Patent Application
20180340494
The embodiments herein generally relate to actuators, and more particularly to thermo-acoustic actuators.
Ultrasonic waves may be used to provide flame enhancement in a combustor (also referred to as a burner, combustion chamber, or flame holder) of an engine. Flame enhancement in the combustor is desirable because it results in higher produced power and higher efficiency of the engine.
Conventionally, piezoelectric transducers may be used to provide ultrasonic waves. Piezoelectric transducers are typically constructed of doped, solid-state quartz. However, their electromechanical properties generally change with temperature, making their operation and control difficult without an additional temperature monitoring and control system.
Piezoelectric transducers also typically need to be actively cooled. However, a cooling process creates local cold spots in or around the combustor, and may quench combustion and potentially requires more energy than the ultrasonic waves would add to the process. Furthermore, the delivered frequencies of solid-state quartz can change with temperature, and high temperature typically negatively impacts their durability. Moreover, conventional piezoelectric transducers often produce ultrasound at less than only five frequencies, and usually not even concurrently.
Further, temperature gradients within solid-state quartz can cause stress and fracture during operation in an engine. Also, piezoelectric transducers tend to require external, electric stimulation. The associated structural and electronic support architecture, such as a fixture to hold the actuator, connection wires, and driving circuitry can add complexity and critical weight to an engine, which is not desirable.
Accordingly, piezoelectric transducers may not be practical for installation into the high temperature environments found in combustors. An alternative method is to use small speakers to generate ultrasonic waves. However, the small speakers that produce ultrasound are conventionally constructed of thin, flexible plastic membranes and copper wire, which could either burn or melt in a high temperature engine combustor.
In view of the foregoing, an embodiment herein provides a combustor comprising a first perforated layer comprising a first opening having a first diameter, wherein the first opening is configured to receive a flow of fluid comprising a fuel and air mixture; and impart a first rotational instability to the flow of fluid that is dependent on the first diameter; and a second perforated layer surrounding a combustion area, wherein the second perforated later comprises a second opening having a second diameter, and wherein the second layer is located between the first layer and the combustion area.
The second opening may be configured to impart a second rotational instability to the flow that is dependent on the second diameter of the second opening; an offset distance between a first axis of the first opening and a second axis of the second opening; and a distance between the first and second perforated layers.
The second opening may be configured to generate an acoustic signal based on the first and second rotational instabilities on the flow of fluid. The second opening may be configured to generate a flame using the flow of fluid in the combustion area. The second opening may be configured to increase a speed of the flame in the combustion area using the acoustic signal. The combustor may further comprise a filter configured to filter a plurality of harmonics from the acoustic signal, wherein the filter may be operationally coupled to any of the first and second perforated layers.
An embodiment herein provides a method for increasing an efficiency of an engine, the method comprising receiving a flow of fluid comprising a fuel and air mixture through a first opening in a first perforated layer of a combustor of the engine; creating a first rotational instability to the flow of fluid, wherein the first rotational instability is dependent on a first diameter of the first opening; and positioning a second perforated layer between the first layer and a combustion area of the combustor, wherein the second layer comprises a second opening.
The method may further comprise creating, using the second opening, a second rotational instability to the flow of fluid that is dependent on a second diameter of the second opening; an offset distance between a first axis of the first opening and a second axis of the second opening; and a distance between the first and second perforated layers.
The method may further comprise generating, using the second opening, an acoustic signal based on the first and second rotational instabilities on the flow of fluid. The method may further comprise generating a flame using the second opening and the flow of fluid in the combustion area. The method may further comprise increasing a speed of the flame in the combustion area using the acoustic signal. The method may further comprise filtering a plurality of harmonics from the acoustic signal.
An embodiment herein provides for a combustor comprising a plurality of perforated surrounding layers, comprising a first perforated surrounding layer comprising a first opening, wherein the first opening is configured to receive a flow of fuel and air mixture; and impart a first rotational instability to the flow, wherein the first rotational instability is dependent on a first diameter of the first opening; and a second perforated surrounding layer comprising a second opening, wherein the second layer is located between the first layer and a combustion area; and a plurality of intermediate perforated surrounding layers, located between the first and second layers, wherein each of the intermediate layers comprise a corresponding intermediate plurality of openings configured to pass the flow and impart a plurality of intermediate rotational instabilities to the flow.
The second opening may be configured to impart a second rotational instability to the flow, wherein the second rotational instability is dependent on a first offset distance between a first axis of the first opening and an intermediate axis of an intermediate opening of an intermediate layer of the plurality of intermediate layers; a second offset distance between the intermediate axis and a second axis of the second opening; a second diameter of the second opening; an intermediate diameter of the intermediate opening; a first distance between the first and the intermediate layer; and a second distance between the intermediate layer and the second layer.
The second opening may be configured to generate an acoustic signal based on the first, second, and the plurality of intermediate rotational instabilities on the flow. The second opening may be configured to generate a flame using the flow in the combustion area.
The second opening may be configured to increase a speed of the flame in the combustion area using the acoustic signal. The combustor may further comprise a filter configured to filter out a plurality of harmonics of the acoustic signal.
These and other aspects of the embodiments herein will be better appreciated and understood when considered in conjunction with the following description and the accompanying drawings. It should be understood, however, that the following descriptions, while indicating preferred embodiments and numerous specific details thereof, are given by way of illustration and not of limitation. Many changes and modifications may be made within the scope of the embodiments herein without departing from the spirit thereof, and the embodiments herein include all such modifications.
