SPRING ASSEMBLY FOR AIRCRAFT COMPONENTS

    公开(公告)号:US20160167770A1

    公开(公告)日:2016-06-16

    申请号:US14568059

    申请日:2014-12-11

    发明人: Nicholas Toon

    IPC分类号: B64C25/20

    摘要: A spring assembly elongate along a longitudinal direction includes a first spring that includes a first spring member and a first elongate member that extends from the first spring member along the longitudinal direction. The spring assembly includes a second spring including a second spring member and a second elongate member that extends from the second spring member along the longitudinal direction. The second elongate member extends through the first spring member, and the first elongate member extends through the second spring member such that the first and second spring members are spaced apart with respect to each other along the longitudinal direction.

    SPRING ASSEMBLY FOR AIRCRAFT COMPONENTS
    2.
    发明申请
    SPRING ASSEMBLY FOR AIRCRAFT COMPONENTS 有权
    飞机组件弹簧总成

    公开(公告)号:US20160355255A1

    公开(公告)日:2016-12-08

    申请号:US15244317

    申请日:2016-08-23

    发明人: Nicholas Toon

    IPC分类号: B64C25/20 B64C25/34 B64C25/26

    摘要: A spring assembly elongate along a longitudinal direction includes a first spring that includes a first spring member and a first elongate member that extends from the first spring member along the longitudinal direction. The spring assembly includes a second spring including a second spring member and a second elongate member that extends from the second spring member along the longitudinal direction. The second elongate member extends through the first spring member, and the first elongate member extends through the second spring member such that the first and second spring members are spaced apart with respect to each other along the longitudinal direction.

    摘要翻译: 沿着纵向延伸的弹簧组件包括第一弹簧,其包括第一弹簧构件和从第一弹簧构件沿着纵向方向延伸的第一细长构件。 弹簧组件包括第二弹簧,其包括第二弹簧构件和从第二弹簧构件沿着纵向方向延伸的第二细长构件。 第二细长构件延伸穿过第一弹簧构件,并且第一细长构件延伸穿过第二弹簧构件,使得第一和第二弹簧构件沿着纵向相对于彼此间隔开。

    Spring assembly for aircraft components
    3.
    发明授权
    Spring assembly for aircraft components 有权
    弹簧组件用于飞机部件

    公开(公告)号:US09440732B2

    公开(公告)日:2016-09-13

    申请号:US14568059

    申请日:2014-12-11

    发明人: Nicholas Toon

    IPC分类号: B64C25/20

    摘要: A spring assembly elongate along a longitudinal direction includes a first spring that includes a first spring member and a first elongate member that extends from the first spring member along the longitudinal direction. The spring assembly includes a second spring including a second spring member and a second elongate member that extends from the second spring member along the longitudinal direction. The second elongate member extends through the first spring member, and the first elongate member extends through the second spring member such that the first and second spring members are spaced apart with respect to each other along the longitudinal direction.

    摘要翻译: 沿着纵向延伸的弹簧组件包括第一弹簧,其包括第一弹簧构件和从第一弹簧构件沿着纵向方向延伸的第一细长构件。 弹簧组件包括第二弹簧,其包括第二弹簧构件和从第二弹簧构件沿着纵向方向延伸的第二细长构件。 第二细长构件延伸穿过第一弹簧构件,并且第一细长构件延伸穿过第二弹簧构件,使得第一和第二弹簧构件沿着纵向相对于彼此间隔开。

    NOISE-REDUCING AIRCRAFT LANDING GEAR TOW BAR FITTING

    公开(公告)号:US20210380276A1

    公开(公告)日:2021-12-09

    申请号:US16893028

    申请日:2020-06-04

    IPC分类号: B64F1/22 B64C25/60

    摘要: A tow bar fitting for towing an aircraft is disclosed. The tow bar fitting includes a mount, a pin support, and a tow pin. The mount includes an upper attachment and a lower attachment for affixing the tow bar fitting to a landing gear of the aircraft. The pin support extends from the mount away from the landing gear. The tow pin is positioned in the pin support such that a tow pin plane that horizontally bisects the tow pin is lower than a mount plane that horizontally bisects the upper attachment and the lower attachment when the aircraft is right-side-up on the ground.

    Noise-reducing aircraft landing gear tow bar fitting

    公开(公告)号:US11530051B2

    公开(公告)日:2022-12-20

    申请号:US16893028

    申请日:2020-06-04

    IPC分类号: B64F1/22 B64C25/60

    摘要: A tow bar fitting for towing an aircraft is disclosed. The tow bar fitting includes a mount, a pin support, and a tow pin. The mount includes an upper attachment and a lower attachment for affixing the tow bar fitting to a landing gear of the aircraft. The pin support extends from the mount away from the landing gear. The tow pin is positioned in the pin support such that a tow pin plane that horizontally bisects the tow pin is lower than a mount plane that horizontally bisects the upper attachment and the lower attachment when the aircraft is right-side-up on the ground.

    Spring assembly for aircraft components

    公开(公告)号:US09676474B2

    公开(公告)日:2017-06-13

    申请号:US15244317

    申请日:2016-08-23

    发明人: Nicholas Toon

    摘要: A spring assembly elongate along a longitudinal direction includes a first spring that includes a first spring member and a first elongate member that extends from the first spring member along the longitudinal direction. The spring assembly includes a second spring including a second spring member and a second elongate member that extends from the second spring member along the longitudinal direction. The second elongate member extends through the first spring member, and the first elongate member extends through the second spring member such that the first and second spring members are spaced apart with respect to each other along the longitudinal direction.