Patent Application
20240410296
Various embodiments of the present invention pertain to apparatus and methods for cleaning devices that include the gas path including a combustion chamber, and in particular to apparatus and methods for cleaning of a gas turbine engine.
Turbine engines extract energy to supply power across a wide range of platforms. Energy can range from steam to fuel combustion. Extracted power is then utilized for electricity, propulsion, or general power. Turbines work by turning the flow of fluids and gases into usable energy to power helicopters, airplanes, tanks, power plants, ships, specialty vehicles, cities, etc. Upon use, the gas-path of such devices becomes fouled with debris and contaminants such as minerals, sand, dust, soot, carbon, etc. When fouled, the performance of the equipment deteriorates, requiring maintenance and cleaning.
It is well known that turbines come in many forms such as jet engines, industrial turbines, or ground-based and ship-based aero-derived units. The internal surfaces of the equipment, such as that of an airplane or helicopter engine, accumulate fouling material, deteriorating airflow across the engine, and diminishing performance. Correlated to this trend, fuel consumption increases, engine life shortens, and power available decreases. The simplest means and most cost effective means to maintain engine health and restore performance is to properly clean an engine. There are many methods available, such as mist, sprays, and vapor systems. However, all fail to reach deep or across the entire engine gas-path.
Telemetry or diagnostic tools on engine have become routine functions to monitor engine health. Yet, using such tools to monitor, trigger, or quantify improvement from foam engine cleaning have not been utilized in the past.
Various embodiments of the present invention provide novel and unobvious methods and apparatus for the cleaning of such power plants.
Foam material is introduced at the gas-path entry of turbine equipment while off-line. The foam will coat and contact the internal surfaces, scrubbing, removing, and carrying fouling material away from equipment.
One aspect of the present invention pertains to an apparatus for foaming a cleaning agent. Some embodiments include a housing defining an internal flowpath having first, second, and third flow portions, a gas inlet, a liquid inlet for the cleaning agent, and a foam outlet. The first flow portion includes a gas plenum that is adapted and configured for receiving gas under pressure from the gas inlet and including a plurality of apertures, the plenum and the interior of the housing forming a mixing region that provides a first foam of the liquid and the gas. The second flow portion receives the first foam and flows the first foam past a foam growth matrix adapted and configured to provide surface area for attachment and merging of the cells. The third flow portion flows the second foam through a foam structuring member downstream of either the first portion or the second portion adapted and configured to reduce the size of at least some of the cells. It is understood that yet other embodiments of the present invention contemplate a housing having only a first portion; or a first and second portion; or only a first and third portion in various other nucleation devices.
Another aspect of the present invention pertains to a method for foaming a liquid cleaning agent. Some embodiments include mixing the liquid cleaning agent and a pressurized gas to form a first foam. Other embodiments include flowing the first foam over a member or matrix and increasing the size of the cells of the first foam to form a second foam. Yet other embodiments include flowing the second foam through a structure such as a mesh or one or more apertured plates and decreasing the size of the cells of the second foam to form a third foam.
Yet another aspect of the present invention pertains to a system for providing an air-foamed liquid cleaning agent. Other embodiments include an air pump or pressurized gas reservoir providing air or gas at pressure higher than ambient pressure, and a liquid pump providing the liquid at pressure. Still other embodiments include a nucleation device receiving pressurized air, a liquid inlet receiving pressurized liquid, and a foam outlet, the nucleation device turbulently mixing the pressurized air and the liquid to create a foam. Yet other embodiments include a nozzle receiving the foam through a foam conduit, the internal passageways of the nozzle and the conduit being adapted and configured to not increase the turbulence of the foam, the nozzle being adapted and configured to deliver a low velocity stream of foam.
Still another aspect pertains to a method for providing an air-foamed liquid cleaning agent to the inlet of a jet engine installed on an airplane. Some embodiments include providing a source of a pressurized liquid cleaning agent, an air pump, a turbulent mixing chamber, and a non-atomizing supply aperture. Other embodiments include mixing pressurized air with pressurized liquid in the mixing chamber and creating a supply of foam. Still other embodiments include streaming the supply of foam into the installed engine either through the inlet or through various tubing attached to the engine from the aperture.
Yet another aspect of the present invention pertains to an apparatus for foaming a water soluble liquid cleaning agent. Some embodiments include means for mixing a pressurized gas with a flowing water soluble liquid to create a foam. Other embodiments include means for growing the size of the cells of the foam and means for reducing the size of the grown cells.
In various embodiments of the invention, the effluent after a cleaning operation is collected and evaluated. This evaluation can include an on-site analysis of the content of the effluent, including whether or not particular metals or compounds are present in the effluent. Based on the results of this evaluation, a decision is made as to whether or not further cleaning is appropriate.
Still further embodiments of the present invention pertain to a method in which the effect of a cleaning operation is assessed, and that assessment is used to evaluate the terms of a contract. As one example, the contract may pertain to the terms of the engine warranty provided by the engine manufacturer to the operator or owner of the aircraft. In still further embodiments the assessment may be used to evaluate the terms of a contract pertaining to the engine cleaning operation itself. In yet further embodiments the assessment of the cleaning effect on the engine may be used to evaluate the engine relative to establish FAA maintenance standards for that engine.
