This disclosure relates to systems and methods for facilitating dissociation of methane at low temperatures and/or pressures utilizing a reactor designed to generate shockwaves in a supersonic gaseous vortex.
In recent times, there has been a surge in methane produced from hydraulic and explosive fracturing and/or gas production from conventional gas wells in the continental United States and elsewhere around the world. This has led to the price of methane and natural gas falling to the point where many wells are being capped because they are no longer economical. There are many gas wells and oil wells around the world that are either stranded or too small for a pipeline to connect them into the main gas pipeline system. As such, the gas is typically flared or burnt. This gas flaring may represent a very heavy increase in production of carbon dioxide and CO2 equivalents attributed to global climate change. This flaring may also represents a very significant waste of energy and money. Conventional technologies exist for converting methane into useful products that commonly include the Haber Bosch process, which converts nitrogen extracted from ambient air together with hydrogen extracted from methane to produce ammonia, urea, and/or other products. Generally speaking, existing technologies involve high-pressure and high-temperature and are very difficult to implement on a small scale.
One aspect of the disclosure relates to a system configured for facilitating dissociation of methane at low temperatures and/or pressures utilizing a reactor designed to generate shockwaves in a supersonic gaseous vortex. According to exemplary implementations, the system, by using a combination of mechano chemistry and catalysis, may achieve disassociation of methane at relatively low temperatures and/or relatively low pressures. The system may be scaled across a very wide range from implementations configured to process kilos of methane per hour to implementations configured to process thousands of kilos of methane per hour. In some implementations, because the temperature and pressures are restricted to a relatively small reactor, the reactor may be constructed from non-exotic materials.
In accordance with one or more implementations, the system may include one or more of a preprocessing chamber, a reactor, a gas/solid separator, and/or other components. The preprocessing chamber may be configured to receive methane. The preprocessing chamber may be configured to pressurize the methane to a pressure of 300 kPa or more. The preprocessing chamber may be configured to heat the methane to a temperature below a dissociation temperature of methane. The reactor may be configured to dissociate methane received from the preprocessing chamber. The reactor may be configured to operate at a temperature above the dissociation temperature of methane. The reactor may include a chamber having an internal surface that is substantially axially symmetrical about a longitudinal axis. The reactor may include a gas inlet disposed at a first end of the chamber and arranged to emit the methane as a gas stream substantially tangentially to the inner surface of the chamber to effectuate a gaseous vortex rotating about the longitudinal axis within the chamber. The gas inlet may comprise a nozzle that accelerates the gas stream to a supersonic velocity. The nozzle may be structured to adjustably control a frequency of shockwaves emitted from the nozzle into the gaseous vortex. The reactor may include an outlet disposed on the longitudinal axis at a second end of the chamber opposite from the first end. The outlet may be configured to emit product gases and carbon byproduct from the chamber. The gas/solid separator may be configured to receive the product gases and carbon byproduct from the reactor and separate out the carbon byproduct from the product gases.
Another aspect of the disclosure relates to a method for facilitating dissociation of methane at low temperatures and/or pressures utilizing a reactor designed to generate shockwaves in a supersonic gaseous vortex. The method may include receiving methane into a preprocessing chamber. The method may include pressurizing the methane within the preprocessing chamber to a pressure of 350 kPa or more. The method may include heating the methane within the preprocessing chamber to a temperature below a dissociation temperature of methane. The method may include introducing the pressurized and heated methane from the preprocessing chamber into a reactor configured to dissociate methane. The reactor may be configured to operate at a temperature above the dissociation temperature of methane. The methane may be introduced into the reactor as a gas stream substantially tangentially to an inner surface of a chamber of the reactor to effectuate a gaseous vortex rotating about the longitudinal axis within the chamber. The gas stream may be introduced via a gas inlet. The gas inlet may comprise a nozzle that accelerates the gas stream to a supersonic velocity. The method may include controlling a frequency of shockwaves emitted from the nozzle into the gaseous vortex. The method may include emitting product gas and carbon byproduct from the chamber of the reactor via an outlet disposed on the longitudinal axis at a second end of the chamber opposite from the first end. The method may include separating out the carbon byproduct from the product gas using a gas/solid separator.
