcombustion zone204, theairflow channel210, theatomizer component216, and thetube224.

FIG. 4 illustrates thecombustor system402 may include aguide vane404. Theguide vane404 may be disposed adjacent a leading side of the toroidal-shapedcombustion zone204 in a direction of air flow through theairflow channel210 so that theairflow channel210 guides a portion of theair122 from theairflow channel210 directly into the toroidal-shapedcombustion zone204. The portion of theair122 guided by theguide vane404 into the toroidal-shapedcombustion zone204 may provide for a reversed flame vortex406. For example, theguide vane404 may cause reversal of the direction of theflame vortex212 illustrated inFIG. 2. A reversed flame vortex406 may have a higher efficiency of combustion than theflame vortex212 illustrated inFIG. 2.

CONCLUSION

Although the subject matter has been described in language specific to structural features and/or methodological acts, it is to be understood that the subject matter defined in the appended claims is not necessarily limited to the specific features or acts described. Rather, the specific features and acts are disclosed as example forms of implementing the claims.

Claims

What is claimed is:

1. A combustor system comprising:

a toroidal-shaped combustion zone having an outside perimeter opposite a central hole;

an airflow channel interfacing with the outside perimeter of the toroidal-shaped combustion zone for delivering air to the toroidal-shaped combustion zone;

a shaft, at least a portion of the shaft extending into the central hole of the toroidal-shaped combustion zone; and

an atomizer component fixed to the portion of the shaft, the atomizer component for atomizing a liquid fuel into the toroidal-shaped combustion zone when the shaft is rotated.

2. The combustor system ofclaim 1, further comprising a tube having an end arranged proximate to the atomizer component for introducing the liquid fuel to the atomizer component.

3. The combustor system ofclaim 2, wherein the tube has an inside diameter of about 0.09 inch, and the liquid fuel is pressurized, inside of the tube, at about 30 pounds per square inch (psi) for introducing the liquid fuel to the atomizer component.

4. The combustor system ofclaim 1, wherein the atomizer component comprises:

a plate fixed to the portion of the shaft and extending transversely to a longitudinal axis of the shaft,

a wall extending from a perimeter of the plate, the wall having a height varying curvilinearly along the perimeter of the plate, and

wherein when the shaft is rotated and the liquid fuel is introduced to the plate of the atomizer component, the varying height of the wall causes the liquid fuel to atomize away from the atomizer component.

5. The combustor system ofclaim 1, further comprising a gas turbine communicatively coupled to the toroidal-shaped combustion zone.

6. The combustor system ofclaim 5, wherein the portion of the shaft extending into the central hole of the toroidal-shaped combustion zone is a first portion of the shaft, and

wherein a second portion of the shaft is attached to the gas turbine.

7. The combustor system ofclaim 5, further comprising a heat exchanger communicatively coupled to an exhaust of the gas turbine.

8. The combustor system ofclaim 1, wherein when the shaft is rotated, the shaft rotates at about 6000 revolutions per minute (rpm).

9. A combustor system comprising:

10. The combustor system ofclaim 9, further comprising a tube having an end arranged proximate to the atomizer component for introducing the liquid fuel to the atomizer component.

11. The combustor system ofclaim 10, wherein the tube has an inside diameter of about 0.09 inch, and the liquid fuel is pressurized, inside of the tube, at about 30 pounds per square inch (psi) for introducing the liquid fuel to the atomizer component.

12. The combustor system ofclaim 9, wherein the atomizer component comprises:

13. The combustor system ofclaim 9, further comprising a gas turbine communicatively coupled to the toroidal-shaped combustion zone.

14. The combustor system ofclaim 13, wherein the portion of the shaft extending into the central hole of the toroidal-shaped combustion zone is a first portion of the shaft, and

wherein a second portion of the shaft is attached to the gas turbine.

15. The combustor system ofclaim 9, wherein when the shaft is rotated, the shaft rotates at about 6000 revolutions per minute (rpm).

16. A combustor system comprising:

an airflow channel interfacing with the outside perimeter of the toroidal-shaped combustion zone for delivering air to the toroidal-shaped combustion zone; and

an atomizer component arranged with the toroidal-shaped combustion zone, the atomizer component for atomizing a liquid fuel into the toroidal-shaped combustion zone.

17. The combustor system ofclaim 16, further comprising a tube having an end arranged proximate to the atomizer component for introducing the liquid fuel to the atomizer component.

18. The combustor system ofclaim 17, wherein the tube has an inside diameter of about 0.09 inch, and the liquid fuel is pressurized, inside of the tube, at about 30 pounds per square inch (psi) for intruding the liquid fuel to the atomizer component.

19. The combustor system ofclaim 16, wherein the atomizer component comprises:

a plate and a wall extending from a perimeter of the plate, the wall having a height varying curvilinearly along the perimeter of the plate, and

wherein when the atomizer component is rotated and the liquid fuel is introduced to the plate of the atomizer component, the varying height of the wall causes the liquid fuel to atomize into the toroidal-shaped combustion zone.

20. The combustor system ofclaim 19, wherein the varying height of the wall causes the atomized liquid fuel to have a wide droplet area having a width of about 0.15 inches.

21. The combustor system ofclaim 16, wherein the atomizer component is fixable to at least a portion of the shaft, and

wherein when the shaft is rotated and the liquid fuel is introduced to the atomizer component, the liquid fuel is atomized into the toroidal-shaped combustion zone.