In one embodiment, the assessment method includes operating an engine in a commercial flight environment for more than about one month. It is anticipated that in some embodiments this operation can include multiple flights per day, and usage of the aircraft for up to seven days per week. The method further includes operating the used engine and establishing a baseline characteristic. In some embodiments, the baseline characteristic can be specific fuel consumption at a particular level of thrust, exhaust pressure ratio, or rotor speed. In some alternatives, the method includes correcting this baseline data for ambient atmospheric characteristics. In yet other embodiments, the baseline parameter could be the elapsed time for the start of an engine from zero rpm up to idle speed. In still further embodiments, the baseline assessment of the used engine includes the assessment of engine start time in the following manner: performing a first start of an engine; shutting down the engine; motoring the engine on the starter (without the combustion of fuel) for a predetermined period of time; and after the motoring, performing a second engine start, and using the second engine start time as the baseline start time.
The method further includes cleaning the engine. This cleaning of the engine may include one or more successive cleaning cycles. After the engine is cleaned, the baseline test method is repeated. This second test results (of the cleaned engine) are compared to the baseline test results (of the used engine, as received); and the changes in engine characteristics are assessed against a contractual guarantee. As one example, the operator of the cleaning equipment may have offered contractual terms to the owner or operator of the aircraft with regards to the improvement to be made by the cleaning method. In still further embodiments, the delta improvement provided by the cleaning method (or alternatively, the test results of the cleaned engine considered by itself) can be compared to a contractual guarantee between the manufacturer of the engine (or the facility that performed the previous overhaul of the engine, or the licensee of the engine) to assess whether or not the cleaned engine meets those contractual terms.
In still further embodiments, there is a cleaning method in which a baseline test is performed on a used engine; the engine is cleaned; and the baseline test is performed a second time. The comparison of the baseline test to the clean engine test can be used for any reason.
In yet other embodiments, the cleaning method includes a procedure in which the engine is operated in a cleaning cycle, and that cleaning cycle (or a different cleaning cycle), is subsequently applied to the engine. Preferably, the cleaning chemicals are provided to the engine at relatively low rotational speeds, and preferably less than about one-half the typical idle speed for that engine.
In still further embodiments, such as in those engines supported substantially vertically, the cleaning chemical can be applied to the engine when the engine is static (i.e., zero rpm). After applying a sufficient amount of chemicals, the engine can then be rotated at any speed, and the cleaning chemicals subsequently flushed.
Yet other embodiments of the present invention pertain to methods for cleaning an engine that include manipulation of the temperature of the cleaning chemicals and/or manipulation of the temperature of the engine that is being cleaned. In one embodiment, the cleaning system includes a heater that is adapted and configured to heat the cleaning chemicals prior to the creation of a cleaning foam. In still further embodiments, the method includes a heater for heating the air being used to create the foam with the cleaning liquids. In still further embodiments, the cleaning apparatus includes one or more air blowers that provide a source of heated ambient air (similar to “alligator” space heaters used at construction sites). These hot air blowers can be positioned at the inlet of the engine, and the engine can be motored (i.e., rotated on the starter, without combustion of fuel) for either a predetermined period of time (which may be based on ambient conditions), or motored until thermocouples or other temperature measurement devices in the engine hot section have reached a predetermined temperature. In still further embodiments, the temperature of the engine prior to the introduction of the cleaning foam can be raised by starting the engine and operating the engine at idle conditions for a predetermined period of time, and subsequently shut down the engine prior to introduction of the cleaning foam. In still further embodiments, the engine can be motored after the shutdown from idle and before the introduction of chemicals to further achieve a consistent baseline temperature condition prior to introduction of the foam. Still further embodiments of the present invention contemplate any combination of preheated liquid chemicals, preheated compressed air used for foaming, externally heated engines, and engines made “warm” by one or more recent periods of operation.
In still further embodiments of the present invention, the cleaning foam can be heated by providing a heating element within the device used to mix and create the cleaning foam.
It will be appreciated that the various apparatus and methods described in this summary section, as well as elsewhere in this application, can be expressed as a large number of different combinations and subcombinations. All such useful, novel, and inventive combinations and subcombinations are contemplated herein, it being recognized that the explicit expression of each of these combinations is unnecessary.
Some of the figures shown herein may include dimensions. Further, some of the figures shown herein may have been created from scaled drawings or from photographs that are scalable. It is understood that such dimensions, or the relative scaling within a figure, are by way of example, and not to be construed as limiting.
The following is a list of element numbers and at least one noun used to describe that element. It is understood that none of the embodiments disclosed herein are limited to these nouns, and these element numbers can further include other words that would be understood by a person of ordinary skill reading and reviewing this disclosure in its entirety.
For the purposes of promoting an understanding of the principles of the invention, reference will now be made to the embodiments illustrated in the drawings and specific language will be used to describe the same. It will nevertheless be understood that no limitation of the scope of the invention is thereby intended, such alterations and further modifications in the illustrated device, and such further applications of the principles of the invention as illustrated therein being contemplated as would normally occur to one skilled in the art to which the invention relates. At least one embodiment of the present invention will be described and shown, and this application may show and/or describe other embodiments of the present invention.
It is understood that any reference to “the invention” is a reference to an embodiment of a family of inventions, with no single embodiment including an apparatus, process, or composition that should be included in all embodiments, unless otherwise explicitly stated. Further, although there may be discussion with regards to “advantages” provided by some embodiments of the present invention, it is understood that yet other embodiments may not include those same advantages, or may include yet different advantages. Any advantages described herein are not to be construed as limiting to any of the claims. The usage of words indicating preference, such as “preferably,” refers to features and aspects that are present in at least one embodiment, but which are optional for some embodiments.
