The present invention provides a
power apparatus for an aircraft. The apparatus comprises a base, a drive source and a rotation
propeller, wherein the drive source drives the rotation
propeller to rotate. The rotation
propeller comprises a rotation propeller shaft and a propeller blade
assembly. The rotation propeller shaft forms a rotatable connection with the drive source. The propeller blade
assembly is provided with a propeller blade shaft, wherein the propeller blade shaft is perpendicular to the rotation propeller shaft, and can rotate around the axial line of the propeller blade shaft. The base is provided with a
cam part, and a guidance part with a preset shape is formed on the
cam part. The propeller blade
assembly is provided with a conduction part and a rotation angle spacing part, wherein the conduction part contacts the guidance part to drive the propeller blade assembly to rotate around the propeller blade shaft, the rotation angle spacing part limits the rotation angle of the propeller blade assembly around the propeller blade shaft. According to the present invention, the problems of requirements of large amount of continuous and stable air working medium with a certain
dynamic pressure energy during the vertical aircraft taking off and landing process are solved; the
power apparatus provided by the present invention has characteristics of simple structure, large
power load, high efficiency and convenient and flexible operation.