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1. 发明申请

US20100100355A1 IN-FLIGHT DETECTION OF WING FLAP FREE WHEELING SKEW 有权
标题翻译：飞行检测飞轮免费轮辋
公开(公告)号：US20100100355A1
公开(公告)日：2010-04-22
申请号：US12253747
申请日：2008-10-17
申请人： Alan D. Marx , Gary A. Emch , Mark J. Gardner , Richard I. Apfel , Michael E. Renzelmann , Christopher D. Feet , Michael R. Finn , Mark S. Good , Gregory J. Seehusen
发明人： Alan D. Marx , Gary A. Emch , Mark J. Gardner , Richard I. Apfel , Michael E. Renzelmann , Christopher D. Feet , Michael R. Finn , Mark S. Good , Gregory J. Seehusen
IPC分类号： G06F15/00
CPC分类号： B64D45/0005 , B64D2045/001
摘要： A method for detecting freewheeling skew failures in the wing flaps of an aircraft includes measuring the outputs of flap skew sensors when the aircraft is in flight (IF) and the flaps are extended to a selected position, and when the aircraft is next on the ground (OG) and the flaps are extended to the selected position. The respective differences between the IF and OG outputs of symmetrical pairs of the flap skew sensors are computed, and then the respective difference between the computed IF output difference and the computed OG output difference of each symmetrical pair of the sensors is computed. The computed IF and OG difference of each symmetrical pair of the sensors is then compared with each of predetermined maximum and minimum threshold value to determine whether a freewheeling skew failure exists in any of the flaps of the aircraft.
摘要翻译：一种用于检测飞行器翼片中的续流偏斜故障的方法，包括当飞机处于飞行中（IF）时测量襟翼歪斜传感器的输出，并且襟翼延伸到选定的位置，并且当飞机在地面上时（OG），并且襟翼延伸到所选位置。计算襟翼偏斜传感器的对称对的IF和OG输出之间的各自的差异，然后计算计算的IF输出差和每对传感器对的计算的OG输出差的相应差。然后将每个对称的传感器对的计算的IF和OG差与预定的最大和最小阈值中的每一个进行比较，以确定是否存在飞行器的任何襟翼中的空转歪斜故障。

2. 发明授权

US07945425B2 In-flight detection of wing flap free wheeling skew 有权
标题翻译：飞翼检测机翼翼片自由轮偏移
公开(公告)号：US07945425B2
公开(公告)日：2011-05-17
申请号：US12253747
申请日：2008-10-17
申请人： Alan D. Marx , Gary A. Emch , Mark J. Gardner , Richard I. Apfel , Michael E. Renzelmann , Christopher D. Feet , Michael R. Finn , Mark S. Good , Gregory J. Seehusen
发明人： Alan D. Marx , Gary A. Emch , Mark J. Gardner , Richard I. Apfel , Michael E. Renzelmann , Christopher D. Feet , Michael R. Finn , Mark S. Good , Gregory J. Seehusen
IPC分类号： G06F11/30
CPC分类号： B64D45/0005 , B64D2045/001
摘要： A method for detecting freewheeling skew failures in the wing flaps of an aircraft includes measuring the outputs of flap skew sensors when the aircraft is in flight (IF) and the flaps are extended to a selected position, and when the aircraft is next on the ground (OG) and the flaps are extended to the selected position. The respective differences between the IF and OG outputs of symmetrical pairs of the flap skew sensors are computed, and then the respective difference between the computed IF output difference and the computed OG output difference of each symmetrical pair of the sensors is computed. The computed IF and OG difference of each symmetrical pair of the sensors is then compared with each of predetermined maximum and minimum threshold value to determine whether a freewheeling skew failure exists in any of the flaps of the aircraft.
摘要翻译：一种用于检测飞行器翼片中的续流偏斜故障的方法，包括当飞机处于飞行中（IF）时测量襟翼歪斜传感器的输出，并且襟翼延伸到选定的位置，并且当飞机在地面上时（OG），并且襟翼延伸到所选位置。计算襟翼偏斜传感器的对称对的IF和OG输出之间的各自的差异，然后计算计算的IF输出差和每对传感器对的计算的OG输出差的相应差。然后将每个对称的传感器对的计算的IF和OG差与预定的最大和最小阈值中的每一个进行比较，以确定是否存在飞行器的任何襟翼中的空转歪斜故障。