The use of an N-series prefix for an element number (NXX.XX) refers to an element that is the same as the non-prefixed element (XX.XX), except as shown and described. As an example, an element 1020.1 would be the same as element 20.1, except for those different features of element 1020.1 shown and described. Further, common elements and common features of related elements may be drawn in the same manner in different figures, and/or use the same symbology in different figures. As such, it is not necessary to describe the features of 1020.1 and 20.1 that are the same, since these common features are apparent to a person of ordinary skill in the related field of technology. Further, it is understood that the features 1020.1 and 20.1 may be backward compatible, such that a feature (NXX.XX) may include features compatible with other various embodiments (MXX.XX), as would be understood by those of ordinary skill in the art. This description convention also applies to the use of prime (′), double prime (″), and triple prime (′″) suffixed element numbers. Therefore, it is not necessary to describe the features of 20.1, 20.1′, 20.1″, and 20.1′″ that are the same, since these common features are apparent to persons of ordinary skill in the related field of technology.
Although various specific quantities (spatial dimensions, temperatures, pressures, times, force, resistance, current, voltage, concentrations, wavelengths, frequencies, heat transfer coefficients, dimensionless parameters, etc.) may be stated herein, such specific quantities are presented as examples only, and further, unless otherwise explicitly noted, are approximate values, and should be considered as if the word “about” prefaced each quantity. Further, with discussion pertaining to a specific composition of matter, that description is by example only, and does not limit the applicability of other species of that composition, nor does it limit the applicability of other compositions unrelated to the cited composition.
What follows are paragraphs that express particular embodiments of the present invention. In those paragraphs that follow, some element numbers are prefixed with an “X” indicating that the words pertain to any of the similar features shown in the drawings or described in the text.
What will be shown and described herein, along with various embodiments of the present invention, is discussion of one or more tests that were performed. It is understood that such examples are by way of example only, and are not to be construed as being limitations on any embodiment of the present invention. Further, it is understood that embodiments of the present invention are not necessarily limited to or described by the mathematical analysis presented herein.
Various references may be made to one or more processes, algorithms, operational methods, or logic, accompanied by a diagram showing such organized in a particular sequence. It is understood that the order of such a sequence is by example only, and is not intended to be limiting on any embodiment of the invention.
Various references may be made to one or more methods of manufacturing. It is understood that these are by way of example only, and various embodiments of the invention can be fabricated in a wide variety of ways, such as by casting, centering, welding, electrodischarge machining, milling, as examples. Further, various other embodiment may be fabricated by any of the various additive manufacturing methods, some of which are referred to 3-D printing.
This document may use different words to describe the same element number, or to refer to an element number in a specific family of features (NXX.XX). It is understood that such multiple usage is not intended to provide a redefinition of any language herein. It is understood that such words demonstrate that the particular feature can be considered in various linguistical ways, such ways not necessarily being additive or exclusive.
What will be shown and described herein are one or more functional relationships among variables. Specific nomenclature for the variables may be provided, although some relationships may include variables that will be recognized by persons of ordinary skill in the art for their meaning. For example, “t” could be representative of temperature or time, as would be readily apparent by their usage. However, it is further recognized that such functional relationships can be expressed in a variety of equivalents using standard techniques of mathematical analysis (for instance, the relationship F=ma is equivalent to the relationship F/a=m). Further, in those embodiments in which functional relationships are implemented in an algorithm or computer software, it is understood that an algorithm-implemented variable can correspond to a variable shown herein, with this correspondence including a scaling factor, control system gain, noise filter, or the like.
A wide variety of methods have been used to clean gas turbine engines. Some users utilize water sprayed into the inlet of the engine, others utilize a cleaning fluid sprayed into the inlet of the engine, and still further users provide solid, abrading material to the inlet of the engine, such as walnut shells.
These methods achieve varying degrees of success, and further create varying degrees of problems. For example, some cleaning agents that are strong enough to clean the hot section of the engine and are chemically acceptable on hot section materials, are chemically unacceptable on material used in the cold section of the engine. Water washes are mild enough to be used on any materials in the engine, but are also not particularly effective in removing difficult deposits, and still further can leave deposits of silica in some stages of the compressor. A number of water-soluble cleaning agents are recognized in MIL-PRF-85704C, but many users of these cleaning agents consider them to be marginally successful in restoring performance to an engine operating parameter, and still other users have noted that simple washes with these MIL cleaning agents can actually degrade some operational parameters.
Therefore, many operators of aircraft are suspicious of the claims made with regards to some liquid cleaning methods, as to how effective liquids will be in restoring performance to the engine. There are expenses incurred by liquid washing of an engine, including the cost of the liquid wash and the value of the time that the air vehicle is removed from operation. Often, the benefits of the liquid wash do not outweigh the incurred costs, or provide only negligible commercial benefit.
Various embodiments of the present invention indicate a substantial commercial benefit to be gained by washing of gas turbine engines with a foam. As will be shown herein, the foam cleaning of an engine can provide substantial improvements in operating parameters, including improvements not obtainable with liquid washing. The reason for the substantial improvement realized by foam washing is not fully understood. Back-to-back engine tests have been performed on the same specific engine, with the introduction of atomized liquid into the inlet, followed by the introduction of a foam of that same liquid into the inlet. In all cases, the liquid (or the foam) was observed in the engine exhaust section, indicating that the liquid (or the foam) appears to be wetting the entire gaspath. Nonetheless, the use of a foamed version of a liquid provides significant improvements over and above any liquid washing improvements in important operational parameters, such as engine start times, specific fuel consumption, and turbine temperatures required to achieve a particular power output.
Some embodiments of the present invention pertain to a system for generating a foam from a water-soluble cleaning agent. It has been found that there are differences in the apparatus and methods of creating an acceptable foam with a water-soluble chemical, or a non-water-soluble chemical. Various embodiments of the present invention pertain to systems including nucleation chambers provided with pressurized liquid and also pressurized air.
