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Mike Rapoport wrote:
"John Gilmer" wrote in message ... "Mike Rapoport" wrote in message rthlink.net... "Ralph Nesbitt" wrote in message odigy.com... At altitude A/C cabins are like a pressure vessel. A/C cabins are pressurized to maintain ~ 12 PSI Gauge, ~ the same as normal atmospheric pressure @ 11,000' ASL, in the cabin irrespective of altitude above 11,000' ASL. Ralph Nesbitt Professional FD/CFR/ARFF Type No, the cabin is not at a constant preasure above 11,000' (and the number that you are looking for is 8,000') unless the rate controller is set to a rate greater than the climb rate of the aircraft (which is never done). If what you say were true then the cabin altitude would not climb with the airplane above 11,000' (8,000') which it clearly does. If you doubt this, go buy an altimeter watch and see for yourself. Or you could buy a pressurized airplane. OK, I'll bite. Just how does the psia in the cabin track the psia "ambient." What are you asking? Mike The comment was made that the pressure inside the cabin is not necessarily constant above a certain altitude, unless certain cabin rate settings were made, possibly leading to confusion over cabin altitude vs. actual aircraft altitude. It is a simplification to say that cabin altitude is constant above a given aircraft altitude. In fact, the cabin altitude will move toward a certain altitude (8,000' in most cases, it seems) as set by the cabin pressurization controller (or any of its several other names), IF the outside pressure altitude is higher than the cabin altitude. That is to say that if you take off from sea level and climb to 10,000', the cabin altitude will steadily climb, at a rate set by the cabin pressure controller, toward 8,000'. If you were to level off at 5,000' and stay there long enough for the cabin pressure to catch up, it will maintain 5,000' until the aircraft begins to climb again, at which it will again climb at the set rate until it reaches either the set cabin altitude or the actual ambient pressure altitude. So the cabin pressure can be below 8,000' (or whatever the set altitude is) at actual altitudes above the set altitude, but will be moving toward the set altitude in that case. Note that cabin altitude cannot be maintained ABOVE the actual pressure altitude, as air is continually pumped into the cabin by the bleed air system, and is let out (or leaks out) to maintain the set altitude or rate of change. If you descend quickly enough, you may temporarily get a cabin altitude above ambient, but air will not exit the aircraft (outside pressure would prevent any air from leaving through the outflow valve, and in some cases a safety valve may automatically open to allow air to flow INTO the aircraft, relieving the negative pressure differential) and air flowing into the cabin will tend to increase pressure rapidly until equilibrium is reached. Having attained the pressure set by the controller, the system will typically attempt to maintain that pressure altitude until it is reset to another altitude, although it may not always be able to. Descents with low engine power may result in not airflow into the cabin to match the outflow, due either to the controller not closing the outflow valve fast or far enough, or due to leaks in the airframe letting more air out than the system can pump in. Also, the cabin controller will typically not allow a pressure differential above a certain limit- too much pressure differential stresses the fuselage. The controller will open the outflow valve to maintain that maximum differential, so at that point, if the aircraft climbs then the cabin altitude will increase as well. Prior to or during the descent, the cabin pressure controller would normally be set to the field pressure altitude (which is normally below the cabin altitude during cruise, but this may not always be the case). The controller will then begin to decrease the cabin altitude, again at the set rate. This prevents rapid pressure changes as the aircraft descends through the cruise cabin altitude and is more easier on the passengers and crew. Long and convoluted enough for you? Mike EC-130H Compass Call "In Jam, no one can hear you scream" |
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