首页> 外国专利> Adjustable fittings for attaching support members to fluid conduits, including aircraft fuel conduits, and associated systems and methods

Adjustable fittings for attaching support members to fluid conduits, including aircraft fuel conduits, and associated systems and methods

机译:用于将支撑构件附接到流体导管(包括飞机燃料导管)的可调节配件以及相关的系统和方法

摘要

Adjustable fittings for attaching support members to fluid conduits, including aircraft fuel conduits, are disclosed herein. An aircraft system in accordance with one embodiment of the invention includes a fluid conduit carried by an aircraft and a housing fixedly attached to the fluid conduit. The housing can include a first attachment feature having one of a projection extending outwardly from the housing or an aperture extending at least partially through the housing. The system further includes a support member having an attachment portion positioned proximate to the attachment feature. The attachment portion includes a support member aperture positioned over at least a portion of the first attachment feature. An adjustable fitting couples the support member to the housing. The adjustable fitting can include a first side, a second side opposite the first side, and an engagement portion at the second side positioned within at least a portion of the support member aperture. The fitting can also include a second attachment feature mated with the first attachment feature. The second attachment feature includes the other one of the projection or the aperture. The second attachment feature has a center point eccentrically offset from a center point of the fitting.
机译:本文公开了用于将支撑构件附接到包括飞机燃料导管的流体导管的可调节配件。根据本发明的一个实施例的飞行器系统包括由飞行器携带的流体导管和固定地附接到该流体导管的壳体。壳体可以包括第一附接特征,该第一附接特征具有从壳体向外延伸的突起或至少部分地延伸穿过壳体的孔中的一个。该系统还包括支撑构件,该支撑构件具有位于该附接特征附近的附接部分。附接部分包括位于第一附接特征的至少一部分上方的支撑构件孔。可调节的配件将支撑构件联接至壳体。可调节配件可包括第一侧,与第一侧相对的第二侧以及位于第二侧的接合部分,该接合部分位于支撑构件孔的至少一部分内。配件还可以包括与第一附接特征配合的第二附接特征。第二附接特征包括突起或孔中的另一个。第二附接特征具有与配件的中心点偏心的中心点。

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