It has been found that injecting this foam into an engine inlet by way of conditional atomizing nozzles can reduce the cleaning effectiveness of the foam. Still further, any plumbing, tubing, or hoses that deliver foam from the nucleation chamber to the nozzle should be generally smooth, and substantially free of turbulence-generating features in the flowpath (such as sharp turns, sudden reductions in flow area of the foam flowpath, or delivery nozzles having sections with excessive convergence, such as convergence to increase the velocity of the foam).
It is helpful in various embodiments of the present invention to provide a flowpath for the generated foam that maintains the higher energy state of the foam, and not dissipate that energy prior to delivery.
Various embodiments of the present invention also are assisted by the introduction of gas (including air, nitrogen, carbon dioxide, or any other gas) in a pressurized state into a flow of the cleaning liquid. Preferably, air is pressurized to more than about 5 psig and less than about 120 psig, and supplied by a pump or pressurized reservoir. Although some embodiments of the present invention do include the use of airflow eductors that can entrain ambient air, yet other embodiments using pressurized air had been found to provide improved results.
Yet other embodiments of the present invention pertain to the commercial use of foam cleaning with aviation engines. As discussed earlier, the mechanism by which a foamed cleaning agent provides results superior to a non-foamed cleaning agent are not currently well understood. To the converse, many experts in the field of jet engine maintenance initially believe that a foamed cleaning agent will provide the same disappointing results as would be provided by a non-foamed cleaning agent. Therefore, as the use of a foam cleaning agent becomes better understood, the effect of the improved foam cleaning on the financial considerations in supporting a family of engines will become better understood. Some of these improvements may be readily apparent, such as the improvements in operating temperature, specific fuel consumption, and start times indicated by the testing documented herein. Yet other impacts from the use of foam cleaning agents may further impact the design of other, life-limited components in the engine.
For example, engines are currently designed with life-limited parts (such as those based on hours of usage, time at temperature, number of engine cycles, or others), and inspections of those components may be scheduled at times coincident with liquid washing of the engine. However, the use of foam washing may generally increase the time that an engine can be installed on the aircraft, since the foam washing will restore the used engine to a better performance level than liquid washing would. However, an increase in time between foam washings (increased as compared to the interval between liquid washings) could be lengthened to the extent that a foam washing no longer coincides with an inspection of a life-limited part. Under these conditions, it may be financially rewarding to design the life-limited part to a slightly longer cycle. The increase in the cost of the longer-lived life-limited component may be more than offset by the increased time that the foam cleaned engine can remain on the wing.
In such embodiments, there can be a shift in the paradigm of the engine washing, inspection, and maintenance intervals, resulting at least in part by the improved cleaning resulting from foam washing. In some embodiments, the effect of foam washing on an engine performance parameter (such as start time, temperature at max rated power, specific fuel consumption, carbon emission, oxides of nitrogen emission, typical operating speeds of the engine at cruise and take-off, etc.) can be quantified. That quantification can occur within a family of engines, but in some instances may be applicable between different families. As a specific engine within that family is operated on an aircraft, the operator of the aircraft will note some change in an operating parameter that can be correlated with an improvement to be gained by a foam washing of that specific engine. That information taken by the aircraft operator is passed on to the engine owner (which could be the U.S. government, an engine manufacturer, or an engine leasing company), and that owner determines when to schedule a foam cleaning of that specific engine.
It has been found experimentally that various embodiments of the foam washing methods and apparatus described herein are more effective in removing contaminants from a used engine than by way of spray cleaning of a liquid cleaning agent. In some cases, the effluent collected in the turbine after the foam cleaning has been compared to the effluent collected in the turbine after a liquid wash, with the liquid wash having preceded the foam wash. In these cases, the foam effluent was found to have contained in it substantial amounts of dirt and deposits that were not removed by the liquid wash.
It is believed that in some families of engines the use of a foam wash will provide an improvement in the cleanliness of the combustor liner. It is well known that combustor liners include complex arrangements of cooling holes, these cooling holes being designed to not just maintain a safe temperature for the liner itself, but further to reduce gas path temperatures and thereby limit the formation of oxides of nitrogen. It is anticipated that various embodiments of the present invention will demonstrate reductions in the emission of a cleaned engine of the oxides of nitrogen.
The introduction of gas through the apertures X70 are adapted and configured to create a foam with the cleaning liquid within a nucleation zone X65. Preferably, the foam is created by nucleation of pre-certified aviation chemicals with proper arrangement of high speed air jets, diffuser sections, growth spikes, and/or centrifugal sheering of the chemicals, any of which can be used to create the foam which is a higher energy, short-lived state of the more stable non-foamed liquid chemical. The resultant foam is provided to outlet X64 for introduction into the inlet of the device being cleaned.
In some embodiments, chamber X60 further includes a cell growth section X74 in which there is material or an apparatus that encourages merging of smaller foam cells into a larger foam cell. In still other embodiments, nucleation chamber X60 can include a cell structuring section X78 that includes material or apparatus for improving the homogeneity of the foam material. Still further embodiments of chamber X60 include a laminar flow section X82 in which the foamed material 28 is made less turbulent so as to increase the longevity of the foam cells and thus increase the number of foam cells delivered to the inlet 11 of the product 10 being cleaned.
Some of the nucleation chambers X60 include nucleation zones, growth sections, and structuring sections that are arranged serially within the foam flowpath. In yet other embodiments these zones and sections are arranged concentrically, with the foam first being created proximate to the centerline of the flowpath. In yet other embodiments the zones and sections are arranged concentrically with the foam being created at the periphery of the flowpath, with the cells being grown and structured progressively toward the center of the flowpath.
