Fuel System components for Aircraft Application

Fuel System components for Aircraft Application

Project Description

1      Differential Pressure Switch
2      Electric Re-fuelling Valve
3      Float Valve
4      Flow Transmitter with Flow Straightner
5      Fuel Shut off Cock with Thermal Relief
6      Low Pressure Fuel Shut off Cock dia 25mm
7      Motorized Fuel Transfer Valve
8      Transfer Cum Refueling Valve
9      Refuel Transfer cum stop air valve

Documents

Please to access project documents.

Project Awarded

FAQs

Can an educational institution participate directly in this project ?

Answer – No. An educational institution can provide R & D support for a company or industry executing the project. Under such circumstances also, the involvement of an educational or a research institution cannot exceed 40%.

How will I receive the funding ?

Funding under this scheme is facilitated either as a grant – in– aid [for reimbursements only] or as an advance against bank guarantee. You may refer to the SOP Document in the “About the Scheme” section of this website.