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1. 发明授权

US08157215B2 Door opening and closing apparatus for aircraft 有权
标题翻译：飞机开门和关闭装置
公开(公告)号：US08157215B2
公开(公告)日：2012-04-17
申请号：US12579050
申请日：2009-10-14
申请人： Wataru Yada , Hiroshi Yamanouchi , Hidetaka Nagano
发明人： Wataru Yada , Hiroshi Yamanouchi , Hidetaka Nagano
IPC分类号： B64C1/14 , B64C1/24
CPC分类号： B64C1/1423 , B64C1/1461
摘要： A door opening and closing mechanism for opening and closing the door from the inside of a fuselage. A door pivotally supported at an opening portion of the fuselage includes first and second position restricting links each having one end pivotally supported on the fuselage with a door driving link having one end pivotally supported on the door. The other end of the second position restricting link is pivotally supported on a middle portion of the door driving link. The door opening/closing operation lever is provided at one end with a grip with the other end pivotally supported on the other end of the door driving link. The middle portion of the door opening/closing operation lever is pivotally supported on the other end of the first position restricting link. By pulling the grip toward the inside of the fuselage and thereafter pushing downward, the door can be closed.
摘要翻译：用于从机身内部打开和关闭门的门打开和关闭机构。枢转地支撑在机身的开口部分处的门包括第一和第二位置限制连接件，每个连接件的一端枢转地支撑在机身上，其门驱动连杆具有枢转地支撑在门上的一端。第二位置限制连杆的另一端枢转地支撑在门驱动连杆的中间部分上。门打开/关闭操作杆的一端设置有把手，另一端枢转地支撑在门驱动连杆的另一端。门打开/关闭操作杆的中间部分枢转地支撑在第一位置限制连杆的另一端上。通过向机身内侧拉动把手，然后向下推，门可以关闭。

2. 发明申请

US20110067937A1 FRICTIONAL DRIVE DEVICE AND INVERTED PENDULUM TYPE VEHICLE USING THE SAME 有权
标题翻译：惯性驱动装置和使用相同的倒车型车辆
公开(公告)号：US20110067937A1
公开(公告)日：2011-03-24
申请号：US12884738
申请日：2010-09-17
申请人： Hiroshi GOMI , Shinichiro KOBASHI , Toru TAKENAKA , Kazushi Akimoto , Yuichi Uebayashi , Kazushi HAMAYA , Wataru YADA , Hironori Waita
发明人： Hiroshi GOMI , Shinichiro KOBASHI , Toru TAKENAKA , Kazushi Akimoto , Yuichi Uebayashi , Kazushi HAMAYA , Wataru YADA , Hironori Waita
IPC分类号： B62K11/00 , F16H13/04 , F16H37/02 , B62K1/00
CPC分类号： B62K1/00 , B60B19/003 , B60B19/125 , B60B2200/47 , B60B2310/204 , B60B2310/228 , B60B2310/232 , B60B2310/305 , B60B2360/10 , B60B2360/147 , B60B2360/32 , B60B2360/348 , B60B2360/50 , B60B2380/12 , B60B2380/14 , B60L1/003 , B60L3/0061 , B60L11/1803 , B60L11/1861 , B60L11/1877 , B60L2200/14 , B60L2220/42 , B60L2240/425 , B60L2240/461 , B60L2260/34 , B62K11/007 , Y02T10/646 , Y02T10/7005 , Y02T10/7044 , Y02T10/705 , Y10T74/19
摘要： A frictional drive device comprises a pair of drive disks (48) each rotatably supported by a frame (2, 42) around a central axial line (A) in a mutually opposing relationship, and a pair of actuators (64) supported by the frame for individually rotatively actuating the drive disks and coaxially disposed with respect to the corresponding drive disks, a plurality of drive rollers (56) arranged along an outer periphery of each drive disk and each having a rotational center line so as to be rotatable along a plane which is neither parallel nor perpendicular to the central axial line, and an annular main wheel (85) disposed approximately coaxially with respect to the central axial line and engaged by the drive rollers of the drive disks, the main wheel comprising an annular member (86) and a plurality of driven rollers (92) supported along the annular member so as to be rotatable around a tangential line of the annular member. A speed reduction unit (72, 100) may be interposed between each actuator and the corresponding drive disk all in a coaxial relationship.
摘要翻译：一种摩擦驱动装置，包括一对驱动盘（48），所述驱动盘（48）以相互相对的关系围绕中心轴线（A）由框架（2,22）可旋转地支撑;以及一对致动器（64），由所述框架用于单独地旋转地驱动驱动盘并且相对于相应的驱动盘同轴地布置;多个驱动辊（56），沿着每个驱动盘的外周布置，并且每个具有旋转中心线以沿着平面旋转其不与中心轴线平行或垂直;以及环形主轮（85），其相对于所述中心轴线大致同轴地设置并与所述驱动盘的驱动辊接合，所述主轮包括环形构件（86））和沿着所述环形构件支撑以便能够围绕所述环形构件的切线旋转的多个从动辊（92）。减速单元（72,100）可以以同轴的关系插入在每个致动器和对应的驱动盘之间。

