The pump functions as a self-contained, variable-speed, electric motor-driven cooling pump that flows fluid through aircraft cooling systems. It is a completely sealed unit without drains or sumps. The unit is pad mounted and communicates directly with aircraft electronic controls. The pump can be used in single- or dual-channel operating mode for redundant-system requirements.
APPLICATIONS:
The pump can be used in thermal cooling systems for commercial aircraft including galley cooling, cargo cooling, and electronics cooling.
FEATURES AND ATTRIBUTES:
Adds redundant pumping function for cooling applications. High-reliability impeller design. Added features and components include:
• Electric motor and speed controller
• Cooling pump (impeller)
• Pump flapper valve for backflow prevention
OPTIONAL FEATURES:
• Input power: 3 phase 270 VDC sinusoidal motor
