I am creating a home flight simulation expansion of the Boeing 747 classic series and I have come across an interesting and hard to answer question involving the ductwork of the airplane.
The 747 uses bleed air extracted from the engines/APU or an external ground source to provide air to the various pneumatically operated devices on the airplane (L.E. flaps, air conditioning, reversers, etc.).
On the flight engineer's panel is a very important gauge showing the overall pressure in the duct lines to all of these users. The 747 has a singular circular duct, approximately 6 inches in diameter, to which all sources and users of pneumatic air are connected.
How can I calculate (or closely approximate) the pressure, in psi, in the air ducts for any given set of inputs and outputs? Here is what I know about the system:
EDIT: An important note is that, as far as I am aware, the system is not "demand based" like a lot of newer aircraft. The system supplies a constant amount of pressure to the system based either on APU or Engine RPM.
- Highly compressed air is taken from the engines and regulated to a maximum of approximate 45-47 psi before entering the duct.
- The pressure from the engines can be lower than this 45-47 psi figure, for example, at low thrust with the high stage bleeds open, it can be as low as 25-35 psi.
- Each engine can supply up to 150 ppm of air.
- The APU can supply 660 ppm at no load, 565 ppm maximum load.
- Air conditioning packs use 200 ppm each.
- The duct has a leak rate between 290-390 CFM at 45 psi.
- Other needs of the pneumatic system can vary their usage.
Thanks!