Exemplary implementations may provide a very economical way of producing large quantities of carbon and hydrogen. Gas that would otherwise be flared may instead be turned into useful end products. Carbon may be traded or used to improve soil fertility. Hydrogen may be used for clean energy production with the exhaust being water. It should be noted, however, that for some implementations only some (or none) of the identified advantages may be present and the potential advantages are not necessarily required for all of the implementations.
These and other features, and characteristics of the present technology, as well as the methods of operation and functions of the related elements of structure and the combination of parts and economies of manufacture, will become more apparent upon consideration of the following description and the appended claims with reference to the accompanying drawings, all of which form a part of this specification, wherein like reference numerals designate corresponding parts in the various figures. It is to be expressly understood, however, that the drawings are for the purpose of illustration and description only and are not intended as a definition of the limits of the invention. As used in the specification and in the claims, the singular form of “a”, “an”, and “the” include plural referents unless the context clearly dictates otherwise.
The preprocessing chamber 172 may be configured to receive methane. The preprocessing chamber 172 may be configured to pressurize the methane. According to some implementations, the methane may be pressurized to a pressure of 350 kPa or more. The preprocessing chamber 172 may be configured to heat the methane. In some implementations, the methane may be heated to a temperature below a dissociation temperature of methane. The pressurization and/or heating of the methane may be achieved with conventional apparatuses suited for those purposes, in accordance with some implementations.
The reactor 100 may be configured to receive methane from the preprocessing chamber 172. The reactor may be configured to dissociate methane. The reactor may be configured to operate at a temperature above the dissociation temperature of methane. In some implementations, the methane may enter the reactor 100 through a converging diverging nozzle. The nozzle dimensions may be configured to cause the methane exiting the nozzle to be travelling at least one and a half times speed of sound in methane at that temperature and pressure. The nozzle may be designed to impart supersonic shock waves in the gas. According to some implementations, the methane may be dissociated into one or more produce gases and/or one or more carbon byproducts. Examples of product gases and carbon byproducts may include one or more of hydrogen, alkenes, carbon dust, amorphous carbon, graphitic carbon, carbon nanoparticle structures, carbon nano tubes, graphene and/or other product gases and/or carbon by products.
Chamber 102 may be configured to provide a volume in which methane processing occurs. Chamber 102 may have a substantially circular cross-section centered on a longitudinal axis 124 that is normal to the cross-section. The substantially circular cross-section may facilitate a vortex rotating within chamber 102. A radius of the substantially circular cross-section of chamber 102 may continuously decrease at an end of chamber 102 proximal to outlet 108. The continuous decrease of the radius of the substantially circular cross-section of chamber 102 may be configured to cause an acceleration of a rotational speed of the gaseous vortex. As the continuous decrease of the radius of the substantially circular cross-section of chamber 102 may be shaped as a cone (illustrated in
Chamber 102 may be formed of various materials. Chamber 102 may be formed of a rigid material. Chamber 102 may be formed of a thermally conductive material. Chamber 102 may be formed of an electrically conductive material. According to some implementations, chamber 102 may be formed wholly or partially of steel, iron, iron alloys, silicon carbide, partially stabilized zirconia (PSZ), fused alumina, tungsten carbide, boron nitride, carbides, nitrides, ceramics, silicates, geopolymers, metallic alloys, other alloys, and/or other materials. In some implementations, an internal surface 116 of chamber 102 may be coated with one or more coatings. An exemplary coating may be configured to prevent physical or chemical wear to internal surface 116 of chamber 102. In some implementations, a coating may be configured to promote a chemical reaction within chamber 102. An example of a coating that may promote a chemical reaction may include one or more of iron; nickel; ruthenium; rhodium; platinum; palladium; cobalt; other transition metals and their alloys, compounds, and/or oxides (e.g., the lanthanide series and their compounds, alloys, and/or oxides); and/or other materials.
