The present inventive concept relates generally to engines. More specifically, the present inventive concept is concerned with apparatuses, systems, and methods for injecting fuel into an engine, Even more specifically, the present inventive concept is concerned with apparatuses, systems, and methods for injection of fuels requiring low ignition energy and/or possessing high combustion energy, such as hydrogen.
The use of hydrogen as a fuel in internal combustion engines has the potential to provide many benefits. Hydrogen fuel is capable of being a zero-carbon fuel and has a high energy content per unit mass. Nevertheless, hydrogen fuel is hazardous because of the low ignition energy and high combustion energy of hydrogen, and because it tends to leak easily. As such, conventional systems and methods of fuel injection do not work well with hydrogen fuel.
Therefore, it is desirable to provide apparatuses, systems, and methods for injection of fuels such as hydrogen.
The present inventive concept comprises apparatuses, systems, and methods for injection of fuels requiring low ignition energy and/or possessing high combustion energy, such as hydrogen.
An embodiment of the inventive concept comprises a fuel injection system that includes a completely sealed housing surrounding the key components of the fuel injection system. In some embodiments, the housing surrounds a bidirectional brushless servo motor. One or more orifices extend through a wall of the housing for positive and negative leads to the servo motor. In some embodiments seats or other sealing components surround the leads to prevent leakage through the orifice(s) around the leads. In some embodiments, the housing further includes a housing structure of a needle valve assembly. A drive shaft of the servo motor engages with a stem/plunger that extends into the needle valve assembly housing. Rotation of the servo motor causes the plunger to move up or down (or to the right/left as shown in
The use of a brushless servo motor and sealed housing of the instant inventive concept allows for injection of fuels such as hydrogen input into an injector and out therefrom with the ability to open and close the injector (thereby fully controlling the flow of fuel) without pre-detonation or leakage.
It will be appreciated that various embodiments of the inventive concept are laid out in multiple different ways and structural arrangements. For example, in some embodiments, the servo motor shaft includes a square sleeve that surrounds and engages with the plunger of the needle valve assembly, allowing the plunger to be rotated while at the same time sliding up and down within the square shaft of the servo motor. In other embodiments, screw drive or gear drive assemblies are utilized in connection with the servo motor and needle valve assemblies.
In some embodiments, the nozzle/outlet of the needle valve assembly is positioned to inject fuel into the prechamber of an engine. In some embodiments, the nozzle/outlet of the needle valve assembly is positioned to inject fuel into the intake of a combustion engine.
It will be appreciated that other embodiments of the inventive concept include other types of motors, solenoids, or other suitable mechanisms to control the up/down (right/left, or in/out) motion of the needle valve plunger.
The foregoing and other objects are intended to be illustrative of the inventive concept and are not meant in a limiting sense. Many possible embodiments of the inventive concept may be made and will be readily evident upon a study of the following specification and accompanying drawings comprising a part thereof. Various features and subcombinations of inventive concept may be employed without reference to other features and subcombinations. Other objects and advantages of this inventive concept will become apparent from the following description taken in connection with the accompanying drawings, wherein is set forth by way of illustration and example, an embodiment of this inventive concept and various features thereof.
A preferred embodiment of the inventive concept, illustrative of the best mode in which the applicant has contemplated applying the principles, is set forth in the instant description and is shown in the drawings.
As required, a detailed embodiment of the present invention is disclosed herein; however, it is to be understood that the disclosed embodiment is merely exemplary of the principles of the invention, which may be embodied in various forms. Therefore, specific structural and functional details disclosed herein are not to be interpreted as limiting, but merely as a basis for the claims and as a representative basis for teaching one skilled in the art to variously employ the present invention in virtually any appropriately detailed structure.
Referring to
In various embodiments of the system of
In the foregoing description, certain terms have been used for brevity, clearness and understanding; but no unnecessary limitations are to be implied therefrom beyond the requirements of the prior art, because such terms are used for descriptive purposes and are intended to be broadly construed. Moreover, the description and illustration of the inventions is by way of example, and the scope of the inventions is not limited to the exact details shown or described.
