Hi guys,I thought I"d start this topic to see where it goes.It seems to me that most gyroplanes in our fleet are compromised because although most can be landed very short, almost all have to take off very long.While a powerful pre-rotator eliminates the need for taxying up and down milking the rotor up to speed, and also reduces the distance required to match the accelerating rotor with the increasing airspeed during the first part of the takeoff roll, a substantial distance is still nevertheless often necessary before the gyro flies itself off.I"m not talking here about jump-start gyros, because coming from the helicopter world where every pilot subconsciously levels the rotor before the skids finally lift off, the history of jump-starting in gyros is littered with accidents caused by the jump-start process occurring while the rotor wasn"t absolutely level, and where the jump start goes wrong by having a significant roll or pitch component, leading at best to an extremely untidy liftoff through to at worst a partial tipover and usual rotor strike.And, I write this fully aware that for gyroplanes, airspeed is life. In other words, our fixed pitch autorotating rotors just can"t perform like a powered helicopter rotor where more pitch with more power is pulled in to achieve better climb performance. A fixed pitch autorotating rotor achieves performance increases (ie, higher climb rates) solely by increased translational lift from increasing airspeed, with maximum climb rates obviously attained at airspeeds where the engine can maintain gyro airspeeds that allow the rotor to entrain more air per second without a lot of that engine power being robbed by airframe parasite drag.What I"m talking about with this thread is a prerotator configuration where the fixed-pitch gyro rotor can be taken to a 10% to 20% overspeed and the takeoff roll then commenced. The overspeed method has the benefit of having the rotor absolutely level, or at least the rotor attitude under the very precise control of the pilot (in contrast to a jump situation).A gyro with an oversped rotor will still need to roll sufficiently for it to acquire 25+ to 30+ knots airspeed before it begins to climb. And, to reliably climb at such risky low airspeeds will require about 8 pounds gross weight per installed horsepower. Even so, climbing at around 30 knots still has substantial risks in case of engine failure, where the emergency nose-down manoeuvre will further reduce rotor rpm, probably leaving not enough energy to flare reliably.So, what I"m inviting here is comment on this sort of concept
1) Stationary into, say a 10 knot wind;(2) Rotor oversped by 20% (where flight rpm is say, 360, so we overspeed to 432);(3) Brakes off, takeoff roll commenced; (4) 30 knots indicated - hopefully gyro feels like it"s ready to fly itself off;(5) initial climbout to perhaps 50 feet with IAS holding at low to mid 30"s (mindful of the danger of having not enough rotor inertia to comfortably flare if engine quits); (6) less risky part 2 of the climbout where IAS is let go to mid 40s+ transitioning slowly up to 50; and(7) operations normal after that - 50 - 60 knots cruiseThe initial climbout I"m describing will be right on the boundary of the height-velocity curve, and very likely within the height velocity curve for a heavier gyro.The whole purpose of this concept is to balance the benefit of a short takeoff against the risk of being on the edge of, or behind the power curve for a number of seconds. It would be nice to be able to reliably undertake such a manoeuvre because if the technique was mastered on normal runways or open paddocks, then it would influence the types of landing areas that one could select in the knowledge that you could reliably do a short take off (STO) out of the site.Has anybody got any experience with "rotor overspeeding" from pre-rotation?Has anybody got any experience at transitioning an oversped rotor into normal autorotative flight?Has anybody got experience of engine failure during a steeper than normal initial climbout under full power?What effect does very high installed horsepower have, given that it is likely to tempt the pilot to climb out steeply (at risk if the donk quits?)Does anyone know how much a rotor will slow from normal cruise rpm during a high-power "hanging off the prop" steep attitude climb?Cheers,Mark ReganMelbourne
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