Patents by Inventor Jaspal Rawat
Jaspal Rawat 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: 11794923Abstract: An aircraft refueling system (10) includes a master controller (12), a fleet controller (14) in communication with the master controller, a platform controller (18) in communication with the fleet controller, and a fuel control system (16) in communication with the platform controller. Embodiments of an aircraft refueling system may include a primary pressure controller (20), a secondary pressure controller (22), a programmable logic controller (24), and a data logger controller (26). The master controller may be configured to receive and analyze data from at least one of the fleet controller, the platform controller, and the fuel control system; and to modify operational parameters or upgrade the fuel control system based at least in part on the analysis of received data.Type: GrantFiled: September 20, 2019Date of Patent: October 24, 2023Assignee: Eaton Intelligent Power LimitedInventors: Abhijit A. Bodkhe, Ashok K. Vishwakarma, Jaspal Rawat, Steven Hum, Parag More, Chandrashekhar S. Nehete, Robert L. Sbonek, Jeffrey M. Laing, Taruna Khandelwal, Vivek Agarwal
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Patent number: 11597536Abstract: A system for monitoring components of an aircraft ground refueling system includes a first computing device and a second computing device hosting a data base. The first computing device is caused to read a component identification tag secured to a component of an aircraft ground refueling system; the tag contains a unique component identifier. The first computing device transmits the component identifier to the second computing device which verifies that the component identifier is active in the data. The first computer, responsive to the verification, displays a user interface to receive data representative of an operational status of the component and transmits the operational status. The second computing device stores the data in the database to create an operational history of the component. The second computing device analyzes the history of the data to determine a characteristic operational parameter of the component of the aircraft ground refueling system.Type: GrantFiled: August 21, 2020Date of Patent: March 7, 2023Assignee: Eaton Intelligent Power LimitedInventors: Parag More, Jaspal Rawat, Chandrashekhar Nehete
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Publication number: 20220327500Abstract: An aircraft ground refueling management system of the present disclosure utilizes various components already existing in an aircraft ground refueling vehicle to characterize and track, in real time, events of an aircraft refueling operation. The components include a fuel meter, a fuel delivery deadman sensor, a fuel nozzle sensor and a ground refueling vehicle brake sensor. Data from these components in combination with data provided by a mobile computing device that is integral to the refueling operation provide the data points to determine the amount of time elapsed for each event of the refueling operation. Knowledge of each event of the refueling operation provides the opportunity for identifying where time spent can be reduced.Type: ApplicationFiled: April 6, 2022Publication date: October 13, 2022Inventors: Aditee BAPAT, Amit JOSHI, Amit BADDI, Parag MORE, Bhupesh JINGAR, Jaspal RAWAT
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Patent number: 11414206Abstract: A fluid system includes a controller, a control valve, and a fluid manifold. At least one solenoid may be connected to the fluid manifold, the control valve, and/or the controller. A first pressure sensor may be in fluid communication with an output of the control valve. A second pressure sensor may be in fluid communication with the fluid manifold. The controller may be configured to control operation of the control valve via the at least one solenoid according to a first fluid pressure obtained via the first pressure sensor and according to a second fluid pressure obtained via the second pressure sensor.Type: GrantFiled: October 16, 2019Date of Patent: August 16, 2022Assignee: EATON INTELLIGENT POWER LIMITEDInventors: Gilbert P. Freeth, Parag More, Robert L. Sbonek, Jaspal Rawat, Harshad P. Pawale, Chandrashekhar S. Nehete, Vikas Pandey, Balakrishnan Arumugam, Rajan Y. Tribhuvan, Bhupesh Jingar, Rohit Gupta