Although the foregoing detailed description of the present invention has been described by reference to an exemplary embodiment, and the best mode contemplated for carrying out the present invention has been shown and described, it will be understood that certain changes, modification or variations may be made in embodying the above invention, and in the construction thereof, other than those specifically set forth herein, may be achieved by those skilled in the art without departing from the spirit and scope of the invention, and that such changes, modification or variations are to be considered as being within the overall scope of the present invention. Therefore, it is contemplated to cover the present invention and any and all changes, modifications, variations, or equivalents that fall with in the true spirit and scope of the underlying principles disclosed and claimed herein, Consequently, the scope of the present invention is intended to be limited only by the attached claims, all matter contained in the above description and shown in the accompanying drawings shall be interpreted as illustrative and not in a limiting sense.
Having now described the features, discoveries and principles of the invention, the manner in which the invention is constructed and used, the characteristics of the construction, and advantageous, new and useful results obtained; the new and useful structures, devices, elements, arrangements, parts and combinations, are set forth in the appended claims.
It is also to be understood that the following claims are intended to cover all of the generic and specific features of the invention herein described, and all statements of the scope of the invention which, as a matter of language, might be said to fall therebetween.
This application claims priority pursuant to 35 USC. 119(e) to U.S. Provisional Patent Application Ser. No. 63/279,163, filed Nov. 14, 2021, the entire disclosure of which is incorporated herein by reference.
Number | Name | Date | Kind |
---|---|---|---|
465907 | Whipple | Dec 1891 | A |
600723 | Johnson | Mar 1898 | A |
621193 | Wilson | Mar 1899 | A |
711083 | Taylor | Oct 1902 | A |
717445 | Nestius | Dec 1902 | A |
726896 | Franzen | May 1903 | A |
761512 | Lecomte | May 1904 | A |
822700 | Steele | Jun 1906 | A |
830124 | Weeks | Sep 1906 | A |
868841 | Calkins | Oct 1907 | A |
888806 | Hopkins | May 1908 | A |
909774 | Flora | Jan 1909 | A |
983754 | Nichols | Feb 1911 | A |
994825 | Dunbar | Jun 1911 | A |
1052045 | Doedyns | Feb 1913 | A |
1078301 | Moore | Nov 1913 | A |
1098256 | Harper | May 1914 | A |
1229949 | Harrigan | Jun 1917 | A |
1242826 | Llewellyn | Oct 1917 | A |
1277018 | Wolfington | Aug 1918 | A |
1320892 | Munn | Nov 1919 | A |
1376397 | Bylger | May 1921 | A |
1406140 | Julius | Feb 1922 | A |
1488528 | Luigi | Apr 1924 | A |
1567912 | Falkland | Dec 1925 | A |
1737942 | Pagel | Dec 1929 | A |
1850904 | Woodward | Mar 1932 | A |
1872361 | John | Aug 1932 | A |
2168726 | Frank | Aug 1939 | A |
2297529 | Frank | Sep 1942 | A |
2367676 | Griffith | Jan 1945 | A |
2447929 | Frank | Aug 1948 | A |
2478206 | Redding | Aug 1949 | A |
2504414 | Hawthorne | Apr 1950 | A |
2505660 | Baumann | Apr 1950 | A |
2526409 | Price | Oct 1950 | A |
2526941 | Fishbein | Oct 1950 | A |
2541098 | Redding | Feb 1951 | A |
2614503 | Berry | Oct 1952 | A |
2636480 | Becker | Apr 1953 | A |
2702985 | Raymond | Mar 1955 | A |
2817322 | Ralph | Dec 1957 | A |
2920610 | Breelle | Jan 1960 | A |
3153907 | Griffith | Oct 1964 | A |
