Invention Grant
- 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.: US08464979B2Publication Date: 2013-06-18
- Inventor: Sunstar Im
- Applicant: Sunstar Im
- Main IPC: B64C3/00
- IPC: B64C3/00 ; B64C37/00

Abstract:
An aircraft structure is provide, an aircraft structure for an aircraft. including front Wing and rear wing of the Swan-Wing, 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 wing of the Swan-Wing are Disposed horizontally in front portion of the fuselage. rear wings of the Swan-Wing 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, cockpit 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 cabin disposed. front window, rear Window, side window and doors. under the belly of the Swan-Wing disposed Pontoons.
Public/Granted literature
- US20110000999A1 Foldable swan-wings aircraft Public/Granted day:2011-01-06
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