Patents by Inventor Daanish MAQBOOL
Daanish MAQBOOL has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).
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Patent number: 11867138Abstract: A system and method for ram air intake for pulse combustion systems is disclosed that improves the ability of pulse combustions to ingest air into the inlet pipe when the pulse combustion system is moving in a direction opposite the direction the open end of the inlet pipe is facing and the system and method includes the ability to increase the thrust output from the pulse combustion system.Type: GrantFiled: October 28, 2022Date of Patent: January 9, 2024Assignee: NORTH AMERICAN WAVE ENGINE CORPORATIONInventor: Daanish Maqbool
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Publication number: 20230133001Abstract: A system and method for ram air intake for pulse combustion systems is disclosed that improves the ability of pulse combustions to ingest air into the inlet pipe when the pulse combustion system is moving in a direction opposite the direction the open end of the inlet pipe is facing and the system and method includes the ability to increase the thrust output from the pulse combustion system.Type: ApplicationFiled: October 28, 2022Publication date: May 4, 2023Inventor: Daanish MAQBOOL
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Patent number: 11592184Abstract: A system and method is disclosed for the start-up and control of pulsejet engines and this system includes an Electronic Fuel Injection (“EFI”) system that further includes one or more electrically controlled fuel injectors that can be selectively operated for start-up and control of such pulsejet engines. According to the system and method, the rate and/or pattern of fuel delivery to pulsejet engines can be varied not only by controlling the amount of time the fuel injectors are open versus closed to define a “duty cycle,” but also with the capability to selectively disable one or more fuel injectors in the programmed manner for start-up and control of such pulsejet engines.Type: GrantFiled: April 17, 2019Date of Patent: February 28, 2023Assignee: NORTH AMERICAN WAVE ENGINE CORPORATIONInventors: Daanish Maqbool, Nitay Ravin, Carson Myers
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Patent number: 11585532Abstract: A system and method is disclosed for the start-up and control of pulsejet engines and this system includes an Electronic Fuel Injection (“EFI”) system that further includes one or more electrically controlled fuel injectors that can be selectively operated for start-up and control of such pulsejet engines. According to the system and method, the rate and/or pattern of fuel delivery to pulsejet engines can be varied not only by controlling the amount of time the fuel injectors are open versus closed to define a “duty cycle,” but also with the capability to selectively disable one or more fuel injectors in the programmed manner for start-up and control of such pulsejet engines.Type: GrantFiled: April 17, 2019Date of Patent: February 21, 2023Assignee: NORTH AMERICAN WAVE ENGINE CORPORATIONInventors: Daanish Maqbool, Nitay Ravin, Carson Myers
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Patent number: 11578681Abstract: A pulse combustor system for operating pulse combustors in anti-phase. The pulse combustor system includes two pulse combustors connected at their combustion chambers by a connecting tube. Each of the pulse combustors has a fundamental oscillation mode and one or more additional oscillation modes when operated in isolation. The connecting tube has a length corresponding to ¼ of the fundamental oscillation mode wavelength.Type: GrantFiled: March 18, 2016Date of Patent: February 14, 2023Assignee: UNIVERSITY OF MARYLANDInventor: Daanish Maqbool
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Patent number: 11434851Abstract: A pulse combustor system for efficiently operating a pulse combustor. The pulse combustor system includes the pulse combustor and a duct. The pulse combustor has a combustion chamber defining an internal space, a conduit having a first end in fluid communication with the internal space and a second end in fluid communication with an environment outside of the pulse combustor system, and a fuel injector configured to inject fuel into the internal space of the combustion chamber. The duct has two openings, with one opening disposed adjacent to the second end of the conduit. The pulse combustor system has an average operating frequency, and the duct has a length that is about one quarter of a wavelength corresponding to the average operating frequency. The pulse combustor and the duct each has a central longitudinal axis, and the two axes are substantially aligned.Type: GrantFiled: January 23, 2020Date of Patent: September 6, 2022Assignee: NORTH AMERICAN WAVE ENGINE CORPORATIONInventor: Daanish Maqbool
