JavaScript Menu, DHTML Menu Powered By Milonic
Technical Support
CPU Flow Calculator
Input:
This calculator allows you to input the Static Pressure, Differential Pressure, and Temperature from the gauges on a Tronair Cabin Pressurization Unit and the resultant output will be the flow and mass flows. This is provided as an alternative method to using the curves provided in the operation and technical manual.

MODELS: 15-7600-1000, 15-7602-1000, 15-7603-1000, 15*7603-1000 (* = letters A through K)
 
Aircraft Manufacturer:   
Aircraft Model:   
Aircraft Registration #:   
 
System Pressure from Pressure Gauge (NOT cabin pressure):      psi (0-15 psi)
Differential Pressure from Magnahelic or Capsuhelic Pressure Gauge:      inWC (0-20 inches of water column)
Temperature from Temperature Gauge:      F (50-300 degrees F)

Results:
Flow in SCFM: 
Mass Flow in lb/hr: 
Mass Flow in lb/min: 
 
DISCLAIMER: Tronair, Inc. not responsible for incorrect use of this "CPU Flow Calculator", and subsequent incorrect values that may result.
REVISION: 5/17/2006