Invention Application
- Patent Title: Super aircraft structrue
- Patent Title (中): 超级飞机结构
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Application No.: US12317733Application Date: 2008-12-29
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Publication No.: US20100163669A1Publication Date: 2010-07-01
- Inventor: Sunstar Im
- Applicant: Sunstar Im
- Main IPC: B64C1/00
- IPC: B64C1/00 ; B64C3/00 ; B64D11/00 ; B64C35/00 ; B64D11/06 ; B64C9/00 ; B64C3/14 ; B64C1/14 ; B64C25/04 ; B64D45/00

Abstract:
An aircraft structure is provided. The aircraft structure for an aircraft includes a fuselage, front wings, rear small wings, vertical winglets, and four levels. The fuselage has a cross-section of substantially a half circle fuselage shape. Being is wide enough to provide lifting force, and includes four levels separated by multi partition structure. The front wings are disposed horizontally in front portions of the fuselage. The rear small wings are disposed horizontally in rear portions of the fuselage. The vertical winglets are disposed at the wingtips of the rear small wings. The first level disposed at a bottom of the four levels includes a fuel tank storages and a plurality of landing gear bays. The second level disposed at a middle of the four levels includes cargo bay. The third level may comprise a top cockpit and a plurality of passenger cabins. The fuselage provides major portion of lifting force and the wings provides steering force, and lifting force. The fourth level may comprises a plurality of passenger cabins.
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