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1.发明申请SYSTEMS AND METHODS FOR PROVIDING DIFFERENTIAL MOTION TO WING HIGH LIFT DEVICE 有权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
IPC分类号： B64C13/38
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。
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2.发明授权Aircraft wing systems for providing differential motion to deployable lift devices 有权飞机机翼系统，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
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。
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3.发明授权Systems and methods for providing differential motion to wing high lift device 有权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
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。
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公开(公告)号：US09417634B2
公开(公告)日：2016-08-16
申请号：US13394421
申请日：2010-08-25
申请人： Glynn Michael Thomas
发明人： Glynn Michael Thomas
IPC分类号： G05D7/01
CPC分类号： G05D7/0133 , G05D7/03 , Y10T137/7784 , Y10T137/7808 , Y10T137/85986 , Y10T137/8671
摘要： The present invention relates generally to flow regulation in aircraft systems. More particularly, the present invention relates to a flow regulator 100 and a high-lift system 200 for an aircraft incorporating such a flow regulator 100. The flow regulator 100 comprises a fluid input port 102 for receiving a pressurized fluid, a fluid output port 104 for providing fluid having a regulated flow rate, and a regulator valve 106 connected in fluid communication between the fluid input port 102 and the fluid output port 104. The regulator valve 106 is operable to provide regulated fluid at a substantially constant output flow rate to the fluid output port 104. The flow regulator 100 also includes a flow switching mechanism 108 for switching the substantially constant output flow of the flow regulated fluid provided by the regulator valve 106 between a first flow rate and a second flow rate, the first flow rate being less than the second flow rate.
摘要翻译： 本发明一般涉及飞机系统中的流量调节。 更具体地说，本发明涉及一种用于包含这种流量调节器100的飞行器的流量调节器100和高升程系统200.流量调节器100包括用于接收加压流体的流体输入端口102，流体输出端口104 用于提供具有调节流速的流体，以及在流体输入端口102和流体输出端口104之间流体连通地连接的调节阀106.调节阀106可操作以将基本恒定的输出流量的调节流体提供给 流量调节器100还包括流量切换机构108，用于在第一流量和第二流量之间切换由调节阀106提供的流量调节流体的基本恒定的输出流量，第一流量为 小于第二流量。
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公开(公告)号：US20120168560A1
公开(公告)日：2012-07-05
申请号：US13394421
申请日：2010-08-25
申请人： Glynn Michael Thomas
发明人： Glynn Michael Thomas
CPC分类号： G05D7/0133 , G05D7/03 , Y10T137/7784 , Y10T137/7808 , Y10T137/85986 , Y10T137/8671
摘要： The present invention relates generally to flow regulation in aircraft systems. More particularly, the present invention relates to a flow regulator 100 and a high-lift system 200 for an aircraft incorporating such a flow regulator 100. The flow regulator 100 comprises a fluid input port 102 for receiving a pressurised fluid, a fluid output port 104 for providing fluid having a regulated flow rate, and a regulator valve 106 connected in fluid communication between the fluid input port 102 and the fluid output port 104. The regulator valve 106 is operable to provide regulated fluid at a substantially constant output flow rate to the fluid output port 104. The flow regulator 100 also includes a flow switching mechanism 108 for switching the substantially constant output flow of the flow regulated fluid provided by the regulator valve 106 between a first flow rate and a second flow rate, the first flow rate being less than the second flow rate.
摘要翻译： 本发明一般涉及飞机系统中的流量调节。 更具体地说，本发明涉及一种用于包含这种流量调节器100的飞行器的流量调节器100和高升程系统200.流量调节器100包括用于接收加压流体的流体输入端口102，流体输出端口104 用于提供具有调节流速的流体;以及调节阀106，其连接在流体输入端口102和流体输出端口104之间的流体连通中。调节阀106可操作以将基本恒定的输出流量的调节流体提供给 流量调节器100还包括流量切换机构108，用于在第一流量和第二流量之间切换由调节阀106提供的流量调节流体的基本恒定的输出流量，第一流量为 小于第二流量。
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