The embodiments herein will be better understood from the following detailed description with reference to the drawings, in which:
The embodiments herein and the various features and advantageous details thereof are explained more fully with reference to the non-limiting embodiments that are illustrated in the accompanying drawings and detailed in the following description. Descriptions of well-known components and processing techniques are omitted so as to not unnecessarily obscure the embodiments herein. The examples used herein are intended merely to facilitate an understanding of ways in which the embodiments herein may be practiced and to further enable those of skill in the art to practice the embodiments herein. Accordingly, the examples should not be construed as limiting the scope of the embodiments herein.
The embodiments herein provide a multi-mode thermo-acoustic actuator that passively uses the air flow and fuel vapor which is already present in a combustor, to produce range discrete acoustic waves that enhance the combustion. An embodiment herein provides for producing an acoustic tone composed of discrete acoustic harmonics, with frequencies above the ultrasonic limit of 22 kHz.
Referring now to the drawings, and more particularly to
In an embodiment herein, a flow of fuel and air mixture 110 enters the combustion area 108 through the perforated layers 102, 104, and 106. In an embodiment herein, openings (illustrated in
As the fuel and air mixture 110 passes through the perforated layers 201 and 203, each of the openings 202 and 204 imparts rotational instability to the flow that contribute to creating the acoustic waves 212. The embodiments herein further provide for tuning the acoustic waves 212 by changing its frequency components. The frequency components of the acoustic waves 212 are determined by any of a diameter 205 of the openings 202, a diameter 206 of the openings 204, the offset distance 208 between the opening axes 207 and 209, and the spacing 210 between the layers 201 and 203.
When the fuel-air mixture 110 exits the layer 203 and combusts, the waves 212 cause the flames 214 to oscillate, which in turn produce pressure oscillations, or sound, at the corresponding frequencies. In an embodiment herein, the combustion of the fuel-air mixture 110 includes a chemical combination of the fuel and the oxygen components in the fuel-air mixture 110. The chemical combination may include production of heat and light and cause combustion of the fuel-air mixture 110. The acoustic waves 212 improve combustion by further increasing flame speed which increases combustion stability and increases combustor heat release. Consequently, the combustor 101 can be built smaller and lighter without sacrificing generated power. The acoustic waves 212 may further break down diffusion gradients at the interfaces between gases and surface to increase heat transfer, and also combustion exhaust mass transfer. Hence, the embodiments herein provide for increased efficiency of the combustor 101.
The acoustic waves 212 may further be tuned to provide noise cancelling interaction with other acoustic waves generated by the combustor 101, which may cause instability for combustion, or environmental sound, or air pollution. In an embodiment herein, the tuning of the acoustic waves 212 may be performed by changing its frequency components. As described above, the frequency components of the acoustic waves 212 may be determined by any of the diameter 205 of the openings 202, the diameter 206 of the openings 204, the offset distance 208 between the opening axes 207 and 209, and the spacing 210 between the layers 201 and 203. In an embodiment herein, the discrete frequencies in the acoustic waves 212 may be filtered, by a filter 112, to provide a single tone acoustic signal, or multiple specific discrete acoustic signals.
In an embodiment herein, in order to produce the desired acoustic tone and constituent frequencies of the acoustic waves 212, the fuel and air mixture 110 may be directed through any number of perforated layers similar to the prorated layers 201 and 203. The perforated layers 201 and 203 may have any number of openings 202 and 204, and the openings 202 and 204 may have any shape including any of circular, oval, rectangular, triangular, and polygon.
In an embodiment herein, the method 400 may include imparting, using the second opening 204, a second rotational instability to the flow of fluid 110 that is dependent on a second diameter 206 of the second opening 204, an offset distance 208 between a first axis 207 of the first opening 202 and a second axis 209 of the second opening 204, and a distance 210 between the first and second perforated layers 201 and 203. The method 400 may include generating, using the second opening 204, an acoustic signal based on the first and second rotational instabilities on the flow of fluid 110.
In some embodiments, additional perforated layers with openings can similarly be used by method 400 to impart further rotational instability on the flow of fluid 110. In this case, the acoustic signal can also be generated by method 400 based on the further rotational instability of the additional perforated layers.
In an embodiment herein, the method 400 may include generating a flame using the second opening 204 and the flow of fluid 110 in the combustion area 108. The method 400 may include increasing a speed of the flame in the combustion area 108 using the acoustic signal. The method 400 may include filtering a plurality of harmonics from the acoustic signal.
The techniques provided by the embodiments herein use the passive nature of a multi-mode thermos-acoustic actuator that allow for the formation of acoustic tones using high temperature flows, without the need of actuation by delicate ultrasonic transducers or speakers that need electronic circuitry to drive their operation. This will allow for the formation of flame enhancing sound without complex components and circuitry in a high temperature environment.
The foregoing description of the specific embodiments will so fully reveal the general nature of the embodiments herein that others can, by applying current knowledge, readily modify and/or adapt for various applications such specific embodiments without departing from the generic concept, and, therefore, such adaptations and modifications should and are intended to be comprehended within the meaning and range of equivalents of the disclosed embodiments. It is to be understood that the phraseology or terminology employed herein is for the purpose of description and not of limitation. Therefore, while the embodiments herein have been described in terms of preferred embodiments, those skilled in the art will recognize that the embodiments herein can be practiced with modification within the spirit and scope of the appended claims.
The embodiments herein were made by employees of the United States Government and may be manufactured, used, and/or licensed by or for the United States Government without the payment of royalties thereon.
