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    • 1. 发明授权
    • Self-orienting aircraft landing gear
    • 自主定向飞机起落架
    • US09169003B2
    • 2015-10-27
    • US14333791
    • 2014-07-17
    • Byron YoungJon KarkowSteen Strand
    • Byron YoungJon KarkowSteen Strand
    • B64C25/50B64C25/36
    • B64C25/36B64C25/50
    • An aircraft landing gear self-orients so to align itself within a plane parallel to the plane defined by the aircraft's roll and yaw axis. A nose gear of a tricycle landing gear configuration includes the ability to not only caster 360 degrees but also self-orient itself to be aligned parallel with the plane defined by the aircraft's roll and yaw axis once removed from any interaction with the ground. A simple and efficient mechanical design provides the landing gear with a substantially constant centering torque that neither impedes nor impairs ground movement yet returns the nose gear to a proper alignment for retraction and stowage.
    • 飞机起落架自我定位,使其在平行于由飞机的侧倾和偏转轴限定的平面的平面内对准。 三轮车起落架配置的起落架包括不仅能够将脚轮360度的自动定向本身与由飞机的侧倾和偏航轴定义的平面对准的能力,一旦从与地面的任何相互作用中被去除, 一种简单有效的机械设计为起落架提供了基本上恒定的定心转矩,既不妨碍也不损害地面运动,而是使起落架返回正确的对齐方式以缩回和装载。
    • 3. 发明申请
    • SELF-ORIENTING AIRCRAFT LANDING GEAR
    • 自主研发飞机起落架
    • US20150021434A1
    • 2015-01-22
    • US14333791
    • 2014-07-17
    • Byron YoungJon KarkowSteen Strand
    • Byron YoungJon KarkowSteen Strand
    • B64C25/36
    • B64C25/36B64C25/50
    • An aircraft landing gear self-orients so to align itself within a plane parallel to the plane defined by the aircraft's roll and yaw axis. A nose gear of a tricycle landing gear configuration includes the ability to not only caster 360 degrees but also self-orient itself to be aligned parallel with the plane defined by the aircraft's roll and yaw axis once removed from any interaction with the ground. A simple and efficient mechanical design provides the landing gear with a substantially constant centering torque that neither impedes nor impairs ground movement yet returns the nose gear to a proper alignment for retraction and stowage.
    • 飞机起落架自我定位,使其在平行于由飞机的侧倾和偏转轴限定的平面的平面内对准。 三轮车起落架配置的起落架包括不仅能够将脚轮360度的自动定向本身与由飞机的侧倾和偏航轴定义的平面对准的能力,一旦从与地面的任何相互作用中被去除, 一种简单有效的机械设计为起落架提供了基本上恒定的定心转矩,既不妨碍也不损害地面运动,而是使起落架返回正确的对齐方式以缩回和装载。
    • 5. 发明授权
    • Multiple function intubation apparatus and method
    • 多功能插管装置及方法
    • US4613323A
    • 1986-09-23
    • US672414
    • 1984-11-19
    • Jane A. NortonDiana L. TwymanA. Byron YoungRobert Rapp
    • Jane A. NortonDiana L. TwymanA. Byron YoungRobert Rapp
    • A61J15/00A61M25/00
    • A61M25/0069A61J15/0003A61J15/0069A61J15/0073A61J15/0088A61J15/0096
    • An apparatus and its method of use are provided allowing lavage, sump and enteral feeding operations with only one intubation. The apparatus includes a first tube having two distinct passageways. One of these passageways completely contains a second, feeding tube during intubation. Once the first tube is in place in the patient, the second tube is extended from the first tube so as to enter the stomach. The extension of the second tube opens ports in the first passageway of the first tube, thereby allowing sump or lavage treatment with the second passageway of the first tube serving as an air vent. A constriction in the end of the first passageway engages a band on the proximal end of the second tube to keep the tubes together. Once gastric emptying of the patient resumes, the second tube immediately moves into the duodenum then into the jejunum past the Ligament of Treitz and the first tube is withdrawn from the patient while maintaining the second tube in position for enteral feeding through feeding ports in its distal end.
    • 提供了一种装置及其使用方法,其允许仅使用一次插管的灌洗,贮槽和肠内喂养操作。 该装置包括具有两个不同通道的第一管。 这些通道中的一个在插管期间完全包含第二个进料管。 一旦第一管位于患者的适当位置,第二管从第一管延伸以进入胃。 第二管的延伸部分打开第一管的第一通道中的端口,从而允许用作排气口的第一管的第二通道进行贮槽或灌洗处理。 在第一通道的端部处的收缩部接合在第二管的近端上的带以将管保持在一起。 一旦胃排空的患者恢复恢复,第二管立即进入十二指肠,然后进入经过Treitz韧带的空肠,第一个管从患者身上取出,同时将第二个管保持在适当的位置,以通过其远端的进料口进行肠内喂养 结束。