Multi -rotor aircraft

The application discloses multi -rotor aircraft. This multi -rotor aircraft includes: first rotor subassembly, it includes first supporting part, and install in the first group rotor of first supporting part, second rotor subassembly, it includes the second supporting part, and install in the second group rotor of second supporting part, rotating component, it is configured as pivot ground and connects first rotor subassembly with second rotor subassembly, so that first rotor subassembly and second rotor subassembly can rotate the axis around one and rotate relatively each other, wherein the axis perpendicular to rotates first supporting part with the principal plane of second supporting part, and the locking component, it is configured as works as first rotor subassembly for second rotor subassembly rotates and locks when one or more is predetermined to expand the position first rotor subassembly with relative rotation between the second rotor subassembly. 本申请公开了一种多旋翼飞行器。该多旋翼飞行器包括：第一旋翼组件，其包括第一支撑部，以及安装于所述第一支撑