Some of the nucleation chambers X60 described herein include nucleation zones, growth sections, and structuring sections that are arranged within a single plenum. However, it is understood that yet other embodiments contemplate a modular arrangement to the nucleation chamber. For example, the nucleation zone can be a separate component that is bolted to a structuring zone, or a to laminar flow zone. For example, the various sections can be attached to one another by flanges and fasteners, threaded fittings, or the like. Still further, the systems X20 are described herein to include a single nucleation chamber. However, it understood that the cleaning system can include multiple nucleation chambers. As one example, a plurality of chambers can be fed from manifolds that provide the liquids and gas. This parallel flow arrangement can provide a foam output that likewise is manifolded together to a single nozzle X28, or to a plurality of nozzles arranged in a pattern to best match the engine inlet geometry.
The various washing systems X20 discussed herein can include a mixture of liquids (such as water, chemical A, and chemical B) that are provided to the inlet of the nucleation chamber, within which gas is injected so as to create a foam from the mixture of liquids. However, the present invention is not so limited, and further includes those embodiments in which the liquids may be foamed separately. For example, a cleaning system according to another embodiment of the present invention may include a first nucleation chamber for chemical A, and a second nucleation chamber for a mixture of chemical B and water. The two resultant foams can then be provided to a single nozzle X28, or can be provided to separate nozzles X28.
The various descriptions that follow pertain to a variety of embodiments of nucleation chambers X60 incorporating numerous differences and numerous similarities. It is understood that each of these is presented by way of example only, and are not intended to place boundaries on the broad ideas expressed herein. As yet another example, the present invention contemplates an embodiment in which the liquid product is provided to an inlet X63 and flows within a flowpath surrounded by a circumferential gas chamber X66. In such embodiments, gas chamber X66 defines an annular flow space and provides gas under pressure from an inlet X62 into the liquid product flowing within the annulus.
Gas tube 66 is located generally concentrically within housing 61 (although a concentric location is not required), such that liquid from inlet 63 flows generally around the outer surface of tube 66. Tube 66 preferably includes a plurality of apertures 70 that are adapted and configured to flow gas from within tube 66 generally into the interior foam-creating passageway of housing 61. As shown in
As one example, the nucleation jets 70 are adapted and configured to have a total flow area that is about equal to the cross sectional flow area of housing 61 or less than that cross sectional area. As one example, the jets 70 have hole diameters from about one-eighth of an inch to about one-sixteenth of an inch.
The foam within nucleation chamber 60 is first created within a nucleation zone 65 that includes the initial mixing of gas and liquid streams as previously discussed. As the foam leaves this zone, it flows into a downstream growth section 74 and passes over a corresponding growth material 75. Material 75 is adapted and configured to provide structural surface area on which individual foam cells can attach and combine with other foam cells to divide into more foam cells. Material 75 includes a plurality of features that cause larger, more energized cells to divide into a number of smaller cells. In some embodiments, material 75 is a mesh preferably formed from a metallic material. Plastic materials can also be substituted, provided that the organic material can withstand exposure to the liquids 22 used for cleaning. It is further contemplated by yet other embodiments that material 75 can be materials other than a mesh.
As the more divided foam cells exit growth section 74, they enter a cell structuring section 78 that preferably includes a material 79 within the internal foam passage of housing 61. The material 79 of cell-structuring section 78 is adapted and configured to receive a first, various distribution of foam cell sizes from section 74, and provide to output 64 a second, smaller, and tighter distribution of cell sizes. In some embodiments, the structuring material 79 includes a mesh formed from a metal, with the cell size of the mesh of section 78 being smaller than the mesh size of growth section 74.
After the merged (more abundant cells) and structured (improved homogeneity) cells exit section 78, they enter a portion of flowpath, parts of which can be within housing 61, and parts of which can be outside of housing 61, in which the flowpath is adapted and configured to provide laminar flow of the foam 28. Therefore, the cross sectional area of the laminar flow section 82 is preferably larger than the representative cross sectional flow areas of nucleation section 65, growth section 74, or structuring section 78. Flow section 82 encourages laminar flow and also discourages turbulence that could otherwise reduce the quantity or quality of the foam. Still further, the output section of apparatus 60, along with the flow passageways extending to nozzle 30, are generally smooth, and with sufficiently gentle turn radii to further encourage laminar flow and discourage turbulence.
Gas tube 266 is located generally concentrically within housing 261 (although a concentric location is not required), such that liquid from inlet 263 flows generally around the outer surface of tube 266. Tube 266 preferably includes a plurality of regularly-spaced apertures 270 that are adapted and configured to flow gas from within tube 266 generally into the interior foam-creating passageway of housing 261. As shown in
The nucleation, growth, and cell structuring zones (272, 274, and 278, respectively) are arranged concentrically. The nucleation zone 272 is created between the outer periphery of tube or pipe 266. Wire mesh material 275 of growth section 274 wraps around the outer periphery of tube 266, as best seen in
After the merged (grown) and structured (improved homogeneity) cells exit section 278, they enter a portion of flowpath, parts of which can be within housing 261, and parts of which can be outside of housing 261, in which the flowpath is adapted and configured to encourage laminar flow of the foam 228 (as best seen in
Gas tube 366 is located generally concentrically within housing 361 (although a concentric location is not required), such that liquid from inlet 363 flows generally around the outer surface of tube 366. Tube 366 preferably includes a plurality of apertures 370 that are adapted and configured to flow gas from within tube 366 generally into the interior foam-creating passageway of housing 361. As shown in
Nucleation zone 365 includes jets or perforations 370 that are arranged in a plurality of subzones, the jets within such subzones 372 introducing gas into the flowing liquid at different angles of attack. A first nucleation zone 372a is located upstream of a second, intermediate nucleation zone 372b, which is followed by a third nucleation zone 372c (each of which is located along and spaced apart along the length of the gas chamber 366). As indicated on
The jets or perforations 370a within zone 372a are preferably adapted and configured to have an angle of attack that is generally opposite (or against) the prevailing flow of liquid (which flow is from left to right, as viewed in
The nucleation jets 370 within zone 372b are angled so as to impart a rotational swirl to the fluid within the foam flowpath. In one embodiment, the nucleation jets 370b are angled about 30-40 degrees from a normal line extending from the flowpath centerline, in a direction to impart tornado-like rotation within nucleation chamber 360.
