公开(公告)号：US20100314498A1

公开(公告)日：2010-12-16

申请号：US12456008

申请日：2009-06-10

Applicant: Sunstar Im

Inventor： Sunstar Im

IPC: B64G1/14 ,  B64G1/40 ,  B64G1/60 ,  B64C25/00 ,  B64C3/20 ,  B64C3/56

CPC classification number: B64C39/068 ,  B64C3/56 ,  B64G1/14 ,  B64G1/401

Abstract: The spacecraft structure is provide, the spacecraft structure for the spacecraft includes, a center fuselage, right wing side fuselage, left wing side fuselage, front wings, and rear wings of Arch-Wings, vertical winglets, and the first levels, the fuselage has a cross-section of substantially flat floor fuselage shape, being is wide enough to provide lifting force.The front wings of the Arch-Wings are disposed horizontally in rear portions of the fuselage the vertical winglets are disposed the top of the rear fuselage the first level disposed fuel tank storage, plurality of landing gear bays, cockpit with control panel, various avionic instruments, cabin doors.The top of the rear fuselage disposed jet-power plants and further more at compartment of the Arch-Wings disposed rocket power plants.The fuselage provide lifting force and the wings provides lifting force and steering force, he whole structure of spacecraft comprises carbon fiber honey comb composite molded structure which is makes the spacecraft lighter weight and shear strong.At the front portion of wing body compartment of the Arch-Wings comprises retro rocket power plant with covered door, and under belly of the Arch-Wings disposed pontoon systems which could provide float at sea port.

Abstract translation: 航天器结构提供，航天器的航天器结构包括中心机身，右翼侧机身，左翼侧机身，前翼，拱门后翼，垂直小翼和第一层，机身具有 基本平坦的地面机身形状的截面宽度足以提供提升力。 拱门的前翼水平放置在机身的后部，垂直小翼设置在后机身的顶部，第一级设置的燃油箱存储，多个起落架舱，驾驶舱与控制面板，各种航空电子仪器 ，客舱门。 后部机身的顶部设置了喷气发电厂，并在Arch-Wings的隔间安置了火箭发电厂。 机身提供提升力，机翼提供提升力和转向力，整个飞船结构包括碳纤维蜂蜜复合模制结构，使航天器的重量和剪力更轻。 Arch-Wings机翼舱前部包括复盖火箭发电厂，带盖门，拱门下设置浮筒系统，可在海港提供浮球。