SUMMARY
Motive flow in an aircraft fuel system refers to the use of fuel to pump fuel, primarily for transferring fuel between tanks. Two main types of motive flow pumps are utilized: ejector pumps, which employ the venturi effect, and turbine pumps, which use high-pressure motive flow to drive a turbine for fuel movement. These systems are lightweight and simpler than mechanically driven transfer pumps, allowing for efficient cycling of fuel that is not consumed back into the tanks.
PREREQUISITES
- Understanding of aircraft fuel systems
- Knowledge of ejector and turbine pump mechanisms
- Familiarity with the venturi effect
- Basic principles of fluid dynamics
NEXT STEPS
- Research the operation of ejector pumps in aviation fuel systems
- Explore turbine pump technology and its applications in aircraft
- Study the venturi effect and its implications in fluid transfer
- Investigate the advantages of motive flow systems over mechanical pumps
USEFUL FOR
Aerospace engineers, aircraft maintenance technicians, and anyone involved in the design or maintenance of aircraft fuel systems will benefit from this discussion.