Fuel pump with electronic controlled pressure regulation and failure mitigation
OwnerGary Schultz, Conrad P. Lindberg +1inventors
InventorsGary Schultz, Conrad P. Lindberg, Charles Duffie
Life of this patent
Estimating the term…
Loading patent…
OwnerGary Schultz, Conrad P. Lindberg +1inventors
InventorsGary Schultz, Conrad P. Lindberg, Charles Duffie
Estimating the term…
A fuel pump system for aircraft includes an auxiliary fuel pump in-line with the primary pump, and an electric motor driving the auxiliary fuel pump at an operational motor speed. The system includes an electric control circuit (ECC) and a pressure sensor to regulate the speed of the electric motor based on the output pressure from the sensor to maintain a constant predetermined output pressure. The system may have additional fault mitigation circuitry configured to automatically switch from a processor-controlled to a fixed voltage as a source of power driving the electric motor at either a regulated speed or a constant fixed speed, respectively. The system may include a switch having user-selectable operational modes, including ECC-controlled mode and a high boost mode selectable if the ECC fails. In high boost mode, the ECC is bypassed to drive the electric motor at a fixed safe speed.
A fuel pump system for a vehicle, comprising:
A fuel pump system for a vehicle, comprising:
A fuel pump system for a vehicle, comprising:
A method of operating a fuel pump system for a vehicle, the fuel pump system including a primary fuel pump and an auxiliary fuel pump in-line with the primary fuel pump and fluidly connected to a fuel tank, and an electric motor for driving the auxiliary fuel pump, the method comprising:
A method of operating a fuel pump system for a vehicle, the fuel pump system including a primary fuel pump and an auxiliary fuel pump in-line with the primary fuel pump and fluidly connected to a fuel tank, and an electric motor for driving the auxiliary fuel pump, the method comprising:
A method of operating a fuel pump system for a vehicle, the fuel pump system including a primary fuel pump and an auxiliary fuel pump in-line with the primary fuel pump and fluidly connected to a fuel tank, and an electric motor for driving the auxiliary fuel pump, the method comprising:
Dependencies are inferred from the claim text.