Abstract: A test stand and method for calibrating aircraft fuel components which utilizes a fuel look-alike with a flash point above 180° F. and a viscosity below 2.8. Furthermore, the look-alike has the specific gravity and dielectric constant similar to that of aircraft fuel. An operator sets input parameters and adjusts the components until the desired output parameters are attained.
Type:
Grant
Filed:
June 15, 1998
Date of Patent:
July 17, 2001
Assignee:
The United States of America as represented by the Secretary
of the Navy