Aerocraft steering engine non-rubber deviation load torque following mechanism

The invention relates to a steering engine non-rubber deviation load torque following mechanism. A torsion rod spring locating slider in the prior art is improved to 'a non-rubber deviation load torque following mechanism' so that the steering engine non-rubber deviation load torque following mechanism can follow aerocraft steering engine load torque caused by non-rubber deviation factors such asa flight attack angle, an angle of slideslip and autorotation speed of aerocraft and the like in a flight simulation experiment. The non-rubber deviation load torque following mechanism converts non-rubber deviation load torque into a torque valent weight angle according to the current load, follows in real time by a position servosystem, thus achieving the purpose of following the aerocraft steering engine load torque caused by non-rubber deviation factors such as a flight attack angle, an angle of slideslip and autorotation speed of aerocraft and the like and causing 'a simulation load device' to be capable of bette