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公开(公告)号：US09242722B2
公开(公告)日：2016-01-26
申请号：US14405758
申请日：2013-06-07
发明人： Florence Buoy , Etienne Merlet , Herve Gorecki , Oleg Gomolko , Sebastien Fontaine , Yann Vandenbaviere , Christian Gouard , Guillaume Pointel
CPC分类号： B64C13/04 , G05G9/047 , G05G2009/04707 , G05G2009/04714 , G05G2009/04766 , Y10T74/20201
摘要： The invention relates to a joystick (200) for controlling an aircraft, including a frame (201), a lever (202) mounted so as to be rotatably movable relative to the frame, and a mechanical linking assembly (203) for connecting the lever to the frame, the mechanical linking assembly (203) including: a first linking piece (213, 223) movably mounted relative to the frame (201) about a first rotation axis (X), a second linking piece (233, 243) movably mounted relative to the frame (201) about a second rotation axis (Y), the second rotation axis forming a non-zero angle with the first rotation axis, a third intermediate piece (255, 265) mounted so as to the rotatably movable relative to the first linking piece (213, 223) about a third rotation axis (Y′), a fourth intermediate piece (275, 285) mounted so as to be rotatably movable relative to the second linking piece (233, 243) about a fourth rotation axis (X′), the fourth rotation axis forming a non-zero angle with the third rotation axis, in which the linking pieces (213, 223; 233, 243) or the intermediate pieces (255, 265; 275, 285) are rotatably movable in relation to one another about a fifth rotation axis (Z′) forming a non-zero angle with the first rotation axis (X) and the second rotation axis (Y) or with the third rotation axis (Y′) and the fourth rotation axis (X′), respectively, so as to enable a variation of the angle formed between the first rotation axis and the second rotation axis or of the angle formed between the third rotation axis and the fourth rotation axis, respectively.
摘要翻译： 本发明涉及一种用于控制飞行器的操纵杆（200），包括框架（201），安装成可相对于框架可旋转地移动的杆（202）和用于连接杆 所述机械联接组件包括：围绕第一旋转轴线（X）相对于所述框架可移动地安装的第一连接件（213,223），可移动地连接到所述第二连接件（233,243） 相对于所述框架（201）围绕第二旋转轴线（Y）安装，所述第二旋转轴线与所述第一旋转轴线形成非零角度;第三中间件（255,265），安装成可旋转地移动的相对 绕第三旋转轴线（Y'）延伸到第一连接件（213,223），第四中间件（275,285）安装成相对于第二连接件（233,243）可旋转地移动， 旋转轴线（X'），第四旋转轴线与第三旋转轴线形成非零角度 s，其中连接件（213,223; 233,243）或所述中间件（255,265; 275,285）可相对于彼此绕所述第一旋转轴线（X）形成非零角度的第五旋转轴线（Z'）可旋转地运动，并且 第二旋转轴线（Y）或第三旋转轴线（Y'）和第四旋转轴线（X'），以便能够形成在第一旋转轴线和第二旋转轴线之间的角度的变化， 分别形成在第三旋转轴线和第四旋转轴线之间的角度。
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公开(公告)号：US20150128754A1
公开(公告)日：2015-05-14
申请号：US14405766
申请日：2013-06-07
发明人： Florence Buoy , Etienne Merlet , Herve Gorecki
CPC分类号： B64C13/04 , G05G1/04 , G05G5/03 , G05G9/047 , G05G2009/04766 , Y10T74/20474
摘要： The invention relates to a joystick (1) for controlling an aircraft, including a frame (2), a lever (3), a mechanical linking assembly (4) for connecting the lever to the frame enabling a rotation of the lever (3) relative to the frame (2) about a first rotation axis (X), in which the mechanical linking assembly (4) includes a first pivot joint (9), the first pivot join (9) including a first portion, a second portion movably mounted relative to the first portion, and at least two flexible blades, each flexible blade having an end that is attached to the first portion and another end that is attached to the second portion, and being resiliently deformable in order to enable a rotation of the second portion relative to the first portion along the first rotation axis (X) and to generate a return torque which hinders the rotation of the second portion relative to the first portion.
