DT56
Posts: 156
Joined: 3/15/2005 From: Lucedale,
MS, USA Status: offline
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The reason this wouldn't work is well known to full scale pilots. Full scale helicopters have a very limited range of collective pitch travel compared to RC models. There are definite high and low RPM limits for the rotor system, with the low end being the greatest concern. Lower rotor RPM causes the aircraft to descend due to loss of lift. Adding collective pitch to compensate causes an increase in drag at the blade, further decreasing RPM. Once reaching a certain point, the blade stalls and drag exceeds the power available from the engine, with RPM decreasing even further. There is insufficient negative collective pitch to allow a recovery of RPM and the rotor speed continues to decay until the aircraft augers in. Since helicopters are usually flown fairly low, most crash before RPM reduces to the point of blade structural failure. In a helicopter with a low inertia rotor system, such as the Robinson R22, there are flight conditions in which full down collective pitch is required within 2 seconds of an engine failure to prevent reaching an unrecoverable low rotor RPM. No surprise that maintaining rotor RPM is the most important lesson learned in flight training! DT56
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