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81. 发明专利

JP2019514236A 複数カメラネットワークを利用して静止シーン及び/又は移動シーンを取り込むためのシステム及び方法审中-公开
公开(公告)号：JP2019514236A
公开(公告)日：2019-05-30
申请号：JP2018540861
申请日：2017-01-27
申请人：ソニー株式会社
发明人：ベレストフアレクサンダー , リウミン−チャン , リーチュエン−チエン
IPC分类号： H04N5/232 , B64C39/02 , B64D47/08 , B64C19/02 , B64C13/20 , G03B15/00 , G03B37/00 , G06T7/593 , H04N5/222 , H04N5/247
摘要：本明細書では、ネットワーク内で複数のカメラを利用して移動シーンを取り込むためのシステム及び方法の様々な態様を開示する。システムは、複数の無人航空機(UAV)を含む。複数のUAVの各々は、複数の画像を取り込むように構成された撮像装置を伴う。複数のUAVのうちの第1のUAVは、1又は2以上の静止物体及び/又は移動物体の第1の一連の画像を取り込むように構成された第1の撮像装置を含む。第1のUAVは、1又は2以上の撮像装置から焦点レンズ情報と、現在位置と、現在の配向とを受け取るように構成される。1又は2以上の撮像装置の各々の目標位置及び目標配向を決定する。1又は2以上の撮像装置の各々の現在位置及び現在の配向を決定された目標位置及び目標配向に修正するための制御情報を1又は2以上の他のUAVに通信する。【選択図】図4A

82. 发明专利

JP2010047109A Unmanned aircraft system and method for operating the same 有权
标题翻译：不间断的飞机系统及其操作方法
公开(公告)号：JP2010047109A
公开(公告)日：2010-03-04
申请号：JP2008212958
申请日：2008-08-21
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： SUZUKI SATOSHI
IPC分类号： B64C37/02 , B64C13/20 , B64C19/02 , B64D47/08
CPC分类号： B64C39/024 , B64C37/02 , B64C2201/082 , B64C2201/206
摘要： PROBLEM TO BE SOLVED: To provide an unmanned aircraft system capable of taking off or landing in a state that an unmanned aircraft and a manned aircraft are combined, the unmanned aircraft used for the unmanned aircraft system, the manned aircraft used for the unmanned aircraft system, and an operation method of the unmanned aircraft system.
SOLUTION: The unmanned aircraft system has the manned aircraft 100 and the unmanned aircraft 200. The manned aircraft 100 is provided with a manned aircraft main wing 120, a manned aircraft fuselage 110, a manned aircraft landing system, and a manned aircraft combining mechanism 180 provided at a bottom 111 of the manned aircraft fuselage 110. The unmanned aircraft 200 is provided with an unmanned aircraft main wing 220, an unmanned aircraft fuselage 210, an unmanned landing system 270, and an unmanned aircraft combining mechanism 280 provided at a ceiling 211 of the unmanned aircraft fuselage 210. The manned aircraft combining mechanism 180 and the unmanned aircraft combining mechanism 280 are separably combined.
COPYRIGHT: (C)2010,JPO&INPIT
摘要翻译：要解决的问题：提供一种能够在无人驾驶飞机和载人飞机组合的状态下起飞或着陆的无人机系统，用于无人驾驶飞机系统的无人驾驶飞机，用于无人驾驶飞机系统，以及无人机系统的操作方法。解决方案：无人机系统有载人飞机100和无人驾驶飞机200.载人飞机100设有载人飞机主翼120，载人飞机机身110，载人飞机着陆系统和载人飞机组合机构180设置在载人飞行器机身110的底部111处。无人驾驶飞行器200设置有无人驾驶飞行器主翼220，无人驾驶飞机机身210，无人飞行器着陆系统270和设在其上的无人飞行器组合机构280 无人驾驶飞机机身210的天花板211.人造飞行器组合机构180和无人飞行器组合机构280可分离组合。版权所有（C）2010，JPO＆INPIT

83. 发明专利

JP4201468B2 Sling system by helicopter 有权
公开(公告)号：JP4201468B2
公开(公告)日：2008-12-24
申请号：JP2000265830
申请日：2000-09-01
申请人：富士重工業株式会社
发明人：猛志竹原
IPC分类号： B64C13/18 , B64D1/22 , B64C19/02 , B64C27/04 , G01S19/14 , G01S19/41 , G01S19/51

84. 发明专利

JP2000272591A PILOTING PEDAL FOR TWO-SEAT COCKPIT 失效
公开(公告)号：JP2000272591A
公开(公告)日：2000-10-03
申请号：JP7904899
申请日：1999-03-24
申请人： MITSUBISHI HEAVY IND LTD
发明人： MAKINO KENGO
IPC分类号： B64C13/12 , B64C19/02 , G05G1/30 , G05G1/34 , G05G1/44 , G05G1/14
摘要： PROBLEM TO BE SOLVED: To secure mechanical rigidity by a simple structure, to improve reliability with high accuracy and stability, and to reduce costs in a piloting pedal disposed for two-seat cockpit for an aircraft or the like. SOLUTION: One shaft 30 is provided to communicate a chief-pilot seat with a co-pilot seat, pairs of left and right foot pedals 1a and 1b and 2a and 2b respectively provided in the pilot seats are supported in common on the shaft 30, ones among the left and right food pedals disposed in the same direction of the left or right are fixed to the shaft 30 while the remaining ones are supported rotatably, the left and right food pedals of each pilot seat are linked with each other to be rotatable relatively in reverse directions, and even when mainly piloted by any of the chief-or co-pilot seat, its movement is caused to appear as the integral movement of a unified article in the movement of the other pilot seat.

85. 发明专利

JPH06191493A AIRCRAFT 失效
公开(公告)号：JPH06191493A
公开(公告)日：1994-07-12
申请号：JP34430292
申请日：1992-12-24
申请人： MITSUBISHI HEAVY IND LTD
发明人： KITAMA SHIYOUJI
IPC分类号： B64C19/02 , B64D33/02 , B64D33/04
摘要： PURPOSE:To provide a tandem two-seat type twin-engined aircraft whose fuselage frontal projected area can be made small while excellent forward field of view is secured for a rear seat. CONSTITUTION:Two engines 2 and 3 are mounted onto an aircraft 1 in such a way as to be arranged in parallel in the vertical direction of its airframe, and air intakes 4 for the engines 2 and 3 are provided for both the sides of its fuselage. A tandem two-seat assembly where a rear seat is disposed higher than a front seat, is provided for the forward half section of the airframe so as to allow a canopy 5 for the tandem two-seat assembly to be secured therein. This constitution thereby enables the aircraft to be formed into the tandem two-seat type aircraft with the air intakes provided for both the sides of the fuselage thus as mentioned above, and moreover enables the field of view for the rear seat to be secured.

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