The first gas inlet 104 may be configured to introduce a high-velocity stream of methane gas into chamber 102. The first gas inlet 104 may be disposed and arranged so as to effectuate a vortex of the stream of gas circulating within chamber 102. The vortex may rotate about longitudinal axis of chamber 102. The gas inlet may be disposed so that the gas stream 116 is directed substantially perpendicular to longitudinal axis 124 of chamber 102. The first gas inlet 104 may be disposed so that the gas stream 116 is directed substantially tangent to a portion of the internal surface 126 of the substantially circular cross-section of chamber 102.
According to some implementations, the first gas inlet 104 may comprise inlet gas nozzle (not depicted in this example) disposed within the first gas inlet 104. In those implementations, the inlet nozzle may be configured to accelerate the stream of gas being introduced into chamber 102, to emit the stream of gas at a supersonic speed, to emit shockwaves in the stream of gas emitted from inlet nozzle, and/or for any other purposes. Exemplary implementations of a gas inlet (e.g., first gas inlet 104) and/or an inlet nozzle are disclosed in U.S. patent application Ser. No. 14/298,868 filed on Jun. 6, 2014 and entitled “A REACTOR CONFIGURED TO FACILITATE CHEMICAL REACTIONS AND/OR COMMINUTION OF SOLID FEED MATERIALS” and U.S. patent application Ser. No. 14/298,877 filed on Jun. 6, 2014, and entitled “SYSTEMS AND METHODS FOR PROCESSING SOLID MATERIALS USING SHOCKWAVES PRODUCED IN A SUPERSONIC GASEOUS VORTEX,” which are both incorporated herein by reference.
The gas stream 116 introduced by the first gas inlet 104 may include any number of gaseous materials. In some implementations, the gas may include one or more of steam, methane, ethane, propane, butane, pentane, ammonia, hydrogen, carbon monoxide, carbon dioxide, oxygen, nitrogen, chlorine, fluorine, ethene, hydrogen sulphide, acetylene, carbonyls and/or other halogenated metal complexes, and/or other gaseous materials. In some implementations, in the gas, a wide variety of chemical reactions that are normally multiple step reactions, e.g., due to Le Chateliers principle. Such a wide variety of chemical reactions may be possible in the reactor 100 because of the wide temperature and pressure difference within the reactor 100 itself. As soon as a given reaction has taken place due to pressure and/or temperature and/or catalytic action within the reactor the products are conveyed to a region within the reactor in nanoseconds where the temperature and pressure are reduced. This makes a great number of organic and organo metal reactions possible in a greatly reduced number of steps. It also makes many chemical reactions possible or economic that are not presently practicable or even attainable. Applications include pharmaceuticals, insecticides, and the precursor organo metals or carbonyls, which are used in Chemical Vapor Deposition (CVD) used in integrated circuit manufacture, electronics in general as well as 3D printing of metals
Methane may be processed by reactor 100 by mechanisms facilitated by shockwaves 128 within chamber 102. For example, methane may be processed by cavitation in the stream of gas within chamber 102. Methane may undergo a chemical transformation due to the catalytic effect built into the first replaceable part wear part 112, and/or due to the electric field imparted on the first replaceable part wear part 122.
The outlet 108 may be configured to emit the gas and processed material from chamber 102. The outlet 108 may be disposed at an end of chamber 102 opposite to the first gas inlet 104. The outlet may be disposed on longitudinal axis 124 of chamber 102.
In some implementations, outlet 108 may include one or more of an outlet nozzle 130 (illustrated in
For resisting wear in reactor 100, a first replaceable wear part 112 may be disposed at a first portion 122 of the inner surface 126 of chamber 102. The first portion 122 may be an area on the inner surface 126 where the stream 116 contacts the surface 126. As such, the first portion 122 may be opposite to the first gas inlet 104 within chamber 102. The first replaceable wear part 112 may be disposed at the first portion 122 in a way to absorb impacts to first portion 122 on the inner surface 126 caused by gases and/or carbon byproducts entrained by the gas stream 116 introduced by the first gas inlet 104. The first replaceable wear part 112 may be made of hard material such as tungsten carbide, titanium carbide, or titanium nitride, diamond, and/or any other materials for wear resistance. In some implementations, the first replaceable wear part 112 may have a polycrystalline diamond facing.
In some implementations, the first replaceable wear part 122 may be configured to continuously advance into the chamber as the surface of the contact end is worn.