3. 发明申请

US20130341467A1 SWING TIP ASSEMBLY ROTATION JOINT 有权
标题翻译：旋转总成旋转接头
公开(公告)号：US20130341467A1
公开(公告)日：2013-12-26
申请号：US13530089
申请日：2012-06-21
申请人： Seiya Sakurai , Kelly T. Jones , Stephen J. Fox , Bruce R. Fox , Nicholas I. Bennett , Mark S. Good
发明人： Seiya Sakurai , Kelly T. Jones , Stephen J. Fox , Bruce R. Fox , Nicholas I. Bennett , Mark S. Good
IPC分类号： B64C9/00 , F16C11/10 , B23P11/00 , F16C11/04
CPC分类号： B64C3/56 , Y02T50/14 , Y10T29/49826 , Y10T403/32254 , Y10T403/32327 , Y10T403/32361 , Y10T403/32606
摘要： A rotation joint and methods for rotationally coupling a swing tip assembly to a fluid-dynamic body are presented. A rotation plate configured to couple to the swing tip assembly comprises a slide ring comprising an open center, an upper slide surface, an inner slide surface, and a lower slide surface. An upper joint plate is slidably coupled to the upper slide surface and the inner slide surface is configured to couple the fluid-dynamic body. A lower joint plate is slidably coupled to the lower slide surface and the inner slide surface, and is coupled to the upper joint plate through the open center. The lower joint plate is configured to couple to the fluid-dynamic body.
摘要翻译：提出了旋转接头和用于将摆动尖端组件旋转耦合到流体动力体的方法。构造成联接到摆动尖端组件的旋转板包括滑动环，该滑动环包括敞开的中心，上部滑动表面，内部滑动表面和下部滑动表面。上接合板可滑动地联接到上滑动表面，并且内滑动表面构造成联接流体动力体。下接合板可滑动地联接到下滑动表面和内滑动表面，并且通过打开的中心联接到上接头板。下连接板被配置为联接到流体动力体。

4. 发明授权

US07494094B2 Aircraft wing systems for providing differential motion to deployable lift devices 有权
标题翻译：飞机机翼系统，用于为可部署升降机提供差速运动
公开(公告)号：US07494094B2
公开(公告)日：2009-02-24
申请号：US10935846
申请日：2004-09-08
申请人： Mark S. Good , Paul M. Viigen , Seth E. Gitnes , Glynn Michael Thomas
发明人： Mark S. Good , Paul M. Viigen , Seth E. Gitnes , Glynn Michael Thomas
IPC分类号： B64C3/50 , B64C9/00
CPC分类号： B64C3/50 , B64C9/14 , B64C13/26 , Y02T50/14 , Y02T50/32
摘要： Systems and methods for providing differential motion to wing high lift devices are disclosed. A system in accordance with one embodiment of the invention includes a wing having a leading edge, a trailing edge, a first deployable lift device with a first spanwise location, and a second deployable lift device with a second spanwise location different than the first. The wing system can further include a drive system having a drive link operatively coupleable to both the first and second deployable lift devices, and a control system operatively coupled to the drive system. The control system can have a first configuration for which the drive link is operatively coupled to the first and second deployable lift devices, and activation of at least a portion of the drive link moves the first and second deployable lift devices together. In a second configuration, the drive link is operatively coupled to at least the first deployable lift device and operatively decoupled from the second deployable lift device, so that actuation of at least a portion of the drive link moves the first deployable lift device relative to the second deployable lift device.
摘要翻译：公开了用于向机翼高升降装置提供差速运动的系统和方法。根据本发明的一个实施例的系统包括具有前缘，后缘，具有第一翼展位置的第一可展开升降装置和具有不同于第一翼展位置的第二翼展位置的第二可展开提升装置的翼。机翼系统还可以包括驱动系统，该驱动系统具有可操作地连接到第一和第二可展开提升装置两者的驱动链路，以及可操作地耦合到驱动系统的控制系统。控制系统可以具有第一构造，驱动连杆可操作地联接到第一和第二可展开提升装置，并且驱动连杆的至少一部分的启动使第一和第二可展开举升装置移动到一起。在第二构造中，驱动连杆可操作地联接到至少第一可展开提升装置并且可操作地与第二可展开提升装置分离，使得驱动连杆的至少一部分的致动使第一可展开提升装置相对于第二可展开提升装置。

