dbill74
Mechanical
- Feb 26, 2009
- 538
I have come into a problem in which I need help in understanding and identifying problems and situations to avoid.
The problem: A military aircraft is to be parked in a new hanger and its pneumatic systems charged so crews can conduct training exercises in and on the plane. Normally the pneumatics systems are charged/powered by bleed air from the aircraft's engines in flight, with the plan sitting on the ground, this would be an obvious waste of fuel and create unwanted noise issues. Use of an AGE (Aircraft Ground Equipment) cart is not desirable with the aircraft being parked in a hanger, noise and exhaust issues. With these options 'off-the-table' client requested that the building's compressed air system be used to charge/power the pneumatic systems on the plane.
The hanger has been built and the designed and installed compressed air system are not meeting the aircraft's needs. My job now is to evaluate, validate and propose solutions.
My questions:
1) Is a bleed air requirement of 150 Lbm/min typical? Does this sound reasonable (units)?
2) What is the typical temperature range of bleed air as it comes off an aircraft's engine? From an AGE cart?
3) Do AGE carts providing bleed air to an aircraft typically a pre-cooler?
4) If answer to #3 is yes, what is typical temperature range bleed air is provided to the aircraft's pneumatic systems?
5) How critical is the temperature of the air entering the bleed air system of on aircraft?
In a typical building compressed air system (powering pneumatic tools), the air is compressed to 120 psig and provided in SCFM (Standard Cubic Feet per Minute). This is too high for an aircraft and I have been given a pressure requirement of 35 psig. I have made some calculations trying to convert the Lbm/min to SCFM, but as I've learned more about bleed air systems for aircraft, I've learned that my assumption are likely grossly wrong especially in regard to air temperatures.
Since this does involve military hardware, you'll excuse me if I'm hesitant to provide too many details and talk in more general terms.
The problem: A military aircraft is to be parked in a new hanger and its pneumatic systems charged so crews can conduct training exercises in and on the plane. Normally the pneumatics systems are charged/powered by bleed air from the aircraft's engines in flight, with the plan sitting on the ground, this would be an obvious waste of fuel and create unwanted noise issues. Use of an AGE (Aircraft Ground Equipment) cart is not desirable with the aircraft being parked in a hanger, noise and exhaust issues. With these options 'off-the-table' client requested that the building's compressed air system be used to charge/power the pneumatic systems on the plane.
The hanger has been built and the designed and installed compressed air system are not meeting the aircraft's needs. My job now is to evaluate, validate and propose solutions.
My questions:
1) Is a bleed air requirement of 150 Lbm/min typical? Does this sound reasonable (units)?
2) What is the typical temperature range of bleed air as it comes off an aircraft's engine? From an AGE cart?
3) Do AGE carts providing bleed air to an aircraft typically a pre-cooler?
4) If answer to #3 is yes, what is typical temperature range bleed air is provided to the aircraft's pneumatic systems?
5) How critical is the temperature of the air entering the bleed air system of on aircraft?
In a typical building compressed air system (powering pneumatic tools), the air is compressed to 120 psig and provided in SCFM (Standard Cubic Feet per Minute). This is too high for an aircraft and I have been given a pressure requirement of 35 psig. I have made some calculations trying to convert the Lbm/min to SCFM, but as I've learned more about bleed air systems for aircraft, I've learned that my assumption are likely grossly wrong especially in regard to air temperatures.
Since this does involve military hardware, you'll excuse me if I'm hesitant to provide too many details and talk in more general terms.