Invention Application
- Patent Title: Foldable swan-wings aircraft
- Patent Title (中): 可折叠天鹅翼飞机
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Application No.: US12455473Application Date: 2009-06-02
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Publication No.: US20110000999A1Publication Date: 2011-01-06
- Inventor: Sunstar Im
- Applicant: Sunstar Im
- Main IPC: B64C39/00
- IPC: B64C39/00 ; B64C3/56

Abstract:
An aircraft structure is provide, an aircraft structure for an aircraft. Including front wings And rear wings of the Swan-Wings, vertical winglets and the first level floor body. The Fuselage has a cross-section of substantially flat fuselage shape being is wide enough to Provide lifting force. The front wings of the Swan-Wings are disposed horizontally in Front portion of the fuselage. The rear wings of the Swan-Wings are disposed Horizontally in rear portion of the fuselage.The vertical winglets are disposed at the top of the rear fuselage.The first level disposed fuel tank storages, a plurality of landing gear bays, cockpits with Control panels, various avionics and cabin doors.The top of the rear fuselage disposed jet power plants, the fuselage provide lifting force And the wings provides steering force and lifting force the whole structure of an aircraft Comprises carbon fiber honey comb composite molded structure which lighter weight And shear strong structure. The cockpit and cabins disposed. Front window, rear window Side window and doors. Under the belly of the Swan-Wings disposed pontoons.
Public/Granted literature
- US08464979B2 Foldable swan-wings aircraft Public/Granted day:2013-06-18
Information query
IPC分类:
B | 作业;运输 |
B64 | 飞行器;航空;宇宙航行 |
B64C | 飞机;直升飞机(气垫车入B60V) |
B64C39/00 | 其他飞行器 |