5. 发明申请

US20090206209A1 SYSTEMS AND METHODS FOR PROVIDING DIFFERENTIAL MOTION TO WING HIGH LIFT DEVICE 有权
标题翻译：用于提供差分运动以实现高提升装置的系统和方法
公开(公告)号：US20090206209A1
公开(公告)日：2009-08-20
申请号：US12352447
申请日：2009-01-12
申请人： Mark S. Good , Paul M. Viigen , Seth E. Gitnes , Glynn Michael Thomas
发明人： Mark S. Good , Paul M. Viigen , Seth E. Gitnes , Glynn Michael Thomas
IPC分类号： B64C13/38
CPC分类号： B64C3/50 , B64C9/14 , B64C13/26 , Y02T50/14 , Y02T50/32
摘要： Systems and methods for providing differential motion to wing high lift devices are disclosed. A system in accordance with one embodiment of the invention includes a wing having a leading edge, a trailing edge, a first deployable lift device with a first spanwise location, and a second deployable lift device with a second spanwise location different than the first. The wing system can further include a drive system having a drive link operatively coupleable to both the first and second deployable lift devices, and a control system operatively coupled to the drive system. The control system can have a first configuration for which the drive link is operatively coupled to the first and second deployable lift devices, and activation of at least a portion of the drive link moves the first and second deployable lift devices together. In a second configuration, the drive link is operatively coupled to at least the first deployable lift device and operatively decoupled from the second deployable lift device, so that actuation of at least a portion of the drive link moves the first deployable lift device relative to the second deployable lift device.
摘要翻译：公开了用于向机翼高升降装置提供差速运动的系统和方法。根据本发明的一个实施例的系统包括具有前缘，后缘，具有第一翼展位置的第一可展开升降装置和具有不同于第一翼展位置的第二翼展位置的第二可展开提升装置的翼。机翼系统还可以包括驱动系统，该驱动系统具有可操作地连接到第一和第二可展开提升装置两者的驱动链路，以及可操作地耦合到驱动系统的控制系统。控制系统可以具有第一构造，驱动连杆可操作地联接到第一和第二可展开提升装置，并且驱动连杆的至少一部分的启动使第一和第二可展开举升装置移动到一起。在第二构造中，驱动连杆可操作地联接到至少第一可展开提升装置并且可操作地与第二可展开提升装置分离，使得驱动连杆的至少一部分的致动使第一可展开提升装置相对于第二可展开提升装置。

6. 发明申请

US20130327883A1 LATCHING APPARATUS AND METHODS 有权
公开(公告)号：US20130327883A1
公开(公告)日：2013-12-12
申请号：US13493688
申请日：2012-06-11
申请人： Jan A. Kordel , Mark S. Good
发明人： Jan A. Kordel , Mark S. Good
IPC分类号： B64C3/56 , E05B65/00 , B23P11/00 , E05C1/12
CPC分类号： B64C3/56 , B64C23/072 , Y02T50/164 , Y10T29/49826 , Y10T74/20238 , Y10T292/0962 , Y10T292/558
摘要： Latching apparatus and methods are disclosed herein. An example apparatus includes a first latch portion including a first tooth and a first pin disposed in a first aperture defined by the first tooth and a second latch portion including a second tooth and a second pin disposed in an second aperture defined by the second tooth. The second tooth of the second latch portion is to mesh with the first tooth of the first latch portion to substantially orient the first pin and the second pin along an axis. The example apparatus further includes an actuator adjacent a first end of one of the first latch portion or the second latch portion to move the first pin and the second pin along the axis to lock the first latch portion to the second latch portion.