3203406 | Georges | Aug 1965 | A |
3435808 | Allender | Apr 1969 | A |
3550565 | Sanchez | Dec 1970 | A |
3674960 | Krantz | Jul 1972 | A |
3797237 | Kamiya | Mar 1974 | A |
3863609 | Ikarashi | Feb 1975 | A |
4053136 | Perl | Oct 1977 | A |
4144004 | Edwards | Mar 1979 | A |
4169451 | Niggemeyer | Oct 1979 | A |
4432314 | Pelekis | Feb 1984 | A |
5596963 | Lai | Jan 1997 | A |
5996965 | Eichholz | Dec 1999 | A |
6129067 | Riley | Oct 2000 | A |
6250602 | Jansen | Jun 2001 | B1 |
6321713 | Mallen | Nov 2001 | B1 |
6394775 | White | May 2002 | B1 |
6488004 | Adamovski | Dec 2002 | B1 |
6672274 | Winterpacht | Jan 2004 | B2 |
7682139 | Riley et al. | Mar 2010 | B2 |
7713042 | Rodgers | May 2010 | B1 |
RE41373 | Gehman | Jun 2010 | E |
8517706 | Lurtz | Aug 2013 | B2 |
8616176 | Jacobsen et al. | Dec 2013 | B2 |
9091201 | Kristani | Jul 2015 | B1 |
9334793 | Marc | May 2016 | B1 |
10094218 | Hartmans | Oct 2018 | B1 |
10145243 | Ribbens et al. | Dec 2018 | B2 |
10844782 | Riley | Nov 2020 | B1 |
11352975 | Pursifull | Jun 2022 | B1 |
11384684 | Riley | Jul 2022 | B2 |
11788462 | Riley | Oct 2023 | B2 |
12163461 | Riley | Dec 2024 | B2 |
20010035163 | Rahardja | Nov 2001 | A1 |
20030084882 | Kabat | May 2003 | A1 |
20050081818 | Mueller | Apr 2005 | A1 |
20050235949 | Okada | Oct 2005 | A1 |
20060120910 | Lurtz | Jun 2006 | A1 |
20060150946 | Wright | Jul 2006 | A1 |
20090174290 | Cooke | Jul 2009 | A1 |
20090255506 | Walker | Oct 2009 | A1 |
20090308347 | Hathaway et al. | Dec 2009 | A1 |
20100116241 | Mistry | May 2010 | A1 |
20100219360 | Mumford | Sep 2010 | A1 |
20110041933 | Pisot | Feb 2011 | A1 |
20110259296 | Jacobsen et al. | Oct 2011 | A1 |
20130139785 | Shkolnik et al. | Jun 2013 | A1 |
20130327291 | Pett, Jr. | Dec 2013 | A1 |
20130336829 | Steinbauer et al. | Dec 2013 | A1 |
20140238337 | Hruschka et al. | Aug 2014 | A1 |
20140245988 | Villeneuve et al. | Sep 2014 | A1 |
20140261290 | Herbruck et al. | Sep 2014 | A1 |
20150308272 | Rolus Borgward | Oct 2015 | A1 |
20180073658 | Ramsperger | Mar 2018 | A1 |
20200378348 | Zhang | Dec 2020 | A1 |
20210040885 | Riley | Feb 2021 | A1 |
20220056802 | Riley | Feb 2022 | A1 |
20230092617 | Riley | Mar 2023 | A1 |
Number | Date | Country |
---|---|---|
102428259 | Apr 2012 | CN |
112912601 | Jun 2021 | CN |
112912601 | Sep 2023 | CN |
117090708 | Nov 2023 | CN |
724091 | Aug 1942 | DE |
736114 | Jun 1943 | DE |
4010573 | Jun 2022 | EP |
40075725 | Jan 2023 | HK |
202202753 | Jun 2022 | ID |
202037020268 | Jul 2021 | IN |
2009-545699 | Dec 2009 | JP |
2022-544188 | Oct 2022 | JP |
10-20190130934 | Nov 2019 | KR |
10-2022-0042039 | Apr 2022 | KR |
A2022001579 | Jul 2022 | MX |
2316660 | Feb 2008 | RU |
2325542 | May 2008 | RU |
2551718 | May 2015 | RU |
2201000799 | May 2023 | TH |
202106966 | Feb 2021 | TW |
2012159637 | Nov 2012 | WO |
2018187811 | Oct 2018 | WO |
2021029906 | Feb 2021 | WO |
2022026777 | Feb 2022 | WO |
2022096868 | May 2022 | WO |
2022026777 | Jun 2022 | WO |
Entry |
---|
“Commercial Aviation Safety Team: CAST;“Fundamentals of Gas Turbine Engines””, https://www.cast-safety.org/pdf/3_engine_fundamentals.pdf; last accessed Apr. 16, 2020. |
“Corrected Notice of Allowability Received for U.S. Appl. No. 16/732,318, mailed on Jun. 13, 2022”. |
“Corrected Notice of Allowability Received for U.S. Appl. No. 16/732,318, mailed on Mar. 25, 2022.”. |
“Corrected Notice of Allowability received for U.S. Appl. No. 16/732,318, Mailed on May 12, 2022.”. |
“Final Office Action Received for U.S. Appl. No. 16/732,318, mailed on Aug. 12, 2021”. |