摘要翻译： 本发明涉及一种用于控制飞机的操纵杆（1），其包括框架（2），杠杆（3），用于将杠杆连接到框架的机械连接组件（4），使得能够使杠杆（3）旋转， 相对于所述框架（2）围绕第一旋转轴线（X），所述机械连接组件（4）包括第一枢转接头（9），所述第一枢转接头（9）包括第一部分，第二部分可移动地 相对于第一部分安装，以及至少两个柔性叶片，每个柔性叶片具有附接到第一部分的端部，以及附接到第二部分的另一端部，并且可弹性变形，以便能够使 第二部分，沿着第一旋转轴线（X）相对于第一部分，并且产生阻止第二部分相对于第一部分旋转的返回转矩。
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公开(公告)号：US20140331799A1
公开(公告)日：2014-11-13
申请号：US14363244
申请日：2012-12-03
发明人： Julie Rafaitin , Etienne Merlet
CPC分类号： F16H25/22 , F16C33/1025 , F16C33/1095 , F16H25/2252 , F16H57/041 , F16H57/042 , F16H57/0497 , Y10T74/18744
摘要： The invention relates to a mechanical member wherein a first part in contact with a second part movable relative to the first part, at least one of the parts including a coating of solid lubricant at least at contact zones between the first part and the second part, the solid lubricant being suitable on its own for lubricating the mechanical member. According to the invention, the mechanical member includes retention and capillary distribution means for distributing a fluid between the parts in such a manner as to form a film between said parts, which film can be pierced temporarily at each contact zone.
摘要翻译： 本发明涉及一种机械构件，其中与第二部分相接触的第一部分相对于第一部分可移动，至少一个部分包括至少在第一部分和第二部分之间的接触区域的固体润滑剂涂层， 固体润滑剂本身适用于润滑机械构件。 根据本发明，机械构件包括用于在各部件之间分配流体的保持和毛细管分配装置，以便在所述部件之间形成薄膜，该薄膜可以在每个接触区域临时刺穿。
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公开(公告)号：US09550560B2
公开(公告)日：2017-01-24
申请号：US14405766
申请日：2013-06-07
发明人： Florence Buoy , Etienne Merlet , Herve Gorecki
CPC分类号： B64C13/04 , G05G1/04 , G05G5/03 , G05G9/047 , G05G2009/04766 , Y10T74/20474
摘要： The invention relates to a joystick (1) for controlling an aircraft, including a frame (2), a lever (3), a mechanical linking assembly (4) for connecting the lever to the frame enabling a rotation of the lever (3) relative to the frame (2) about a first rotation axis (X), in which the mechanical linking assembly (4) includes a first pivot joint (9), the first pivot joint (9) including a first portion, a second portion movably mounted relative to the first portion, and at least two flexible blades, each flexible blade having an end that is attached to the first portion and another end that is attached to the second portion, and being resiliently deformable in order to enable a rotation of the second portion relative to the first portion along the first rotation axis (X) and to generate a return torque which hinders the rotation of the second portion relative to the first portion.
摘要翻译： 本发明涉及一种用于控制飞机的操纵杆（1），其包括框架（2），杠杆（3），用于将杠杆连接到框架的机械连接组件（4），使得能够使杠杆（3）旋转， 相对于框架（2）围绕第一旋转轴线（X），其中机械连接组件（4）包括第一枢转接头（9），第一枢转接头（9）包括第一部分，第二部分可移动地 相对于第一部分安装，以及至少两个柔性叶片，每个柔性叶片具有附接到第一部分的端部，以及附接到第二部分的另一端部，并且可弹性变形，以便能够使 第二部分，沿着第一旋转轴线（X）相对于第一部分，并且产生阻止第二部分相对于第一部分旋转的返回转矩。
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公开(公告)号：US09360094B2
公开(公告)日：2016-06-07
申请号：US14363244
申请日：2012-12-03
发明人： Julie Rafaitin , Etienne Merlet
CPC分类号： F16H25/22 , F16C33/1025 , F16C33/1095 , F16H25/2252 , F16H57/041 , F16H57/042 , F16H57/0497 , Y10T74/18744
摘要： The invention relates to a mechanical member wherein a first part in contact with a second part movable relative to the first part, at least one of the parts including a coating of solid lubricant at least at contact zones between the first part and the second part, the solid lubricant being suitable on its own for lubricating the mechanical member. According to the invention, the mechanical member includes retention and capillary distribution means for distributing a fluid between the parts in such a manner as to form a film between said parts, which film can be pierced temporarily at each contact zone.
