Eaton Intelligent Power Limited

Chandrashekhar S Nehete

Parag More

Jaspal Rawat

Robert L Sbonek

Gilbert Peter Freeth

Harshad P Pawale

Rohit Gupta

Bhupesh Jingar

Vikas Pandey

Balakrishnan Arumugam

Rajan Y Tribhuvan

Subrata Sarkar

Alan Ernest Massey

Ashok K Vishwakarma

Amit Kalmegh

Vismay Walle

Abhijit A Bodkhe

Vivek Agarwal

Taruna Khandelwal

Jeffrey M Laing

Steven Hum

Kailash Golecha

Prasant Jha

Surbhi Kohli

An aircraft refueling system () includes a master controller (), a fleet controller () in communication with the master controller, a platform controller () in communication with the fleet controller, and a fuel control system () in communication with the platform controller. Embodiments of an aircraft refueling system may include a primary pressure controller (), a secondary pressure controller (), a programmable logic controller (), and a data logger controller (). 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.

Aircraft refueling system

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.

Asset utilization management for aircraft ground refueling equipment

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.

Fluid system having a control valve and a monitoring system therefor

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.

Fuel tank inerting system

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.

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Pune, India

Chandrashekhar S Nehete