3. 发明申请

US20080099605A1 Boarding ramp device for aircraft 有权
标题翻译：飞机登机坡道装置
公开(公告)号：US20080099605A1
公开(公告)日：2008-05-01
申请号：US11588262
申请日：2006-10-27
申请人： Wataru Yada , Hiroshi Yamanouchi
发明人： Wataru Yada , Hiroshi Yamanouchi
IPC分类号： B64C1/14
CPC分类号： B64C1/143 , B64C1/1407 , B64C1/24
摘要： When a single door for opening and closing an opening in a body is opened outward with its lower part as a fulcrum, a plurality of plate-shaped steps of a foldable boarding ramp provided on an inner face of the door are swung in association with one another from a stored position along the inner face of the door to a deployed position to be used for ingress and egress of the passengers. Since the boarding ramp is folded into the stored position, it does not impair the space of a passenger compartment. Further, since the steps are folded into a position so as not to interfere with a window provided in an upper part of the door, they do not give an oppressed feeling to the passengers in the passenger compartment. The step is deployed to cover the window provided in the upper part of the door during use.
摘要翻译：当用于打开和关闭主体中的开口的单个门以其下部为支点向外打开时，设置在门的内表面上的可折叠登机坡道的多个板状台阶与一个另一个从沿着门的内表面的存储位置到用于乘客的入口和出口的展开位置。由于登机斜坡被折叠到存储位置，所以不会损害乘客舱的空间。此外，由于台阶被折叠成不妨碍设置在门上部的窗口的位置，所以不会对乘客室内的乘客产生压迫感。在使用过程中，该步骤被部署以覆盖在门的上部提供的窗口。

4. 发明授权

US06464176B2 Flap operating device 有权
标题翻译：翻转操作装置
公开(公告)号：US06464176B2
公开(公告)日：2002-10-15
申请号：US09911372
申请日：2001-07-25
申请人： Minoru Uchida , Hiroshi Yamanouchi , Wataru Yada , Hidetaka Nagano
发明人： Minoru Uchida , Hiroshi Yamanouchi , Wataru Yada , Hidetaka Nagano
IPC分类号： B64C911
CPC分类号： B64C13/30 , B64C3/50 , B64C9/16 , B64C9/20 , Y02T50/44
摘要： A flap mounted on a tapered main wing of an aircraft, is supported by at least two link units. The link units are formed into analogous shapes with an analogous size ratio equal to the ratio between corresponding chord lengths of the main wing. As a result, the amounts of protrusion of the flap are varied in the span direction in accordance with the analogous size ratio, and the flap performs a three-dimensional motion such that it is moved in the span direction while being retracted and lowered. Thus, the flap can be moved to protrude to an optimal position and through an optimal angle according to the chord lengths of the main wing. When the flap is a slotted flap, an appropriate slot width can be ensured at each of the portions in the span direction, whereby the aerodynamic characteristic of the flap mounted on the tapered main wing can be uniform in the span direction.
摘要翻译：安装在飞机的锥形主翼上的翼片由至少两个连杆单元支撑。链节单元形成类似的形状，类似的尺寸比等于主翼翼的相应弦长之比。结果，翼片的突出量根据类似的尺寸比在跨度方向上变化，并且翼片执行三维运动，使得其在缩回和降低的同时在跨度方向上移动。因此，翼片可以根据主翼翼的弦长而移动到突出到最佳位置并且通过最佳角度。当翼片是开槽翼片时，可以在跨越方向的每个部分处确保适当的槽宽度，由此安装在锥形主翼上的翼片的空气动力学特性在跨度方向上可以是均匀的。

