The invention provides a deformable
biplane configuration. The configuration comprises an
upper wing, a
lower wing and a plurality of parallel distributed deformation mechanisms, wherein the
upper wing and the
lower wing are connected through the deformation mechanisms; each
deformation mechanism comprises a connecting strut and 1 to 2 motion mechanisms; a drive mechanism and a locking device are arranged on each motion mechanism which is fixed on the
upper wing or the
lower wing; one end of the connecting strut is mechanically connected with the motion mechanism, while the other end of the connecting strut is mechanically connected with the motion mechanism or fixedly connected with the upper wing or the lower wing; the drive mechanism drives the motion mechanism to drive the connecting strut to ensure that the upper wing and the lower wing rotate in 0 to 180 degrees in the course direction and the height direction; and when the upper wing and the lower wing move to a set position, the locking device locks the motion mechanism, and positions of the upper wing and the lower wing are fixed. Regarding the
wing configuration mode of a solar plane, the deformable
biplane configuration is adopted, compared with single plane configuration, under a condition that the same wing type, the same
wingspan and the same
aspect ratio of a single wing are adopted, through the deformable
biplane configuration, the
takeoff weight can be increased, the effective load can be increased, the induced drag of the wings can be reduced, and the area of a
solar cell panel can be increased, so that the
solar energy absorption capacity can be improved, and the
energy consumption of night flight can be reduced.