In some implementations, the first replaceable wear part 112 may comprise a rotatable cylindrical rod adapted to control impacts of carbon byproducts. In those implementations, the cylindrical rod may rotate about the axis of its cylinder when the pulverized particles contact the rod. The rotation of the rod may allow the wear to be controlled on the surface of the rod.
Various forms of catalysis may be used to reduce the dissociation temperature and/or increase the reaction rate. In some implementations, the contacting end of the first replaceable wear part 112 may be coated with catalyst material. The coating may be configured to protect the surface of the contacting end of the first replaceable wear part 112, and/or to promote a chemical reaction within chamber 102. For example, the catalyst material may be incorporated into the matrix of the first replaceable wear part 112 during manufacturing of the first replaceable wear part 112. The catalyst material that may be coated on the contacting end of the first replaceable wear part 112 may include one or more of platinum, palladium, and/or any other catalyst material for aiding the chemical reaction(s), and/or the comminution inside chamber 102. The coating on the first replaceable wear part 112 may be configured such that the coated catalyst material ablates from the surface of the first replaceable wear part 112 at a rate that exposes a new clean surface of the first replaceable wear part 112. The ablated catalyst material may increase the throughput, and/or activity in chamber 102 by increasing the rate of reactions without a need to physically scale the size of reactor 100.
In some implementations, the first replaceable wear part 112 may be configured to be electronically isolated from chamber 102, and/or other components of reactor 100. This may facilitate an electrical field on the first replaceable wear part 112 having a variable voltage, amperage, frequency, waveform, and/or any other type(s) electrical potential to aid chemical reaction in chamber 102. In those implementations, the first replaceable wear part 112 may enable the Non-Faradaic Electrochemical Modification of Catalytic Activity (NEMCA), also known as Electrochemical Promotion of Catalysis (EPOC), for reducing energy required for comminution, and/or the chemical reactions inside chamber 102.
In some implementations the first replaceable wear part may be made entirely or partially of a material which is designed to act as the initiator or nucleus in carbon nanotube formation. This material may include iron and various alloys as well as materials like Ruthenium, which if incorporated into carbon nanotubes produces a material that exhibits super conductivity at elevated temperatures. It may also include rare earths and many other less exotic metals which give a wide variety of physical and electronic properties.
Returning to
In some implementations, inner surface 126 of chamber 102 may comprise pockets (e.g., disruptors) around the periphery of the chamber 126. The pockets may be configured with appropriate sizes to receive some or all of the process material such that it is packed into the inner surface 126.
In some implementations, additional gas inlets and replaceable wear parts may be included in reactor 100 to reduce and control effects caused by drag or boundary layers in reactor 100 as process material is required to travel a long flight path before existing.
Returning to
Other components that may be included in reactor 100 may include, a heating component configured to provide heat to chamber 102, a ventilation component 122 configured to vent gas from a region surrounding chamber 102, one or more sensors configured to provide a signal conveying information related to one or more parameters associated with reactor 100, and/or any other components. Exemplary implementations of reactor 100 and/or components of reactor 100 are disclosed in U.S. patent application Ser. No. 14/690,111 filed on Apr. 17, 2015 and entitled “PROVIDING WEAR RESISTANCE IN A REACTOR CONFIGURED TO FACILITATE CHEMICAL REACTIONS AND/OR COMMINUTION OF SOLID FEED MATERIALS USING SHOCKWAVES CREATED IN A SUPERSONIC GASEOUS VORTEX,” which is incorporated herein by reference.
From a theoretical point of view, 74.9 kJ may be needed per mole to dissociate methane. The enthalpy of combustion of the two moles of hydrogen produced from this dissociation can provide 572 kJ of energy. This may mean that the energy available from the combustion of the hydrogen exceeds the energy needed for dissociation by about seven times. According to some implementations, the overall efficiency of system 170, which may include a combination of insulation and recuperation, determines how much of the available energy may be needed for reactions and hence the amount of hydrogen leftover after dissociation.
Referring again to
The product gas separator 178 may be configured to receive product gases and separate the product gases into individual types or mixtures of gases. In some implementations, the product gas separator 178 may include
Commercial Off The Shelf (COTS) equipment and/or other suitable apparatuses.
