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公开(公告)号：US11167840B2
公开(公告)日：2021-11-09
申请号：US16385542
申请日：2019-04-16
Applicant: The Boeing Company
Inventor： Samuel Lewis Block , Orion Parker Watson , Daniel Harvey Fletcher , Michael Robert Rush , Elizabeth Rose Benson
Abstract: Aircraft main landing gear drag brace backup fitting assemblies and related methods are described herein. An example aircraft wing disclosed herein includes a rear spar having a rear side and a front side opposite the rear side, a side-of-body rib coupled to the rear spar, a rib post disposed on the front side of the rear spar, where the rib post is to couple a second rib to the rear spar, a side-of-body fitting coupled to the side-of-body rib, an intercostal member coupled between the side-of-body fitting and the rib post, and a drag brace fitting disposed on the rear side of the rear spar. The drag brace fitting is coupled to the rib post and the side-of-body fitting via a first plurality of fasteners extending through the rear spar.
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公开(公告)号：US20200331595A1
公开(公告)日：2020-10-22
申请号：US16385542
申请日：2019-04-16
Applicant: The Boeing Company
Inventor： Samuel Lewis Block , Orion Parker Watson , Daniel Harvey Fletcher , Michael Robert Rush , Elizabeth Rose Benson
Abstract: Aircraft main landing gear drag brace backup fitting assemblies and related methods are described herein. An example aircraft wing disclosed herein includes a rear spar having a rear side and a front side opposite the rear side, a side-of-body rib coupled to the rear spar, a rib post disposed on the front side of the rear spar, where the rib post is to couple a second rib to the rear spar, a side-of-body fitting coupled to the side-of-body rib, an intercostal member coupled between the side-of-body fitting and the rib post, and a drag brace fitting disposed on the rear side of the rear spar. The drag brace fitting is coupled to the rib post and the side-of-body fitting via a first plurality of fasteners extending through the rear spar.
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公开(公告)号：US20250083796A1
公开(公告)日：2025-03-13
申请号：US18463146
申请日：2023-09-07
Applicant: The Boeing Company
Inventor： Seiya Sakurai , Samuel Lewis Block , Bret Alan Bowers , Bryan Jacob Gruner
IPC: B64C9/20
Abstract: Multi-functional trailing edge apparatus and methods for aircraft are disclosed herein. An example wing of an aircraft disclosed herein includes an aft edge supporting a trailing edge device. The trailing edge device has a control surface and a side surface. A linkage is rotatably coupled to the side surface and the aft edge, and a rotary actuator is operatively coupled to the linkage to move the control surface.
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