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公开(公告)号：US20200047909A1
公开(公告)日：2020-02-13
申请号：US16654374
申请日：2019-10-16
Applicant: Eaton Intelligent Power Limited
Inventor： 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
Abstract: 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.
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公开(公告)号：US20180229853A1
公开(公告)日：2018-08-16
申请号：US15953751
申请日：2018-04-16
Applicant: Eaton Intelligent Power Limited
Inventor： Subrata Sarkar , Alan Massey , Kailash Golecha , Prasant Jha , Surbhi Kohli , Amit Kalmegh , Vismay Walle , Chandrashekhar S. Nehete
CPC classification number: B64D37/32 , A62C3/065 , A62C3/08 , B01D53/346 , B01D53/46 , B01D53/81 , B01D2253/1122 , B01D2257/104 , B64D13/08 , B64D2013/0659 , B65D90/44
Abstract: An aircraft fuel tank inerting system includes an inlet, an oxygen absorption unit, and a vent to discharge oxygen from the system. The inlet may be configured to be in fluid communication with a ullage of a fuel tank. In embodiments, the oxygen absorption unit is in communication with the inlet and includes a chamber, a temperature reversible oxygen absorption medium within said chamber, and a temperature controller for selectively heating or cooling the medium. The reversible oxygen absorption medium may be a medium which absorbs oxygen by chemisorption.
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公开(公告)号：US11794923B2
公开(公告)日：2023-10-24
申请号：US17276559
申请日：2019-09-20
Applicant: Eaton Intelligent Power Limited
Inventor： 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
CPC classification number: B64F1/28 , B64D37/16 , G05B19/052 , G05B23/0232 , B67D7/0401
Abstract: 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.
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公开(公告)号：US11414206B2
公开(公告)日：2022-08-16
申请号：US16654374
申请日：2019-10-16
Applicant: Eaton Intelligent Power Limited
Inventor： 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
Abstract: 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.
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