A third nucleation zone 372c includes a plurality of jets 370c that are angled about 30-40 degrees in a direction so as to axially push liquid generally in the overall direction of flow within the foam flowpath (i.e., from left to right, and generally opposite of the angular orientation of jets 370a).
It is further understood that the perforations or nucleation jets 372 within a zone 370 may have angles of attack as previously described in their entirety among all jets or only partly in some of the jets. Yet other embodiments of the present invention contemplate zones 372a, 372b, 372c in which only some of the jets 370a, 370b, or 370c, respectively, are angled as previously described, with the remainder of the jets 370a, 370b, or 370c, respectively, being oriented differently. Still further, although what has been shown and described is a first zone A with an angle of attack opposite to that of fluid flow and followed by a second section zone B having jets with angles of attack oriented to impart swirl, and then followed by a third section zone C having jets with an angle of attack oriented so as to push foam toward the outlet, it is understood that various embodiments of the present invention contemplate still further arrangements of angled jets. As one example, yet other embodiments contemplate a fluid swirling section located at either the beginning or the end of the nucleation zone. As yet another example, still further embodiments contemplate a counter flow section (previously described as zone 372a) located toward the distal most end of the nucleation zone (i.e., oriented closer toward the growth section 374). In still further embodiments, there are nucleation zones comprising fewer than all three of the zones A, B, and C, including those embodiments having holes arranged with only one of the characteristics of the previously described zones A, B, and C.
Gas tube 466 is located generally concentrically within housing 461 (although a concentric location is not required), such that liquid from inlet 463 flows generally around the outer surface of tube 466. Tube 466 preferably includes a plurality of apertures 470 that are adapted and configured to flow gas from within tube 466 generally into the interior foam-creating passageway of housing 461. As shown in
Gas tube 566 is located generally concentrically within housing 561 (although a concentric location is not required), such that liquid from inlet 563 flows generally around the outer surface of tube 566. Tube 566 preferably includes a plurality of apertures 570 that are adapted and configured to flow gas from within tube 566 generally into the interior foam-creating passageway of housing 561. As shown in
The apertures within zones 572a, 572b, and 572c, are arranged generally as described previously with regards to nucleation chamber 560.
Gas tube 666 is located generally concentrically within housing 661 (although a concentric location is not required), such that liquid from inlet 663 flows generally around the outer surface of tube 666. Tube 666 preferably includes a plurality of apertures 670 that are adapted and configured to flow gas from within tube 666 generally into the interior foam-creating passageway of housing 661. As shown in
The foam within nucleation chamber 660 is first created within a nucleation zone 665 that includes the initial mixing of gas and liquid streams as previously discussed. As the foam leaves this zone, it flows into a downstream growth section 674 and passes over and around an ultrasonic transducer 675. In one embodiment, transducer 675 is a rod (as shown), although in yet other embodiments it is understood that the ultrasonic transducer is adapted and configured to provide sonic excitation to the foam exiting from nucleation zone 665, and can be of any shape. For example, yet other embodiments of the present invention contemplate a transducer having a generally cylindrical shape, such that the foam flows through the inner diameter of the cylinder, and in some embodiments in which the transducer is smaller than the inner diameter of flowpath 661, the foam also passes over the outer diameter of the transducer. Further, although one embodiment includes a transducer that is excited at ultrasonic frequencies, it is understood that yet other embodiments contemplate sensors that vibrate and impart vibrations to the nucleated foam at any frequency, including sonic frequencies and subsonic frequencies.
Referring to the smaller inset figure of
As the larger foam cells exit growth section 674, they enter a cell structuring section 678 that preferably includes a material 679 within the internal foam passage of housing 661. The material 679 of cell-structuring section 678 is adapted and configured to receive a first, larger distribution of foam cell sizes from section 674, and provide to output 664 a second, smaller, and tighter distribution of cell sizes. In some embodiments, the structuring material 679 includes a mesh.
Gas tube 766 is located generally concentrically within housing 761 (although a concentric location is not required), such that liquid from inlet 763 flows generally around the outer surface of tube 766. Tube 766 preferably includes a plurality of nucleation devices 770, each of which include a plurality of small holes for the passage of air. As shown in the inset figure of
More generally, device 770 includes an internal flowpath that receives gas under pressure from within chamber 766. An end of the device 770 includes a plurality of holes (achieved such as by use of porous metal, or achieved by drilling, stamping, chemically etching, photoetching, electrodischarge machining, or the like) in a pattern (random or ordered) such that gas from the internal passageway of device 770 flows into the surrounding mixture of liquids and creates foam. As best seen in
Sill further embodiments contemplate a gas chamber 766 that is fabricated from a porous metal, such as the porous metal discussed above. In such embodiments, gas escapes from the chamber and into the liquid flowpath along the entire length of the porous structure. Still further, some embodiments contemplate gas chambers that are constructed from a material that includes a plurality of holes (formed by drilling, stamping, chemically etching, photoetching, electrodischarge machining, or the like).
