AIRBUS Water Pump

Last crawled date: 1 year, 10 months ago

The key points of this pump are Low Production Cost, Simplicity, Reliability and Size and a unique unbalanced closed cartridge solution adding self-priming features as well as increased pressure throughput. The assembly is designed as per the regulation of CS 29 amdt 3. Following CS 29 amdt 3 general criteria, all the material used in designing the parts are accepted by European Aviation Safety Agency. Additionally, no sharp edges are exposed, all the fasteners are locked and no self-locking fasteners are used. The assembly is able to withstand up to -20 to 120 degree

Technical Characteristics:
-Minimum 50,000hrs operation lifetime
-Steady and consistent flow
-Continuous working mode
-very quiet design, estimated 44DB
-Targeted cost of <$70
-Operating Substance: Water (Glycol and Iso-Propanol Up To 50%+).
- Operating Temperature: -20 to 120 C
- Max. Pressure Difference: 16 Bar (Head: 6ft) [with final geometry optimization likely >20Bar]
- Rated Flow Rate: 14 L/min (impeller design can be changed to target for 8-25L/min and increase max pressure @ 3000RPM]
- Blocked flow protection protection up to - 14 Bar (adjustable)
- Nominal Voltage: 28VDC regulated to 24V for compatibility of motors
- Motor Max Power: 30W
- Inlet Port: 10mm
- Outlet Port: 10mm
- Weight: 0.7 - 0.9 kg.
- Overall Volume: <1L
- Priming Capability: Self Priming
- Mechanical Time Constant: 0.2 Sec.