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    • 1. 发明授权
    • Auxiliary door fuselage closure
    • 辅助门关闭
    • US3704549A
    • 1972-12-05
    • US3704549D
    • 1971-03-22
    • EVERETTE G MCGHEE
    • MCGHEE EVERETTE G
    • E06B3/01E06B3/42
    • E06B3/01
    • The present invention contemplates a closure having primary utility for creating a snug fit between a hangar door and the tail section of an aircraft which projects through the door. In one embodiment, the invention includes carrier support means which are fixed to the hangar door on two opposing sections thereof. Secured to the carrier support means on each side of the opening in the hangar door are aperture carriers, each of which is mounted for movement on the support means toward and away from the other aperture carrier. A slot is formed in the abutting edges of each of the carriers so that when the carriers are adjacent each other, a continuous opening of generally circular cross-sectional configuration is created. Sliding vertically along support means mounted on each of the aperture carriers is an aperture frame which has a semicircular cutout formed thereon to register with the slot formed in the aperture carriers. As in the case of the aperture carriers, the semicircular cutouts formed in the aperture frames are so situated in each of the frames that when the frames abut a circular opening through the planes thereof is formed. Motive means are provided for moving the aperture frames vertically upward and downward with respect to the aperture carriers while similar motive means are provided for moving the aperture carriers toward and away from each other.
    • 本发明考虑到封闭件具有主要用途,用于在机库门和飞行器突出的飞机的尾部之间形成紧密配合。 在一个实施例中,本发明包括载体支撑装置,其固定在其两个相对部分上的机库门上。 固定在机库门的开口的每一侧上的托架支撑装置上的是小孔载体,每个支承装置安装成用于在支撑装置上移动并朝向另一个孔架。 在每个载体的邻接边缘中形成有槽,使得当载体彼此相邻时,形成大致圆形横截面构造的连续开口。 沿着安装在每个孔载体上的支撑装置垂直滑动的是具有形成在其上的半圆形切口的孔眼框架,其与形成在孔载体中的槽对准。 如在孔径载体的情况下,形成在孔眼框架中的半圆形切口被定位在每个框架中,当框架邻接通过其平面的圆形开口时。 提供了用于相对于孔载体垂直向上和向下移动孔眼架的动力装置,同时提供类似的动力装置用于使孔载体朝向和远离彼此移动。