Gas tube 866 is located generally concentrically within housing 861 (although a concentric location is not required), such that liquid from inlet 863 flows generally around the outer surface of tube 866. Tube 866 preferably includes a plurality of devices 870 similar to the nucleation jets 770 described previously.
The foam within nucleation chamber 860 is first created within a nucleation zone 872 that includes the initial mixing of gas and liquid streams as previously discussed. As the foam leaves this zone, it flows into a downstream growth section 874 and passes over a corresponding growth material 875. In some embodiments, material 875 is a mesh preferably formed from a metallic material. Plastic materials can also be substituted, provided that the organic material can withstand exposure to the liquids 822 used for cleaning. It is further contemplated by yet other embodiments that material 875 can be materials other than a mesh.
As the larger foam cells exit growth section 874, they enter a cell structuring section 878 that preferably includes a material 879 within the internal foam passage of housing 861. The material 879 of cell-structuring section 878 is adapted and configured to receive a first, larger distribution of foam cell sizes from section 874, and provide to output 864 a second, smaller, and tighter distribution of cell sizes. In some embodiments, the structuring material 879 includes a mesh formed from a metal, with the cell size of the mesh of section 878 being smaller than the mesh size of growth section 874. In one trial, a device 860 was successful in converting much of the liquids to foam.
Gas chamber 966 is located generally within the foam flowpath of chamber 960, such that liquid from inlet 963 flows generally around the outer surfaces of chamber 966. In one embodiment and as depicted in the inset figure of
In one embodiment, chamber 1066 includes a supply plenum 1066.1 that is in fluid communication with a plurality of longitudinally-extending tubes 1066.2. Preferably, each of tubes 1066.1 and 1066.2 extend within the flowpath of nucleation chamber 1060, and further incorporate a plurality of nucleation jets 1070. As seen in
In some embodiments of the present invention, the total flow area of all nucleation jets is in the range from about 50 percent of the cross sectional flow area N of the gas plenum, to about three times the total cross sectional flow area N of the glass plenum. In order to achieve this ratio of total nucleation jet area to total plenum cross sectional area, the length NL can be adjusted accordingly. In still further embodiments, the ratio of the cross sectional area O of the inner diameter of the nucleation device to the area N of the gas plenum should be less than about five.
Foam from the nozzle 20 supported by boom 23 is provided into the inlet of engine 10, preferably as engine 10 is rotated by its starter. Foam 28 is injected into the inlet 11 as engine 10 is rotated on its starter. In some embodiments, the typical operation of the starter results in a maximum engine motoring (i.e., non-operating) speed, which is typically less than the engine idle (i.e., operating) speed. However, in some embodiments, the method of utilizing system 20 preferably includes rotating the engine at a rotational speed less than the typical motoring speed. With such lower speed operation, the cold section components of engine 10 are less likely to reduce the quality or quantity of foam before it is provided to the engine hot section. In one embodiment, the preferred rotational speed during cleaning is from about 25 percent of the motoring speed to less than about 75 percent of the motoring speed.
As one example, some compressor sections are known to include one or more manifolds or pipes that carry compressed air, such as for providing bleed air to the aircraft or providing relatively cool compressed air for cooling of the engine hot section. In some embodiments, cleaning foam is provided to the engine through these manifolds or pipes. This foam can be provided while the engine is being rotated, or while the engine is static. Further, engine hot sections are known to include pipes or manifolds that receive cooler, compressed air for purposes of cooling the hot section, and blanked-off ports used for boroscope inspections or other purposes. Yet other embodiments of the present invention contemplate the introduction of foam into such pipes and ports, either in a static engine or a rotating engine.
The trailer preferably includes a plurality of collection devices that can be conveniently folded down into a compact shape for transport. These devices can also be extended and supported in an upright condition for collection of foam during the cleaning process.
The aft end of trailer 232.1 includes a collector 232.4 that is adapted and configured to catch runoff from the inlet of the washed engine, and also from underneath the engine if nacelle doors are open. Collector 232.4 extends from the forward end of trailer 232.2, and when supported by vertical supports 232.43 presents an upward angle toward the inlet of the engine being cleaned. Any foam coming out of the engine inlet or out from the engine nacelle falls upon the drainage path created by the support of a sheet 232.41 between a pair of spaced apart, substantially parallel support ribs 232.42. Each of these ribs is pivotally connected to the forward end of the trailer. The vertical supports 232.43 each attach to a rib, and contact the ground. Any foam that falls onto the drain path of concave sheet 232.41 moves by way of gravity toward pool 232.2.
Various aspects of different embodiments of the present invention are expressed in paragraphs X1, X2, X3, X4, X5, X6 and X7 as follows:
Yet other embodiments pertain to any of the previous statements X1, X2, X3, X4, X5, X6 or X7, which are combined with one or more of the following other aspects. It is also understood that any of the aforementioned X paragraphs include listings of individual features that can be combined with individual features of other X paragraphs.
Wherein the first flow portion, the second flow portion, and the third flow portion have substantially the same flow area.
Wherein the housing has an internal wall and an internal axis, and the direction of the internal flowpath is from the axis toward the internal wall.
Wherein at least two of the first, second, and third flow portions are concentric, or the third flow portion is outermost from the first or second portions, or the first flow portion is innermost of the second or third portions.
Wherein the first, second, and third flow portions are concentric, and the second flow portion is between the first portion and the second portion.
Wherein the direction of the internal flowpath is from the liquid inlet toward the foam outlet.
Wherein said growth member includes a wire mesh.