7. 发明授权

US08708286B2 Swing tip assembly rotation joint 有权
标题翻译：摆动头组件旋转接头
公开(公告)号：US08708286B2
公开(公告)日：2014-04-29
申请号：US13530089
申请日：2012-06-21
申请人： Seiya Sakurai , Kelly T. Jones , Stephen J. Fox , Bruce R. Fox , Nicholas I. Bennett , Mark S. Good
发明人： Seiya Sakurai , Kelly T. Jones , Stephen J. Fox , Bruce R. Fox , Nicholas I. Bennett , Mark S. Good
IPC分类号： B64C9/00
CPC分类号： B64C3/56 , Y02T50/14 , Y10T29/49826 , Y10T403/32254 , Y10T403/32327 , Y10T403/32361 , Y10T403/32606
摘要： A rotation joint and methods for rotationally coupling a swing tip assembly to a fluid-dynamic body are presented. A rotation plate configured to couple to the swing tip assembly comprises a slide ring comprising an open center, an upper slide surface, an inner slide surface, and a lower slide surface. An upper joint plate is slidably coupled to the upper slide surface and the inner slide surface is configured to couple the fluid-dynamic body. A lower joint plate is slidably coupled to the lower slide surface and the inner slide surface, and is coupled to the upper joint plate through the open center. The lower joint plate is configured to couple to the fluid-dynamic body.
摘要翻译：提出了旋转接头和用于将摆动尖端组件旋转耦合到流体动力体的方法。构造成联接到摆动尖端组件的旋转板包括滑动环，该滑动环包括敞开的中心，上部滑动表面，内部滑动表面和下部滑动表面。上接合板可滑动地联接到上滑动表面，并且内滑动表面构造成联接流体动力体。下接合板可滑动地联接到下滑动表面和内滑动表面，并且通过打开的中心联接到上接头板。下连接板被配置为联接到流体动力体。

8. 发明授权

US08733692B2 Latching apparatus and methods 有权
标题翻译：闭锁装置和方法
公开(公告)号：US08733692B2
公开(公告)日：2014-05-27
申请号：US13493688
申请日：2012-06-11
申请人： Jan A. Kordel , Mark S. Good
发明人： Jan A. Kordel , Mark S. Good
IPC分类号： B64C3/56
CPC分类号： B64C3/56 , B64C23/072 , Y02T50/164 , Y10T29/49826 , Y10T74/20238 , Y10T292/0962 , Y10T292/558
摘要： Latching apparatus and methods are disclosed herein. An example apparatus includes a first latch portion including a first tooth and a first pin disposed in a first aperture defined by the first tooth and a second latch portion including a second tooth and a second pin disposed in an second aperture defined by the second tooth. The second tooth of the second latch portion is to mesh with the first tooth of the first latch portion to substantially orient the first pin and the second pin along an axis. The example apparatus further includes an actuator adjacent a first end of one of the first latch portion or the second latch portion to move the first pin and the second pin along the axis to lock the first latch portion to the second latch portion.
摘要翻译：本文公开了锁存装置和方法。示例性装置包括第一闩锁部分，其包括第一齿和设置在由第一齿限定的第一孔中的第一销和包括第二齿的第二闩锁部分和设置在由第二齿限定的第二孔中的第二销。第二闩锁部分的第二齿与第一闩锁部分的第一齿啮合，以使第一销和第二销基本上沿轴线定位。该示例设备还包括邻近第一闩锁部分或第二闩锁部分之一的第一端的致动器，以使第一销和第二销沿着轴线移动以将第一闩锁部分锁定到第二闩锁部分。