In some implementations the gases can be separated by differential cyclones, or by liquefaction. By electro static charge, magnetic susceptibility, or by a Calutron type device which can separate gases with very small physical differences.
In some implementations, system 170 may include a gas cleanup unit (not depicted), which may be configured to clean the product gas. The gas cleanup unit may clean the product by way of one or more of dust collection, a dry and wet processes for removing gaseous pollutants, separating heavy metals, abating acid gas, abating dioxins, abating furans, and/or other processes for cleaning gas. With the addition of absorbents or adsorbents of typically alkali metal oxides, carbonates, hydroxides or the like, products like sulphur and chlorine can be captured in the primary reactor, with the byproducts reporting to the solids where they are readily separated.
With the ability to be adaptable to different volumes, the system 170 and/or reactor 100 may have a great ability to make use of gas streams that would otherwise be flared, and turn the waste gas stream from a liability into an asset. The hydrogen produced may be used as a feedstock for many applications both as a fuel in itself for stationary and/or mobile applications and as a chemical feedstock in a variety of operations such as the production of one or more of ammonia, nitric acid, ammonium nitrate, urea, cyanide, acetylene, and/or other useful substances. Exemplary implementations may be used to lighten heavy oils or tars into lighter fractions, which are more readily saleable and have much higher value. The carbon byproducts may have many existing markets ranging from printer inks, tire manufacturing, soil upgrading, various specialty markets, and/or other markets.
At an operation 602, methane may be received into a preprocessing chamber (e.g., preprocessing chamber 172).
At an operation 604, the methane within the preprocessing chamber may be pressurized. In some implementations, the methane may be pressurized to a pressure of 350 kPa or more.
At an operation 606, the methane within the preprocessing chamber may be heated to a temperature below a dissociation temperature of methane.
At an operation 608, the pressurized and heated methane from the preprocessing chamber may be introduced into a reactor (e.g., reactor 100) configured to dissociate methane. The reactor may be configured to operate at a temperature above the dissociation temperature of methane. The methane may be introduced into the reactor as a gas stream substantially tangentially to an inner surface of a chamber of the reactor to effectuate a gaseous vortex rotating about the longitudinal axis within the chamber. The gas stream may be introduced via a gas inlet disposed at a first end of the reactor. The gas inlet may comprise a nozzle that accelerates the gas stream to a supersonic velocity.
At an operation 610, a frequency of shockwaves emitted from the nozzle into the gaseous vortex may be controlled.
At an operation 612, product gas and carbon byproduct may be emitted from the chamber of the reactor via an outlet disposed on the longitudinal axis at a second end of the chamber opposite from the first end.
At an operation 614, the carbon byproduct may be separated out from the product gas using a gas/solid separator (e.g., gas/solid separator 176).
Although the present technology has been described in detail for the purpose of illustration based on what is currently considered to be the most practical and preferred implementations, it is to be understood that such detail is solely for that purpose and that the technology is not limited to the disclosed implementations, but, on the contrary, is intended to cover modifications and equivalent arrangements that are within the spirit and scope of the appended claims. For example, it is to be understood that the present technology contemplates that, to the extent possible, one or more features of any implementation can be combined with one or more features of any other implementation.
