The invention discloses a tilting rotorcraft tilting device and method based on a linear steering engine, and relates to the technical field of aircraft power
system control. The tilting device comprises an electric linear steering engine, a tilting rib plate and a linear steering engine connecting rod; the rear end of the electric linear steering engine is hinged to one end of the tilting rib plate, a telescopic rod on the front portion of the electric linear steering engine is hinged to one end of the linear steering engine connecting rod, the other end of the linear steering engine connecting rod is fixedly provided with a tilting shaft, the tilting shaft is hinged to the other end of the tilting rib plate, and the tilting shaft is used for installing a rotor cabin. The telescopic rod of the electric linear steering engine drives the linear steering engine connecting rod to drive the tilting shaft fixedly arranged at the
tail end of the connecting rod to rotate, so that the rotor cabin is driven to tilt, and flight
mode switching is achieved. The device adopts a simple hinged transmission structure to realize
power transmission, has the characteristics of compact structure, small transmission clearance and simplicity and convenience in control, and is particularly suitable for the requirements of light weight and low cost of small tilting rotorcrafts.