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公开(公告)号：EP2152575B1
公开(公告)日：2012-05-16
申请号：EP07867015.5
申请日：2007-03-12
发明人： LANDRY, Martin
IPC分类号： B64C27/12 , B64D47/06 , H01L41/113
CPC分类号： B64C27/12 , B64D47/06 , B64D2203/00 , H02N2/186 , Y02T50/53
摘要： A rotorcraft, such a helicopter or a tiltrotor aircraft, includes a light emitting device (400) configured to provide light at a tip (135) of a rotor blade. The light emitting device includes a light emitting diode arranged on the rotor blade and a power source, wherein the power source is configured to power the light emitting diode due to a movement of the rotor blade. The power source may include a piezo-electric material configured to create a voltage due to movements of the rotor blade or an electrical generator including a stationary magnet assembly and a moveable coil assembly arranged on a shaft that rotates the rotor blade.
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公开(公告)号：EP2234879B1
公开(公告)日：2013-11-06
申请号：EP09706631.0
申请日：2009-01-16
发明人： LANDRY, Martin
IPC分类号： B64C25/52
CPC分类号： B64C25/52 , B64C2025/325 , Y10T29/49947
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公开(公告)号：EP1881928B1
公开(公告)日：2011-12-21
申请号：EP06748404.8
申请日：2006-03-16
发明人： LANDRY, Martin
CPC分类号： B64C1/22 , B64C1/1415
摘要： An aircraft vehicle (100) includes a body (108), including a front portion and a rearward tail portion, a single panel door (105) constructed and arranged to close an access opening defined in a lower portion of the body (108), and a linkage between the body (108) and the door (105) . The linkage is constructed and arranged to move the door (105) generally rearwardly and upwardly when the door is moved from a closed position to an opened position, so that the door is positioned below and adjacent to the rearward tail portion.
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公开(公告)号：EP2234879A2
公开(公告)日：2010-10-06
申请号：EP09706631.0
申请日：2009-01-16
发明人： LANDRY, Martin
CPC分类号： B64C25/52 , B64C2025/325 , Y10T29/49947
摘要： A multi-piece pivot fitting for use on aircraft with skid type landing gear has a forward fitting, and aft fitting, and at least a lower strap. This configuration allows cross tube loads to be transferred to the keel beams of the aircraft, thereby allowing selected longitudinal rocking of the aircraft and preventing the aircraft from going into a resonance state.
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公开(公告)号：EP2152575A1
公开(公告)日：2010-02-17
申请号：EP07867015.5
申请日：2007-05-12
发明人： LANDRY, Martin
IPC分类号： B64C27/12 , B64D47/06 , H01L41/113
CPC分类号： B64C27/12 , B64D47/06 , B64D2203/00 , H02N2/186 , Y02T50/53
摘要： A rotorcraft, such a helicopter or a tiltrotor aircraft, includes a light emitting device (400) configured to provide light at a tip (135) of a rotor blade. The light emitting device includes a light emitting diode arranged on the rotor blade and a power source, wherein the power source is configured to power the light emitting diode due to a movement of the rotor blade. The power source may include a piezo-electric material configured to create a voltage due to movements of the rotor blade or an electrical generator including a stationary magnet assembly and a moveable coil assembly arranged on a shaft that rotates the rotor blade.
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公开(公告)号：EP1881928A1
公开(公告)日：2008-01-30
申请号：EP06748404.8
申请日：2006-03-16
发明人： LANDRY, Martin
CPC分类号： B64C1/22 , B64C1/1415
摘要： An aircraft vehicle (100) includes a body (108), including a front portion and a rearward tail portion, a single panel door (105) constructed and arranged to close an access opening defined in a lower portion of the body (108), and a linkage between the body (108) and the door (105) . The linkage is constructed and arranged to move the door (105) generally rearwardly and upwardly when the door is moved from a closed position to an opened position, so that the door is positioned below and adjacent to the rearward tail portion.
摘要翻译： 一种飞行器车辆（100），包括：包括前部和后部尾部的主体（108）;构造和布置成关闭限定在主体（108）的下部中的进入开口的单个板门（105） 和主体（108）和门（105）之间的连接。 联动装置被构造和布置成当门从关闭位置移动到打开位置时大致向后和向上移动门（105），使得门位于后部尾部的下方并与之相邻。
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