Number | Name | Date | Kind |
---|---|---|---|
2257907 | Griswold | Oct 1941 | A |
2532554 | Joeck | Dec 1950 | A |
2752097 | Lecher | Jun 1956 | A |
2997245 | Nilsson et al. | Aug 1961 | A |
3178121 | Wallace, Jr. | Apr 1965 | A |
3254848 | Stephanoff | Jun 1966 | A |
3257080 | Snyder | Jun 1966 | A |
3301292 | O'Connor | Jan 1967 | A |
3462086 | Bertrand et al. | Aug 1969 | A |
3565348 | Dickerson et al. | Feb 1971 | A |
3602439 | Nakayama | Aug 1971 | A |
3620946 | Michel | Nov 1971 | A |
3908904 | Kerner et al. | Sep 1975 | A |
4198004 | Albus et al. | Apr 1980 | A |
4248387 | Andrews | Feb 1981 | A |
4354641 | Smith | Oct 1982 | A |
4504017 | Andrews | Mar 1985 | A |
4515093 | Beardmore et al. | May 1985 | A |
4671192 | Hoffert et al. | Jun 1987 | A |
4919853 | Alvarez | Apr 1990 | A |
4921173 | Bartley | May 1990 | A |
5219530 | Hertzberg et al. | Jun 1993 | A |
5246575 | Alexander | Sep 1993 | A |
5277369 | Moriya et al. | Jan 1994 | A |
5306330 | Nasikas | Apr 1994 | A |
5855326 | Beliaysky | Jan 1999 | A |
6089026 | Hu | Jul 2000 | A |
6145765 | Capelle, Jr. et al. | Nov 2000 | A |
6152158 | Hu | Nov 2000 | A |
6158676 | Hughes | Dec 2000 | A |
6167323 | Komino | Dec 2000 | A |
6824086 | Mazurkiewicz et al. | Nov 2004 | B1 |
7137580 | Graham et al. | Nov 2006 | B2 |
7258290 | Taketomi et al. | Aug 2007 | B2 |
7398934 | Capelle, Jr. | Jul 2008 | B1 |
7621473 | Capelle, Jr. | Nov 2009 | B2 |
7789331 | Zehavi et al. | Sep 2010 | B2 |
7850105 | Ito et al. | Dec 2010 | B2 |
8172163 | Soliman Abdalla et al. | May 2012 | B2 |
8398007 | Ito et al. | Mar 2013 | B2 |
8480859 | Kostrov et al. | Jul 2013 | B2 |
8726532 | Hogan | May 2014 | B2 |
9050604 | Lansell et al. | Jun 2015 | B1 |
9452434 | Lansell et al. | Sep 2016 | B1 |
20040063874 | Muhle et al. | Apr 2004 | A1 |
20040200910 | Graham | Oct 2004 | A1 |
20060144760 | Duyvesteyn | Jul 2006 | A1 |
20070267527 | Graham et al. | Nov 2007 | A1 |
20080226535 | Park et al. | Sep 2008 | A1 |
20080236160 | Glotov | Oct 2008 | A1 |
20090241816 | Taylor | Oct 2009 | A1 |
20100025506 | Capelle, Jr. | Feb 2010 | A1 |
20100101978 | Gordon et al. | Apr 2010 | A1 |
20110206593 | Fahs, II et al. | Aug 2011 | A1 |
20110283705 | Oliver | Nov 2011 | A1 |
20110303013 | Kass | Dec 2011 | A1 |
20120131901 | Westervelt | May 2012 | A1 |
20120230877 | Pinchot | Sep 2012 | A1 |
20130221141 | Zhang et al. | Aug 2013 | A1 |
20130224488 | Dos Santos Antunes et al. | Aug 2013 | A1 |
20130309161 | Akay | Nov 2013 | A1 |
20130315792 | O'Dowd | Nov 2013 | A1 |
20130336845 | Chu | Dec 2013 | A1 |
20140058095 | Rende | Feb 2014 | A1 |
20140058165 | Bedard et al. | Feb 2014 | A1 |
20140058170 | Bedard | Feb 2014 | A1 |
20140058178 | Bedard | Feb 2014 | A1 |
20140110307 | Salazar-Guillen | Apr 2014 | A1 |
20140275687 | Beene et al. | Sep 2014 | A1 |
20150165414 | Gattupalli | Jun 2015 | A1 |
20150352558 | Lansell et al. | Dec 2015 | A1 |
20150361010 | Leonard | Dec 2015 | A1 |
20160243488 | Wells et al. | Aug 2016 | A1 |
20160296904 | Knowlen | Oct 2016 | A1 |
20170253492 | Beach et al. | Sep 2017 | A1 |
Number | Date | Country |
---|---|---|
103249667 | Aug 2013 | CN |
102013019949 | May 2015 | DE |
000004 | Sep 1997 | EA |
1048667 | Dec 1953 | FR |
1037770 | Aug 1966 | GB |
1037770 | Aug 1966 | GB |
2 029 621 | Feb 1995 | RU |
2520 | Aug 1996 | RU |
2 088 336 | Aug 1997 | RU |
WO 9408719 | Apr 1994 | WO |