5. 发明授权

US08353378B2 Frictional drive device and inverted pendulum type vehicle using the same 有权
标题翻译：摩擦驱动装置和倒立摆式车辆使用它
公开(公告)号：US08353378B2
公开(公告)日：2013-01-15
申请号：US12884738
申请日：2010-09-17
申请人： Hiroshi Gomi , Shinichiro Kobashi , Toru Takenaka , Kazushi Hamaya , Wataru Yada , Kazushi Akimoto , Yuichi Uebayashi , Hironori Waita
发明人： Hiroshi Gomi , Shinichiro Kobashi , Toru Takenaka , Kazushi Hamaya , Wataru Yada , Kazushi Akimoto , Yuichi Uebayashi , Hironori Waita
IPC分类号： B62K1/00
CPC分类号： B62K1/00 , B60B19/003 , B60B19/125 , B60B2200/47 , B60B2310/204 , B60B2310/228 , B60B2310/232 , B60B2310/305 , B60B2360/10 , B60B2360/147 , B60B2360/32 , B60B2360/348 , B60B2360/50 , B60B2380/12 , B60B2380/14 , B60L1/003 , B60L3/0061 , B60L11/1803 , B60L11/1861 , B60L11/1877 , B60L2200/14 , B60L2220/42 , B60L2240/425 , B60L2240/461 , B60L2260/34 , B62K11/007 , Y02T10/646 , Y02T10/7005 , Y02T10/7044 , Y02T10/705 , Y10T74/19
摘要： A frictional drive device comprises a pair of drive disks (48) each rotatably supported by a frame (2, 42) around a central axial line (A) in a mutually opposing relationship, and a pair of actuators (64) supported by the frame for individually rotatively actuating the drive disks and coaxially disposed with respect to the corresponding drive disks, a plurality of drive rollers (56) arranged along an outer periphery of each drive disk and each having a rotational center line so as to be rotatable along a plane which is neither parallel nor perpendicular to the central axial line, and an annular main wheel (85) disposed approximately coaxially with respect to the central axial line and engaged by the drive rollers of the drive disks, the main wheel comprising an annular member (86) and a plurality of driven rollers (92) supported along the annular member so as to be rotatable around a tangential line of the annular member. A speed reduction unit (72, 100) may be interposed between each actuator and the corresponding drive disk all in a coaxial relationship.
摘要翻译：一种摩擦驱动装置，包括一对驱动盘（48），所述驱动盘（48）以相互相对的关系围绕中心轴线（A）由框架（2,22）可旋转地支撑;以及一对致动器（64），由所述框架用于单独地旋转地驱动驱动盘并且相对于相应的驱动盘同轴地布置;多个驱动辊（56），沿着每个驱动盘的外周布置，并且每个具有旋转中心线以沿着平面旋转其不与中心轴线平行或垂直;以及环形主轮（85），其相对于所述中心轴线大致同轴地设置并与所述驱动盘的驱动辊接合，所述主轮包括环形构件（86））和沿着所述环形构件支撑以便能够围绕所述环形构件的切线旋转的多个从动辊（92）。减速单元（72,100）可以以同轴的关系插入在每个致动器和对应的驱动盘之间。

