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公开(公告)号：US20220234716A1
公开(公告)日：2022-07-28
申请号：US17577863
申请日：2022-01-18
Applicant: The Boeing Company
Inventor： Jenny Young , Daniel Cox , Steven David Ingham , Kyle Alexander Johnson , Mark Ronald McLaughlin , Paul Hungwai Lai
Abstract: A connector to connect a center wing box to a bulkhead of an aircraft. The connector includes a panel with a first edge positioned at the center wing box, an opposing second edge positioned at the bulkhead, and a central section. A first flexible seal extends across the panel and provides for relative movement between the first edge and the central section. A second flexible seal extends across the panel and provides for relative movement between the second edge and the central section.
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公开(公告)号：US20220033051A1
公开(公告)日：2022-02-03
申请号：US17305640
申请日：2021-07-12
Applicant: The Boeing Company
Inventor： Mark Ronald McLaughlin , Branko Lakic , Richard R. Rosman , Bernhard Dopker , Steven David Ingham
Abstract: A pressure deck system for a fuselage of an aircraft. The pressure deck system comprises a first sloping outboard pressure panel, a first longitudinal stiffener connected to the first sloping outboard pressure panel, a second sloping outboard pressure panel opposite the first sloping outboard pressure panel, a second longitudinal stiffener connected to the second sloping outboard pressure panel, pressure panels between the first sloping outboard pressure panel and the second sloping outboard pressure panel and forming the an upper barrier of a wheel well, longitudinal beams connected to the pressure panels and supporting a cabin floor of the fuselage, and a sloping pressure deck connecting a number of these components to the rear spar of the center wing box. A waterline of the pressure deck system is de-coupled from a side-of-body waterline in the fuselage.
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公开(公告)号：US11999464B2
公开(公告)日：2024-06-04
申请号：US17577863
申请日：2022-01-18
Applicant: The Boeing Company
Inventor： Jenny Young , Daniel Cox , Steven David Ingham , Kyle Alexander Johnson , Mark Ronald McLaughlin , Paul Hungwai Lai
Abstract: A connector to connect a center wing box to a bulkhead of an aircraft. The connector includes a panel with a first edge positioned at the center wing box, an opposing second edge positioned at the bulkhead, and a central section. A first flexible seal extends across the panel and provides for relative movement between the first edge and the central section. A second flexible seal extends across the panel and provides for relative movement between the second edge and the central section.
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公开(公告)号：US11634207B2
公开(公告)日：2023-04-25
申请号：US17305640
申请日：2021-07-12
Applicant: The Boeing Company
Inventor： Mark Ronald McLaughlin , Branko Lakic , Richard R. Rosman , Bernhard Dopker , Steven David Ingham
Abstract: A pressure deck system for a fuselage of an aircraft. The pressure deck system comprises a first sloping outboard pressure panel, a first longitudinal stiffener connected to the first sloping outboard pressure panel, a second sloping outboard pressure panel opposite the first sloping outboard pressure panel, a second longitudinal stiffener connected to the second sloping outboard pressure panel, pressure panels between the first sloping outboard pressure panel and the second sloping outboard pressure panel and forming the an upper barrier of a wheel well, longitudinal beams connected to the pressure panels and supporting a cabin floor of the fuselage, and a sloping pressure deck connecting a number of these components to the rear spar of the center wing box. A waterline of the pressure deck system is de-coupled from a side-of-body waterline in the fuselage.
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