Novel deformation aircraft of folding up

• Main Author: HU KAICHUN
• Format: Patent
• Language: Chinese; English
• Published: 29.03.2017
• Subjects: AEROPLANES; AIRCRAFT; AVIATION; CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION; COSMONAUTICS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; HELICOPTERS; PERFORMING OPERATIONS; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS; TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE; TRANSPORTING

The utility model relates to a novel deformation aircraft of folding up, including fuselage, the horn of folding up, wing, the foot rest of folding up, the fuselage includes fuselage shell, fuselage main part, and the fuselage shell cover is established outside the fuselage main part, the horn of folding up reaches to fold up to the fuselage through buckling of the connecting rod of folding up and closes up, and the horn of folding up design is the fretwork horn, the foot rest of folding up includes solid fixed ring of foot rest and stabilizer blade, and every stabilizer blade top and the solid fixed ring of foot rest correspond and set up the foot rest and consolidate fixed ring ear groove, fold up the inner of horn and fuselage main part upper portion outer end swing joint are with wing swing joint directly over the horn outer end of folding up, the lower extreme at fuselage shell is established to the solid fixed ring movable sleeve of foot rest, makes up to become to fold up the deformation aircraft, and