6. 发明授权

US06530272B2 Flap test system 有权
标题翻译：襟翼测试系统
公开(公告)号：US06530272B2
公开(公告)日：2003-03-11
申请号：US09985776
申请日：2001-11-06
申请人： Minoru Uchida , Hiroshi Yamanouchi , Wataru Yada , Katsutoshi Tada
发明人： Minoru Uchida , Hiroshi Yamanouchi , Wataru Yada , Katsutoshi Tada
IPC分类号： G01P500
CPC分类号： G01M5/005 , G01M5/0016
摘要： A first cylinder drives a flap to a predetermined down position. Strain gages detect strains at each part of the flap while a load that corresponds to the down position is applied to the flap by a second cylinder that has been moved by an XY table so as to track the down position. Accordingly, actual aerodynamic forces are precisely reproduced by applying a load having a size and a direction that correspond to the down position of the flap. Thus, a stationary load test, a dynamic load test, and a durability test of the flap can be carried out automatically with a small effort and in a short time.
摘要翻译：第一气缸将挡板驱动到预定的向下位置。应变片检测翼片的每个部分处的应变，而对应于向下位置的负载通过已经被XY台移动以跟踪向下位置的第二圆柱体施加到翼片。因此，通过施加具有与翼片的向下位置对应的尺寸和方向的负载来精确地再现实际的空气动力。因此，能够在短时间内自动进行固定载荷试验，动态载荷试验和翼片的耐久试验。

7. 发明授权

US06464175B2 Rotor blade operating device in airplane and flaperon operating device in airplane 有权
标题翻译：飞机上的转子叶片操作装置和飞机上的襟副翼操作装置
公开(公告)号：US06464175B2
公开(公告)日：2002-10-15
申请号：US09903872
申请日：2001-07-13
申请人： Wataru Yada , Hiroshi Yamanouchi , Minoru Uchida , Katsutoshi Tada
发明人： Wataru Yada , Hiroshi Yamanouchi , Minoru Uchida , Katsutoshi Tada
IPC分类号： B64C1304
CPC分类号： B64C9/00 , B64C9/18 , Y02T50/32 , Y02T50/44
摘要： A flaperon operating device having a center pulley and a slider supported on a center shaft. When the center pulley and the slider are rotated about the center shaft, left and right driving pulleys are rotated in the same direction, whereby left and right flaperons are operated in opposite directions to provide aileron functions. When the slider is slid rearwards on the center shaft by an actuator, the left and right driving pulleys are rotated in opposite directions, whereby both the left and right flaperons are lowered to provide flap functions. If the left and right flaperons are lifted or lowered by a very small angle in the same phase by the actuator, boundary layers on main wings can be controlled to reduce the drag.
摘要翻译：具有中心皮带轮和支撑在中心轴上的滑块的襟副翼操作装置。当中心滑轮和滑块围绕中心轴旋转时，左右驱动滑轮沿相同方向旋转，由此左右襟翼在相反方向上操作以提供副翼功能。当滑块通过致动器在中心轴上向后滑动时，左右驱动滑轮沿相反方向旋转，由此左襟翼和右襟翼都被降低以提供挡板功能。如果左右襟翼在致动器的相同相位中被提升或降低非常小的角度，则可以控制主翼上的边界层以减小阻力。

8. 发明申请

US20100127124A1 DOOR OPENING AND CLOSING APPARATUS FOR AIRCRAFT 有权
标题翻译：开门机关闭装置
公开(公告)号：US20100127124A1
公开(公告)日：2010-05-27
申请号：US12579050
申请日：2009-10-14
申请人： Wataru YADA , Hiroshi Yamanouchi , Hidetaka Nagano
发明人： Wataru YADA , Hiroshi Yamanouchi , Hidetaka Nagano
IPC分类号： B64C1/24 , B64C1/14
CPC分类号： B64C1/1423 , B64C1/1461
摘要： A door opening and closing mechanism for opening and closing the door from the inside of a fuselage. A door pivotally supported at an opening portion of the fuselage includes first and second position restricting links each having one end pivotally supported on the fuselage with a door driving link having one end pivotally supported on the door. The other end of the second position restricting link is pivotally supported on a middle portion of the door driving link. The door opening/closing operation lever is provided at one end with a grip with the other end pivotally supported on the other end of the door driving link. The middle portion of the door opening/closing operation lever is pivotally supported on the other end of the first position restricting link. By pulling the grip toward the inside of the fuselage and thereafter pushing downward, the door can be closed.
摘要翻译：用于从机身内部打开和关闭门的门打开和关闭机构。枢转地支撑在机身的开口部分处的门包括第一和第二位置限制连接件，每个连接件的一端枢转地支撑在机身上，门部驱动连杆具有枢转地支撑在门上的一端。第二位置限制连杆的另一端枢转地支撑在门驱动连杆的中间部分上。门打开/关闭操作杆的一端设置有把手，另一端枢转地支撑在门驱动连杆的另一端。门打开/关闭操作杆的中间部分枢转地支撑在第一位置限制连杆的另一端上。通过向机身内侧拉动把手，然后向下推，门可以关闭。

