Eaton Intelligent Power Limited

Ashok K Vishwakarma

Parag More

Abhijit A Bodkhe

Jaspal Rawat

Chandrashekhar S Nehete

Robert L Sbonek

Pradeep Biradar

Taruna Khandelwal

Jeffrey M Laing

Steven Hum

Hemant P Deore

Divya Juneja

Andres Olmedo

Swastik Balshiram Davkhar

Michael Leo Madlangbayan

Vivek Agarwal

Pushkar Prasad Gijare

The present disclosure relates to an improved pilot valve assembly for a hydrant pit valve. The pilot valve assembly includes a poppet that is movable between an open position and a closed position. The poppet has a molded seal with an interlock feature to hold the seal rigidly. The pilot valve assembly also includes a manually reset mechanism. The reset mechanism can be horizontally positioned and can function to reset the pilot actuator for the next refueling operation. A lanyard can be connected to the poppet to be used a deactuation mechanism.

Pilot valve assembly

The present disclosure relates to a valve assembly for controlling flow. The valve body has an inlet end and an outlet end. A piston is positioned within the valve body and is movable between an open position to open the valve body and a closed position to close the valve body. A spring is mounted between the piston and a spring adjustment member. A portion of the spring adjustment member is accessible through the inlet end of the valve body so as to be engageable by a tool to facilitate rotation of the spring adjustment member to vary compression of the spring to set a spring pressure rating.

Variable pressure control valve

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 coupling assembly () may include a first member () and a second member (), a release sleeve () movably connected to the first member, a retainer sleeve (), and a spring (). The second member includes a second member flange (). The spring may be configured to apply a spring force to the retainer sleeve. The spring force may biases the retainer sleeve into a positive engagement with the second member flange.

Coupling assembly with vibration lock

A temperature monitoring system includes an enclosure, an external temperature sensor, and an internal temperature sensor. The enclosure may be explosion-proof, and may include a controller and an internal display disposed within the enclosure. The external temperature sensor may be configured to detect an outside temperature, and the internal temperature sensor may be configured to detect a temperature inside the enclosure. Upon the external temperature sensor and/or the internal temperature sensor detecting a temperature that meets or exceeds a set or specified value or limit, the system may be configured to implement an action or order. In an embodiment of the system, the system may be configured to stop fueling in the event that the external temperature sensor and/or the interior temperature sensor detect a temperature that meets or exceeds a certain temperature.

Intelligent temperature monitoring system and method therefor

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Maharashtra, India

Ashok K Vishwakarma