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Patent number: 10995703Abstract: A pulse combustor system for reducing noise and/or vibration levels. The system includes a pulse combustor including a combustion chamber, an inlet pipe, an exhaust pipe, and a first fuel injector for injecting fuel into the combustion chamber. The pulse combustor has a fundamental oscillation mode and one or more additional oscillation modes. The system includes at least one pressure sensor for measuring a pressure inside the fuel combustor and/or a at least one fluid velocity sensor for measuring fluid velocity at the inlet pipe or at the exhaust pipe. A controller adjusts a rate of fuel supply to the pulse combustor if the measured pressure and/or the measured velocity is above a predetermined threshold value to reduce excitation of the one or more additional oscillation modes.Type: GrantFiled: December 20, 2018Date of Patent: May 4, 2021Assignee: NORTH AMERICAN WAVE ENGINE CORPORATIONInventor: Daanish Maqbool
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Publication number: 20210108590Abstract: A system and method is disclosed for the start-up and control of pulsejet engines and this system includes an Electronic Fuel Injection (“EFI”) system that further includes one or more electrically controlled fuel injectors that can be selectively operated for start-up and control of such pulsejet engines. According to the system and method, the rate and/or pattern of fuel delivery to pulsejet engines can be varied not only by controlling the amount of time the fuel injectors are open versus closed to define a “duty cycle,” but also with the capability to selectively disable one or more fuel injectors in the programmed manner for start-up and control of such pulsejet engines.Type: ApplicationFiled: April 17, 2019Publication date: April 15, 2021Inventors: Daanish MAQBOOL, Nitay RAVIN, Carson MYERS
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Publication number: 20200256260Abstract: A system and method is disclosed for the start-up and control of pulsejet engines and this system includes an Electronic Fuel Injection (“EFI”) system that further includes one or more electrically controlled fuel injectors that can be selectively operated for start-up and control of such pulsejet engines. According to the system and method, the rate and/or pattern of fuel delivery to pulsejet engines can be varied not only by controlling the amount of time the fuel injectors are open versus closed to define a “duty cycle,” but also with the capability to selectively disable one or more fuel injectors in the programmed manner for start-up and control of such pulsejet engines.Type: ApplicationFiled: April 17, 2019Publication date: August 13, 2020Inventors: Daanish MAQBOOL, Nitay RAVIN, Carson MYERS
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Publication number: 20200158048Abstract: A pulse combustor system for efficiently operating a pulse combustor. The pulse combustor system includes the pulse combustor and a duct. The pulse combustor has a combustion chamber defining an internal space, a conduit having a first end in fluid communication with the internal space and a second end in fluid communication with an environment outside of the pulse combustor system, and a fuel injector configured to inject fuel into the internal space of the combustion chamber. The duct has two openings, with one opening disposed adjacent to the second end of the conduit. The pulse combustor system has an average operating frequency, and the duct has a length that is about one quarter of a wavelength corresponding to the average operating frequency. The pulse combustor and the duct each has a central longitudinal axis, and the two axes are substantially aligned.Type: ApplicationFiled: January 23, 2020Publication date: May 21, 2020Inventor: Daanish MAQBOOL
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Patent number: 10557438Abstract: A pulse combustor system for efficiently operating a pulse combustor. The pulse combustor system includes the pulse combustor and a duct. The pulse combustor has a combustion chamber defining an internal space, a conduit having a first end in fluid communication with the internal space and a second end in fluid communication with an environment outside of the pulse combustor system, and a fuel injector configured to inject fuel into the internal space of the combustion chamber. The duct has two openings, with one opening disposed adjacent to the second end of the conduit. The pulse combustor system has an average operating frequency, and the duct has a length that is about one quarter of a wavelength corresponding to the average operating frequency. The pulse combustor and the duct each has a central longitudinal axis, and the two axes are substantially aligned.Type: GrantFiled: December 16, 2016Date of Patent: February 11, 2020Assignee: NORTH AMERICAN WAVE ENGINE CORPORATIONInventor: Daanish Maqbool
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Publication number: 20200003158Abstract: A system and method is disclosed for improving the performance of pulsejet engines and of flight vehicles that incorporate pulsejet engines as a propulsion system. The system and method will decelerate the oncoming airstream to which a U-shaped pulsejet engine that is the propulsion system for a flight vehicle is exposed so that larger amounts of atmospheric air will be ingested into a rearward-facing inlet pipe for improved engine operation at low and high speeds/altitudes. The system and method provide for the recovery of the dynamic pressure of the incoming fresh airstream to raise the static pressure around the rearward facing inlet pipe to generate higher pressures and higher air density for improving the ingestion of air mass into the inlet pipe of the pulsejet engine thereby producing greater engine power and thrust.Type: ApplicationFiled: June 27, 2019Publication date: January 2, 2020Inventor: Daanish MAQBOOL