9. 发明授权

US07677494B2 Boarding ramp device for aircraft 有权
标题翻译：飞机登机坡道装置
公开(公告)号：US07677494B2
公开(公告)日：2010-03-16
申请号：US11588262
申请日：2006-10-27
申请人： Wataru Yada , Hiroshi Yamanouchi
发明人： Wataru Yada , Hiroshi Yamanouchi
IPC分类号： B64C1/14 , B64C1/24
CPC分类号： B64C1/143 , B64C1/1407 , B64C1/24
摘要： When a single door for opening and closing an opening in a body is opened outward with its lower part as a fulcrum, a plurality of plate-shaped steps of a foldable boarding ramp provided on an inner face of the door are swung in association with one another from a stored position along the inner face of the door to a deployed position to be used for ingress and egress of the passengers. Since the boarding ramp is folded into the stored position, it does not impair the space of a passenger compartment. Further, since the steps are folded into a position so as not to interfere with a window provided in an upper part of the door, they do not give an oppressed feeling to the passengers in the passenger compartment. The step is deployed to cover the window provided in the upper part of the door during use.
摘要翻译：当用于打开和关闭主体中的开口的单个门以其下部为支点向外打开时，设置在门的内表面上的可折叠登机坡道的多个板状台阶与一个另一个从沿着门的内表面的存储位置到用于乘客的入口和出口的展开位置。由于登机斜坡被折叠到存储位置，所以不会损害乘客舱的空间。此外，由于台阶被折叠成不妨碍设置在门上部的窗口的位置，所以不会对乘客室内的乘客产生压迫感。在使用过程中，该步骤被部署以覆盖在门的上部提供的窗口。

10. 发明授权

US07669797B2 Boarding ramp device for aircraft 有权
标题翻译：飞机登机坡道装置
公开(公告)号：US07669797B2
公开(公告)日：2010-03-02
申请号：US11730732
申请日：2007-04-03
申请人： Wataru Yada , Hiroshi Yamanouchi
发明人： Wataru Yada , Hiroshi Yamanouchi
IPC分类号： B64C1/14
CPC分类号： B64C1/24
摘要： A foldable boarding ramp is operatively connected to a door opening provided in a body and is selectively extendable to the ground. The foldable boarding ramp is stored in a folded state inside a fairing covering a connecting portion between the body and a main wing. Thus, a reduction in the space of a passenger compartment and a cargo compartment due to the storage of the folded boarding ramp is prevented. In addition, an increase in air resistance can be suppressed without providing a dedicated fairing for covering the boarding ramp. Further, an interlocking member connects together a door for opening and closing the door opening and the boarding ramp when the door is opened. The boarding ramp may be automatically deployed to improve convenience.
摘要翻译：可折叠的登机斜坡可操作地连接到设置在主体中的门开口，并且可选地可延伸到地面。可折叠登机斜坡以折叠状态存储在覆盖主体和主翼之间的连接部分的整流罩内。因此，防止由于折叠的登机斜坡的存储而导致的乘客舱和货舱的空间减少。此外，可以抑制空气阻力的增加，而无需提供用于覆盖登机斜坡的专用整流罩。此外，当门打开时，互锁构件将门打开和关闭门开口和登机斜坡连接在一起。可以自动部署登机坡道以提高方便性。

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