发明名称 VIRTUAL WINDOW FORMING SYSTEM FOR AIRCRAFT
摘要 PROBLEM TO BE SOLVED: To reduce the weight of an airframe by using a projector to project a video image photographed by a camera fitted to the airframe onto an inner side face of the airframe comparable to a window so as to eliminate cabin windows or decreased number of the cabin windows and to respond to a request of passengers desiring to see the scenery outside the windows. SOLUTION: In a virtual window forming system for an aircraft, a video camera 2 is provided to a cylindrical airframe 1 of an airliner. The video camera 2 is fitted to an outer side face 3 of a shell being the airframe 1 to photograph a video image changing with navigation of the airliner. A projector 5 installed at a ceiling 4 at the inside of the shell is placed nearly to a center of the airframe 1 and has two projection optical systems 6 almost laterally symmetrically. This projector 5 projects the video image photographed by the video camera 2 onto left and right shell walls of the shell. Through this projection, a virtual window 7 is generated on the shell on which no window is provided. The video image projected on the shell wall may not be as real time video image.
申请公布号 JP2000350195(A) 申请公布日期 2000.12.15
申请号 JP19990157613 申请日期 1999.06.04
申请人 MITSUBISHI HEAVY IND LTD 发明人 MURAYAMA KOICHI
分类号 H04N7/18;B64D11/00;B64D47/08 主分类号 H04N7/18
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