The invention discloses an electric folding wing
system with a high
aspect ratio, which comprises a
pulley support, a
servo motor, a synchronous belt,
pulley axle systems, universal couplings, clutchaxle systems, elastic wing axle systems,
axial compression springs, elastic wing rotating shaft mounting seats, elastic wings, locking pin assemblies and a cabin body. At the initial state, the wingsare in the folded state. After an unfolding command is issued, the unfolding function of four groups of elastic wings is realized under the driving of the
servo motor, and the unfolding state of the elastic wings is locked by the locking pin
assembly. The electric folding wing
system with the high
aspect ratio overcomes shortcomings of the prior art, parameterization of the
design process is realized, the
system can be transplanted quickly according to different
weapon system requirements. The system has the advantages of simple mechanism, reliable function, small envelope size in folded state, good aerodynamic shape in unfolded state, less space occupation by the mechanism inside the cabin, smoothness and no
impact in working process, and can be used as a
large aspect ratio folding wing
assembly of an airborne, ground-based and water-surface
barrel-launched
missile.