#B64D37/34

LIQUID-HYDROGEN FUEL SYSTEM FOR AN AIRCRAFT

A fuel system having a hydrogen fuel tank for fueling a fuel feed and propulsion system. The fuel system having a jet pump within the hydrogen fuel tank, at least one primary pump receiving fuel from …

DRIVE·Mar 12·1 min read

B64D37/34 Eaton Intelligent Power Limited

METHOD AND APPARATUS FOR CONTROLLING FUEL FLOW INTO AN AIRCRAFT ENGINE

Based upon measured resistances, a first delta curve and second delta curve are selected. A first fuel valve position (FVP) is received from a first position sensor (102), and the first FVP is applied…

DRIVE·Jul 16·1 min read

B64D37/34 GE AVIO SRL [IT]

CENTRIFUGAL FUEL PUMP ICE PREVENTION

A fuel pump arrangement including a housing and an impeller located within the housing configured for receiving cold fuel through an inlet of the housing, wherein the impeller includes a series of van…

DRIVE·Oct 8·1 min read

B64D37/34 Hamilton Sundstrand Corporation

SCREEN AND SCREEN ELEMENTS FOR FUEL SYSTEMS

A screen element for a fuel system includes a first screen and a second screen. The first screen defines a first aperture and the second screen defines a second aperture. The first aperture and the se…

DRIVE·Feb 4·1 min read

B64D37/34 Hamilton Sundstrand Corporation