摘要翻译： 本发明涉及一种机械构件，其中与第二部分相接触的第一部分相对于第一部分可移动，至少一个部分包括至少在第一部分和第二部分之间的接触区域的固体润滑剂涂层， 固体润滑剂本身适用于润滑机械构件。 根据本发明，机械构件包括用于在各部件之间分配流体的保持和毛细管分配装置，以便在所述部件之间形成薄膜，该薄膜可以在每个接触区域临时刺穿。
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公开(公告)号：US20150158575A1
公开(公告)日：2015-06-11
申请号：US14405758
申请日：2013-06-07
发明人： Florence Buoy , Etienne Merlet , Herve Gorecki , Oleg Gomolko , Sebastien Fontaine , Yann Vandenbaviere , Christian Gouard , Guillaume Pointel
CPC分类号： B64C13/04 , G05G9/047 , G05G2009/04707 , G05G2009/04714 , G05G2009/04766 , Y10T74/20201
摘要： The invention relates to a joystick (200) for controlling an aircraft, including a frame (201), a lever (202) mounted so as to be rotatably movable relative to the frame, and a mechanical linking assembly (203) for connecting the lever to the frame, the mechanical linking assembly (203) including: a first linking piece (213, 223) movably mounted relative to the frame (201) about a first rotation axis (X), a second linking piece (233, 243) movably mounted relative to the frame (201) about a second rotation axis (Y), the second rotation axis forming a non-zero angle with the first rotation axis, a third intermediate piece (255, 265) mounted so as to the rotatably movable relative to the first linking piece (213, 223) about a third rotation axis (Y′), a fourth intermediate piece (275, 285) mounted so as to be rotatably movable relative to the second linking piece (233, 243) about a fourth rotation axis (X′), the fourth rotation axis forming a non-zero angle with the third rotation axis, in which the linking pieces (213, 223; 233, 243) or the intermediate pieces (255, 265; 275, 285) are rotatably movable in relation to one another about a fifth rotation axis (Z′) forming a non-zero angle with the first rotation axis (X) and the second rotation axis (Y) or with the third rotation axis (Y′) and the fourth rotation axis (X′), respectively, so as to enable a variation of the angle formed between the first rotation axis and the second rotation axis or of the angle formed between the third rotation axis and the fourth rotation axis, respectively.
摘要翻译： 本发明涉及一种用于控制飞行器的操纵杆（200），包括框架（201），安装成可相对于框架可旋转地移动的杆（202）和用于连接杆 所述机械联接组件包括：围绕第一旋转轴线（X）相对于所述框架可移动地安装的第一连接件（213,223），可移动地连接到所述第二连接件（233,243） 相对于所述框架（201）围绕第二旋转轴线（Y）安装，所述第二旋转轴线与所述第一旋转轴线形成非零角度;第三中间件（255,265），安装成可旋转地移动的相对 绕第三旋转轴线（Y'）延伸到第一连接件（213,223），第四中间件（275,285）安装成相对于第二连接件（233,243）可旋转地移动， 旋转轴线（X'），第四旋转轴线与第三旋转轴线形成非零角度 s，其中连接件（213,223; 233,243）或所述中间件（255,265; 275,285）可相对于彼此绕所述第一旋转轴线（X）形成非零角度的第五旋转轴线（Z'）可旋转地运动，并且 第二旋转轴线（Y）或第三旋转轴线（Y'）和第四旋转轴线（X'），以便能够形成在第一旋转轴线和第二旋转轴线之间的角度的变化， 分别形成在第三旋转轴线和第四旋转轴线之间的角度。
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