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Patent number: 10473058Abstract: A pulse combustor system for reducing noise and/or vibration levels. The system includes a pulse combustor including a combustion chamber, an inlet pipe, an exhaust pipe, and a first fuel injector for injecting fuel into the combustion chamber. The pulse combustor has a fundamental oscillation mode and one or more additional oscillation modes. The system includes at least one pressure sensor for measuring a pressure inside the fuel combustor and/or a at least one fluid velocity sensor for measuring fluid velocity at the inlet pipe or at the exhaust pipe. A controller adjusts a rate of fuel supply to the pulse combustor if the measured pressure and/or the measured velocity is above a predetermined threshold value to reduce excitation of the one or more additional oscillation modes.Type: GrantFiled: March 18, 2016Date of Patent: November 12, 2019Assignee: North American Wave Engine CorporationInventor: Daanish Maqbool
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Publication number: 20190128216Abstract: A pulse combustor system for reducing noise and/or vibration levels. The system includes a pulse combustor including a combustion chamber, an inlet pipe, an exhaust pipe, and a first fuel injector for injecting fuel into the combustion chamber. The pulse combustor has a fundamental oscillation mode and one or more additional oscillation modes. The system includes at least one pressure sensor for measuring a pressure inside the fuel combustor and/or a at least one fluid velocity sensor for measuring fluid velocity at the inlet pipe or at the exhaust pipe. A controller adjusts a rate of fuel supply to the pulse combustor if the measured pressure and/or the measured velocity is above a predetermined threshold value to reduce excitation of the one or more additional oscillation modes.Type: ApplicationFiled: December 20, 2018Publication date: May 2, 2019Inventor: Daanish MAQBOOL
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Publication number: 20180058319Abstract: A pulse combustor system for operating pulse combustors in anti-phase. The pulse combustor system includes two pulse combustors connected at their combustion chambers by a connecting tube. Each of the pulse combustors has a fundamental oscillation mode and one or more additional oscillation modes when operated in isolation. The connecting tube has a length corresponding to ¼ of the fundamental oscillation mode wavelength.Type: ApplicationFiled: March 18, 2016Publication date: March 1, 2018Applicant: University of Maryland, College ParkInventor: Daanish MAQBOOL
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Publication number: 20170175625Abstract: A pulse combustor system for efficiently operating a pulse combustor. The pulse combustor system includes the pulse combustor and a duct. The pulse combustor has a combustion chamber defining an internal space, a conduit having a first end in fluid communication with the internal space and a second end in fluid communication with an environment outside of the pulse combustor system, and a fuel injector configured to inject fuel into the internal space of the combustion chamber. The duct has two openings, with one opening disposed adjacent to the second end of the conduit. The pulse combustor system has an average operating frequency, and the duct has a length that is about one quarter of a wavelength corresponding to the average operating frequency. The pulse combustor and the duct each has a central longitudinal axis, and the two axes are substantially aligned.Type: ApplicationFiled: December 16, 2016Publication date: June 22, 2017Inventor: Daanish MAQBOOL
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Publication number: 20170082067Abstract: A pulse combustor system for reducing noise and/or vibration levels. The system includes a pulse combustor including a combustion chamber, an inlet pipe, an exhaust pipe, and a first fuel injector for injecting fuel into the combustion chamber. The pulse combustor has a fundamental oscillation mode and one or more additional oscillation modes. The system includes at least one pressure sensor for measuring a pressure inside the fuel combustor and/or a at least one fluid velocity sensor for measuring fluid velocity at the inlet pipe or at the exhaust pipe. A controller adjusts a rate of fuel supply to the pulse combustor if the measured pressure and/or the measured velocity is above a predetermined threshold value to reduce excitation of the one or more additional oscillation modes.Type: ApplicationFiled: March 18, 2016Publication date: March 23, 2017Inventor: Daanish MAQBOOL
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Patent number: D830281Type: GrantFiled: September 5, 2017Date of Patent: October 9, 2018Assignee: NORTH AMERICAN WAVE ENGINE CORPORATIONInventor: Daanish Maqbool