ENGIFAR
Aerospace
- Jan 20, 2017
- 8
Currently designing a system that requires inflating multiple airbags during end of flight recovery. The current approach being taken is to use stored gas within a high pressure cylinder and a solenoid valve to control flow. A pressure switch would monitor the pressure level and activate the solenoids when required.
I am aware that this approach introduces many challenges that must be overcome. I will list a couple that I am aware of below.
-possible leakage through solenoid valves during high accel flight maneuvers.
-working with high pressure and temperature differentials pose multiple concerns. Air from cylinder (~5000 psi) enter[pre][/pre]ing bags will be extremely cold. Gas heating will cause expansion during descent. Changing atmospheric pressure (inflation anywhere from 10k ft to sea level and maintaining pressure throughout descent) presents a moving gauge pressure target (~3 psig, bags passively vent at ~7 psig bags must also fillin a reasonable amount of time <15 seconds)
-initial extremely high flow rate that declines as vessel empties
-decrease in temperature gas is filled at will cause a decrease in available pressure at altitude in cold environment. (Soaks at up to 40k ft long enough to reach equilibrium)
-safety issues filling cylinders to high pressures
-any residual gas in airbags will expand at altitude and possibly cause premature inflation (very bad-worst case failure, emphasizes need for zero leakage solenoid.
Basically, my question is does anyone has any experience with a similar system? Would another approach be more feasible? (gas generation, blower, other ideas?) Any tips to overcome the challenges with a stored gas system or any complications that I am overlooking? Suggestions for a solenoid valve that won't leak (N2) and can withstand the high pressure for an extended amount of time? As a cherry on top of these hurdles, the system must be low cost both initially and per flight.
Thanks in advance for anything you can offer. This is not my area of expertise and information is hard to come by regarding an application such as this.
I am aware that this approach introduces many challenges that must be overcome. I will list a couple that I am aware of below.
-possible leakage through solenoid valves during high accel flight maneuvers.
-working with high pressure and temperature differentials pose multiple concerns. Air from cylinder (~5000 psi) enter[pre][/pre]ing bags will be extremely cold. Gas heating will cause expansion during descent. Changing atmospheric pressure (inflation anywhere from 10k ft to sea level and maintaining pressure throughout descent) presents a moving gauge pressure target (~3 psig, bags passively vent at ~7 psig bags must also fillin a reasonable amount of time <15 seconds)
-initial extremely high flow rate that declines as vessel empties
-decrease in temperature gas is filled at will cause a decrease in available pressure at altitude in cold environment. (Soaks at up to 40k ft long enough to reach equilibrium)
-safety issues filling cylinders to high pressures
-any residual gas in airbags will expand at altitude and possibly cause premature inflation (very bad-worst case failure, emphasizes need for zero leakage solenoid.
Basically, my question is does anyone has any experience with a similar system? Would another approach be more feasible? (gas generation, blower, other ideas?) Any tips to overcome the challenges with a stored gas system or any complications that I am overlooking? Suggestions for a solenoid valve that won't leak (N2) and can withstand the high pressure for an extended amount of time? As a cherry on top of these hurdles, the system must be low cost both initially and per flight.
Thanks in advance for anything you can offer. This is not my area of expertise and information is hard to come by regarding an application such as this.