WO 9733695 | Sep 1997 | WO |
2006067636 | Jun 2006 | WO |
2008083138 | Jul 2008 | WO |
2009073447 | Jun 2009 | WO |
2014210297 | Dec 2014 | WO |
2015053857 | Apr 2015 | WO |
Entry |
---|
International Preliminary Report on Patentability and the Written Opinion of the International Searching Authority as issued in International Patent Application No. PCT/US2015/034554, dated Sep. 3, 2015. |
International Preliminary Report on Patentability and the Written Opinion of the International Searching Authority as issued in International Patent Application No. PCT/US2015/034548, dated Sep. 8, 2015. |
Hartmann, J. et al, “Synchronisation of Air-Jet Generators with an Appendix on the Stem Generator”, Det Kgl. Danske Videnskabernes Selskab. Matematisk-fysiske Meddelelser, Bd. 26, No. 10, 1951(39 pages). |
Demare, D., et al., “Acoustic enhancement of combustion in lifted non-remixed jet flames”, The Combusion Institute, 139 (2004), 312-328, Elsevier, Inc. |
Simpson, E., et al., Acoustic Performance of a Cylindrical Disk-Type Resonator, Journal of Sound and Vibration, (1978) 60(1), 151-156, Academic Press Inc. (London) Limited. |
Narayanan, S., et al. “Acoustic characteristics of chamfered Hartmann whistles”, Journal of Sound and Vibration, 330 (2011) 2470-2496, Elsevier, Ltd. |
Narayanan, S. et al., Aero-acoustic features of internal and external chamfered Hartmann whistles: A comparative study, Journal of Sound and Vibration, 333 (2014) 774-787, Elsevier, Ltd. |
English machine translation for FR 1048667 A (Dec. 1953). |
Final Office Action dated Jan. 27, 2017 in corresponding U.S. Appl. No. 14/690,149 (14 pages). |
Derwent abstract of DE 102013019949 A1. |
International Preliminary Report on Patentability PCT/US2016/028167 dated Oct. 17, 2017. |
International Preliminary Report on Patentability PCT/US2016/028181 dated Oct. 17, 2017. |
International Search Report and Written Opinion dated Sep. 26,2016 in corresponding International Patent Application No. PCT/US2016/046641. |
Final Office Action dated Dec. 6, 2016 in corresponding U.S. Appl. No. 14/298,877 (10 pages). |
M. Reader-Harris, Orifice Plates and Venturi Tubes, Chapter 3: Venturi Tube Design, 2015, pp. 77-96. |
Non-Final Office Action U.S. Appl. No. 14/690,149 dated Jan. 25, 2018. |
International Preliminary Report on Patentability PCT/US2016/046641 dated Feb. 13, 2018. |
Final Office Action U.S. Appl. No. 14/690,149 dated Sep. 4, 2018. |
Notice of Allowance U.S. Appl. No. 141719,303 dated Jul. 25, 2018. |
Details of the First Office Action Chinese Patent Application No. 201680035572.0 dated Jul. 24, 2018 with English translation. |
Extended European Search Report dated Dec. 13, 2018 in related European Patent Application No. 16781030.8, 10 pages. |
Non-Final Office Action dated Jan. 10, 2019 in related U.S. Appl. No. 15/277,975, 10 pages. |
Decision to Grant dated Jan. 15, 2019 in related Chinese Patent Application No. 201680035572.0, 4 pages. |
Notice of Allowance dated Jan. 11, 2019 in related U.S. Appl. No. 14/690,149, 8 pages. |
Notice of Grant received on Apr. 10, 2019 in related Kazakstani Patent Application No. 2017/1058.1, 14 pages. |
Notice of Allowance dated May 22, 2019 in related U.S. Appl. No. 14/690,149, 7 pages. |
Final Office Action dated May 3, 2019 in related U.S. Appl. No. 15/277,975, 11 pages. |
Number | Date | Country | |
---|---|---|---|
20170043315 A1 | Feb 2017 | US |