Wherein the wire mesh has a first mesh size, and said structuring member includes a wire mesh having a second mesh size smaller than the first mesh size.
Wherein said mesh comprises a plastic material or a metallic material.
Wherein said structuring member includes an aperture plate, grating, or fibrous matrix.
Wherein said flowing the first foam over a member increases the turbulence of the first foam.
Which further comprises flowing the third foam within a chamber having an inlet and an outlet, the chamber being adapted and configured to decrease the turbulence of the third foam.
Wherein the chamber is adapted and configured to provide more laminar flow of the third foam between the inlet and the outlet.
Wherein said mixing includes flowing the liquid in a first direction and injecting the gas in a second direction that has a velocity component at least partly opposite to the first direction.
Wherein said flowing the second foam is at a velocity, and which further comprises flowing the third foam at substantially the same velocity onto an object and cleaning the object.
Wherein said nozzle is adapted and configured to provide the stream of foam to a bleed air duct of a jet engine.
Wherein said nozzle is adapted and configured to provide the stream of foam to a manifold of tubing mounted to a jet engine.
Wherein the stream has a substantially constant diameter.
Wherein the nozzle has a first flow area, the conduit has a second flow area, and the first flow area is about the same as the second flow area.
Wherein the foam outlet has a first flow area, the conduit has a second flow area, and the first flow area is about the same as the second flow area.
Wherein the nozzle is one or more nozzles having a total flow area, the foam outlet has an outlet area, and the outlet area is about the same as the total flow area.
Wherein said nucleation device includes an air-pressurized plenum having a plurality of airflow apertures and located within a chamber provided with a flow of the liquid, the apertures expelling air into the flowing liquid to create the foam.
Wherein the air received by said nucleation device has a pressure more than about ten psig and less than about one hundred and twenty psig, and the liquid received by said nucleation device has a pressure more than about ten psig and less than about one hundred and twenty psig.
Wherein the streamed supply is at a velocity greater than about three feet per second and less than about fifteen feet per second.
Wherein the streamed supply is a unitary stream of substantially constant diameter.
Wherein said providing includes a cell growth chamber downstream of the mixing chamber and which further comprises growing the size of the foam cells after said mixing and before said streaming.
Wherein said providing includes a turbulence-reducing chamber downstream of the mixing chamber and which further comprises reducing the turbulence of the mixed foam after said mixing and before said streaming.
Wherein the installed engine is substantially vertical in orientation, and wherein said streaming is into the installed inlet without rotation of the engine.
Wherein said growing means includes a growing mesh, said reducing means includes a reducing mesh, and the mesh size of the reducing mesh is smaller than the mesh size of the growing mesh.
Wherein said growing means is adapted and configured to provide surface area for attachment and merging of cells of the foam from said mixing means.
Wherein said growing means includes a plurality of first passageways, and said reducing means is adapted and configured to reduce the size of at least some of the grown cells by passing the grown cells through a plurality of second passageways smaller than the first passageways.
Wherein said mixing means is the injection of the gas from within a tube into flowing liquid.
Wherein said mixing means is by providing the pressurized gas into flowing liquid through a porous metal filter.
Wherein said mixing means includes a motorized rotating impeller.
Wherein said mixing means imparts swirl into the flowing liquid by injection of the gas.
Wherein said growing means is a vibrating rod, or is an ultrasonic transducer.
Which further comprises providing the measured performance of the specific engine to the owner of the engine, and said determining is by the engine owner.
Wherein the operational parameter is the start time.
Wherein the operational parameter is the specific fuel consumption of the engine.
Wherein the operational parameter is the carbon or oxides of nitrogen emitted by the engine.
Wherein said measuring is during commercial passenger operation.
Which further comprises a vertical support attached at one end to the trailer and at the other end to one of said first ribs, wherein said vertical support maintains the enclosed flowpath in an upright condition to facilitate gravity-induced drainage from the inlet to the drain.
Which further comprises a vertical support attached at one end to the trailer and at the other end to one of said second ribs, wherein said vertical support maintains the drain path at an upward angle to facilitate gravity-induced flow toward the liner.
While the inventions have been illustrated and described in detail in the drawings and foregoing description, the same is to be considered as illustrative and not restrictive in character, it being understood that only certain embodiments have been shown and described and that all changes and modifications that come within the spirit of the invention are desired to be protected.
This application is a continuation of U.S. patent application Ser. No. 17/862,393, filed Jul. 11, 2022, which is a continuation of U.S. patent application Ser. No. 16/173,690, filed Oct. 29, 2018, now issued as U.S. Pat. No. 11,643,946, which is a continuation of U.S. patent application Ser. No. 15/026,512, filed Mar. 31, 2016, now issued as U.S. Pat. No. 10,364,699, which is a 35 U.S.C. § 371 national-stage filing of International Patent Application PCT/US2014/058865, filed Oct. 2, 2014, which claims the benefit of priority to U.S. Provisional Patent Application No. 61/900,749, filed Nov. 6, 2013, and which claims the benefit of priority to U.S. Provisional Patent Application No. 61/885,777, filed Oct. 2, 2013, all of which are incorporated herein by reference.
| Number | Date | Country | |
|---|---|---|---|
| 61900749 | Nov 2013 | US | |
| 61885777 | Oct 2013 | US |
| Number | Date | Country | |
|---|---|---|---|
| Parent | 17862393 | Jul 2022 | US |
| Child | 18808458 | US | |
| Parent | 16173690 | Oct 2018 | US |
| Child | 17862393 | US | |
| Parent | 15026512 | Mar 2016 | US |
| Child | 16173690 | US |
