Eaton Corporation

Eaton Intelligent Power Limited

Vismay Walle

Subrata Sarkar

Alan Ernest Massey

Chandrashekhar S Nehete

Harshad P Pawale

Amit Kalmegh

Anh Hung Vu

Kailash Golecha

Prasant Jha

Surbhi Kohli

Sandip Gaikwad

Sahebrao Tekale

Amit Klamegh

Chandrashekhar Sadashiv Nehete

Anh Vu

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 pressure relief valve assembly includes a housing, a diaphragm assembly separating the housing into a sensing pressure section and a tank pressure section, the sensing pressure section configured to sense both atmospheric pressure and the pressure in the tank pressure section and the tank pressure section is configured to only sense the pressure in the tank pressure section, an orifice disposed between the sensing pressure section and the tank pressure section allowing fluid to flow in through the orifice when the pressure in the sensing pressure section is less than the pressure in the tank pressure section fluid to flow out through the orifice when the pressure in the sensing pressure section is greater than the pressure in the tank pressure section.

Pressure relief valve assembly

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Pune, India

Vismay Walle