9. 发明授权

US07726610B2 Systems and methods for providing differential motion to wing high lift device 有权
标题翻译：用于向机翼高升力装置提供差速运动的系统和方法
公开(公告)号：US07726610B2
公开(公告)日：2010-06-01
申请号：US12352447
申请日：2009-01-12
申请人： Mark S. Good , Paul M. Vijgen , Seth E. Gitnes , Glynn Michael Thomas
发明人： Mark S. Good , Paul M. Vijgen , Seth E. Gitnes , Glynn Michael Thomas
IPC分类号： B64C9/00 , B64C13/02
CPC分类号： B64C3/50 , B64C9/14 , B64C13/26 , Y02T50/14 , Y02T50/32
摘要： Systems and methods for providing differential motion to wing high lift devices are disclosed. A system in accordance with one embodiment of the invention includes a wing having a leading edge, a trailing edge, a first deployable lift device with a first spanwise location, and a second deployable lift device with a second spanwise location different than the first. The wing system can further include a drive system having a drive link operatively coupleable to both the first and second deployable lift devices, and a control system operatively coupled to the drive system. The control system can have a first configuration for which the drive link is operatively coupled to the first and second deployable lift devices, and activation of at least a portion of the drive link moves the first and second deployable lift devices together. In a second configuration, the drive link is operatively coupled to at least the first deployable lift device and operatively decoupled from the second deployable lift device, so that actuation of at least a portion of the drive link moves the first deployable lift device relative to the second deployable lift device.
摘要翻译：公开了用于向机翼高升降装置提供差速运动的系统和方法。根据本发明的一个实施例的系统包括具有前缘，后缘，具有第一翼展位置的第一可展开升降装置和具有不同于第一翼展位置的第二翼展位置的第二可展开提升装置的翼。机翼系统还可以包括驱动系统，该驱动系统具有可操作地连接到第一和第二可展开提升装置两者的驱动链路，以及可操作地耦合到驱动系统的控制系统。控制系统可以具有第一构造，驱动连杆可操作地联接到第一和第二可展开提升装置，并且驱动连杆的至少一部分的启动使第一和第二可展开举升装置移动到一起。在第二构造中，驱动连杆可操作地联接到至少第一可展开提升装置并且可操作地与第二可展开提升装置分离，使得驱动连杆的至少一部分的致动使第一可展开提升装置相对于第二可展开提升装置。

10. 发明授权

US07309043B2 Actuation device positioning systems and associated methods, including aircraft spoiler droop systems 有权
标题翻译：致动装置定位系统及相关方法，包括飞机扰流器下垂系统
公开(公告)号：US07309043B2
公开(公告)日：2007-12-18
申请号：US11116905
申请日：2005-04-27
申请人： Mark S. Good , Neal V. Huynh , Kelly T. Jones , Selya Sakurai
发明人： Mark S. Good , Neal V. Huynh , Kelly T. Jones , Selya Sakurai
IPC分类号： B64C9/00
CPC分类号： B64C9/16 , B64C9/32 , B64C9/323 , B64C2009/143 , Y02T50/32
摘要： Actuation device positioning systems and associated methods, including aircraft spoiler droop systems are generally disclosed herein. One aspect of the invention is directed toward a positioning system that includes an eccentric cam and a drive mechanism coupled to the eccentric cam to rotate the eccentric cam between a first cam position and a second cam position. The system can further include an actuation device having an anchor portion and a movable portion that is movable relative to the anchor portion, the anchor portion operatively coupled to the eccentric cam. The eccentric cam can be positioned to move the anchor portion to a first anchor position when the eccentric cam is rotated to the first cam position and to move the anchor portion to a second anchor position when the eccentric cam is rotated to the second cam position.
摘要翻译：本文通常公开了致动装置定位系统和相关方法，包括飞机扰流器下垂系统。本发明的一个方面涉及一种定位系统，其包括偏心凸轮和联接到偏心凸轮的驱动机构，以在第一凸轮位置和第二凸轮位置之间旋转偏心凸轮。该系统还可以包括具有锚定部分和可相对于锚固部分可移动的可移动部分的致动装置，该锚固部分可操作地联接到偏心凸轮。当偏心凸轮旋转到第一凸轮位置时，偏心凸轮可以定位成将锚固部分移动到第一锚固位置，并且当偏心凸轮旋转到第二凸轮位置时，偏心凸轮可以定位成将锚定部分移动到第一锚定位置。

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