“First Office Action received for China Application No. 202080000213.8 , dated Feb. 22, 2022.”. |
“International Preliminary Report on Patentability for International Application PCT/US2020/013933, Report issued Feb. 3, 2022, Mailed on Feb. 17, 2022.”. |
“International Search Report and Written Opinion for International Application No. PCT/US2020/013933, Search completed Jun. 9, 2020, Mailed Jun. 9, 2020.”. |
“International Search Report and Written Opinion for International Application No. PCT/US2021/043801, Search completed on May 3, 2022 Mailed on May 3, 2022.”. |
“Karim Nice, How Rotary Engines Work, Feb. 9, 2021”. |
“Non-Final Action received for U.S. Appl. No. 16/732,318, Mailed on Feb. 1, 2021”. |
“Non-Final Office Action received for U.S. Appl. No. 17/389,239, Mailed on Aug. 12, 2022”. |
“Non-Final Office Action Received for Application No. 16/745,184, Mailed on Jun. 23, 2020”. |
“Notice of Allowance received for US Application No. 16/745,184, Mailed on Oct. 8, 2020.”. |
“Notice of Allowance received for U.S. Appl. No. 16/732,318, Mailed on Mar. 2, 2022”. |
“Notice of Decision to Grant Received for South Africa Patent Application No. 2022/02809, Mailed on Sep. 26, 2022.”. |
“Restriction Requirement Received for U.S. Appl. No. 17/389,239, mailed on Apr. 19, 2022.”. |
“Restriction Requirement Received for U.S. Appl. No. 16/732,318, mailed on Nov. 23, 2020.”. |
“Second Office Action received for China Patent Application No. 202080000213.8 , Mailed on Sep. 14, 2022.”. |
Clark, John M, et al., “For Industry: Gas Turbine vs. Reciprocating Naval Engineers Journal; Feb. 1967; vol. 79, Issue 1 (pp. 103-106)”. |
“Restriction Requirement Received for U.S. Appl. No. 17/862,172, mailed on Feb. 24, 2023.”. |
“Final Office Action received for U.S. Appl. No. 17/862,172, Mailed on Dec. 22, 2023”. |
“Non-Final Office Action received for U.S. Appl. No. 17/862,172, Mailed on May 30, 2023”. |
“Decision of Rejection Received for Japan Patent Application No. 2022-507795, Mailed on Jan. 31, 2024.”. |
“Decision on Final Rejection Received for Korean Patent Application No. 10-2020-7006369, Mailed on Jul. 3, 2023.”. |
“Examination Report Received for Taiwan Application No. 109103549 mailed on Oct. 6, 2023.”. |
“Extended European Search Report Received for European Patent Application No. 20853437.0, Search completed on Jul. 25, 2023, Mailed on Aug. 3, 2023.”. |
“International Preliminary Report on Patentability for International Application PCT/US2021/043801, Report issued Jan. 31, 2023, Mailed on Feb. 9, 2023.”. |
“Notice of Decision to Grant Received for China Patent Application No. 202080000213.8, Mailed on Jun. 28, 2023.”. |
“Notice of Decision to Grant Received for Korean Patent Application No. 10-2020-7006369, Mailed on Oct. 13, 2023.”. |
“Office Action received for Indonesia Patent Application No. P00202203069, Mailed on Sep. 11, 2023.”. |
“Office Action Received for Japan Patent Application No. 2022-607795, Mailed on Jul. 4, 2023.”. |
“Office Action Received for Korean Patent Application No. 10-2020-7006369, Mailed on Mar. 16, 2023.”. |
“Search & Written Opinion Report Received for Singapore Patent Application No. 11202201141V, Mailed on Dec. 5, 2023.”. |
“Third Office Action received for China Patent Application No. 202080000213.8 , Mailed on Apr. 5, 2023.”. |
“Supplemental Notice of Allowability Received for U.S. Appl. No. 17/862,172, mailed on Nov. 8, 2024”. |
Number | Date | Country | |
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63279163 | Nov 2021 | US |