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Publication number: 20220048644Abstract: An aircraft refueling system (10) includes a master controller (12), a fleet controller (14) in communication with the master controller, a platform controller (18) in communication with the fleet controller, and a fuel control system (16) in communication with the platform controller. Embodiments of an aircraft refueling system may include a primary pressure controller (20), a secondary pressure controller (22), a programmable logic controller (24), and a data logger controller (26). The master controller may be configured to receive and analyze data from at least one of the fleet controller, the platform controller, and the fuel control system; and to modify operational parameters or upgrade the fuel control system based at least in part on the analysis of received data.Type: ApplicationFiled: September 20, 2019Publication date: February 17, 2022Inventors: Abhijit A. Bodkhe, Ashok K. Vishwakarma, Jaspal Rawat, Steven Hum, Parag More, Chandrashekhar S. Nehete, Robert L. Sbonek, Jeffrey M. Laing, Taruna Khandelwal, Vivek Agarwal
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Publication number: 20210053700Abstract: A system for monitoring components of an aircraft ground refueling system includes a first computing device and a second computing device hosting a data base. The first computing device is caused to read a component identification tag secured to a component of an aircraft ground refueling system; the tag contains a unique component identifier. The first computing device transmits the component identifier to the second computing device which verifies that the component identifier is active in the data. The first computer, responsive to the verification, displays a user interface to receive data representative of an operational status of the component and transmits the operational status. The second computing device stores the data in the database to create an operational history of the component. The second computing device analyzes the history of the data to determine a characteristic operational parameter of the component of the aircraft ground refueling system.Type: ApplicationFiled: August 21, 2020Publication date: February 25, 2021Inventors: Parag MORE, Jaspal RAWAT, Chandrashekhar NEHETE
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Publication number: 20200047909Abstract: A fluid system includes a controller, a control valve, and a fluid manifold. At least one solenoid may be connected to the fluid manifold, the control valve, and/or the controller. A first pressure sensor may be in fluid communication with an output of the control valve. A second pressure sensor may be in fluid communication with the fluid manifold. The controller may be configured to control operation of the control valve via the at least one solenoid according to a first fluid pressure obtained via the first pressure sensor and according to a second fluid pressure obtained via the second pressure sensor.Type: ApplicationFiled: October 16, 2019Publication date: February 13, 2020Inventors: Gilbert P. Freeth, Parag More, Robert L. Sbonek, Jaspal Rawat, Harshad P. Pawale, Chandrashekhar S. Nehete, Vikas Pandey, Balakrishnan Arumugam, Rajan Y. Tribhuvan, Bhupesh Jingar, Rohit Gupta
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Patent number: 10532821Abstract: A fluid system includes a controller, a control valve, and a fluid manifold. A first solenoid may be connected to the fluid manifold, the control valve, and/or the controller. A second solenoid may be connected to the fluid manifold, the control valve, and/or the controller. A first pressure sensor may be in fluid communication with an output of the control valve. A second pressure sensor may be in fluid communication with the fluid manifold. The controller may be configured to control operation of the control valve via the first solenoid and the second solenoid according to a first fluid pressure obtained via the first pressure sensor and according to a second fluid pressure obtained via the second pressure sensor.Type: GrantFiled: November 3, 2017Date of Patent: January 14, 2020Assignee: Eaton Intelligent Power LimitedInventors: Gilbert P. Freeth, Parag More, Robert Sbonek, Jaspal Rawat, Harshad P. Pawale, Chandrashekhar Nehete, Vikas Pandey, Balakrishnan Arumugam, Rajan Y. Tribhuvan, Bhupesh Jingar, Rohit Gupta
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Publication number: 20180127109Abstract: A fluid system includes a controller, a control valve, and a fluid manifold. A first solenoid may be connected to the fluid manifold, the control valve, and/or the controller. A second solenoid may be connected to the fluid manifold, the control valve, and/or the controller. A first pressure sensor may be in fluid communication with an output of the control valve. A second pressure sensor may be in fluid communication with the fluid manifold. The controller may be configured to control operation of the control valve via the first solenoid and the second solenoid according to a first fluid pressure obtained via the first pressure sensor and according to a second fluid pressure obtained via the second pressure sensor.Type: ApplicationFiled: November 3, 2017Publication date: May 10, 2018Inventors: Gilbert P. Freeth, Parag More, Robert Sbonek, Jaspal Rawat, Harshad P. Pawale, Chandrashekhar Nehete, Vikas Pandey, Balakrishnan Arumugam, Rajan Y. Tribhuvan, Bhupesh Jingar, Rohit Gupta