Invention Application
US20160096613A1 VTOL SYMMETRIC AIRFOIL FUSELAGE OF FIXED WING DESIGN 审中-公开
固定式设计的垂直变形对称气垫

VTOL SYMMETRIC AIRFOIL FUSELAGE OF FIXED WING DESIGN
Abstract:
Current aircraft technology comprises of fixed wing, multi rotor and vectored engine design. The synthesis of fixed wing technology and vectoring engine technology has been implemented but limited to traditional fixed wing design aircraft. The aircraft presented has been designed with an innovation in airframe expectation, improved vectoring engine design system, and landing gear system.
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