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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：US10029780B2
公开(公告)日：2018-07-24
申请号：US14902850
申请日：2013-08-09
Applicant: The Boeing Company
Inventor： Joshua Amory Ross , Shane Frank Cuda , Mark Ronald McLaughlin , Michael Robert Rush , Colin Lee Farr , David Bruce Smith , Nihar Ashokkumar Desai , Thomas Joseph Kennedy , Lyle Ray Deobald
IPC: B64C3/26 , B29D99/00 , B29C70/30 , B64C3/18 , B29K105/08
Abstract: A stiffened panel comprises a composite panel, and a stiffener including a base flange on the composite panel. The base flange is tapered towards the panel. The stiffened panel further comprises a composite overwrap layer on only the composite panel and a tapered surface of the base flange.
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Patent Agency Ranking
公开(公告)号：US20160176500A1
公开(公告)日：2016-06-23
申请号：US14902850
申请日：2013-08-09
Applicant: THE BOEING COMPANY
Inventor： Joshua Amory Ross , Shane Frank Cuda , Mark Ronald McLaughlin , Michael Robert Rush , Colin Lee Farr , David Bruce Smith , Nihar Ashokkumar Desai , Thomas Joseph Kennedy , Lyle Ray Deobald
CPC classification number: B64C3/26 , B29C70/30 , B29D99/0014 , B29K2105/0872 , B64C3/18 , Y02T50/43
Abstract: A stiffened panel comprises a composite panel, and a stiffener including a base flange on the composite panel. The base flange is tapered towards the panel. The stiffened panel further comprises a composite overwrap layer on only the composite panel and a tapered surface of the base flange.
Abstract translation: 加强板包括复合板，以及在复合板上包括基部凸缘的加强件。 底座法兰朝向面板逐渐变细。 加强板还包括仅在复合板上的复合外包层和基底凸缘的锥形表面。
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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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公开(公告)号：US11479336B2
公开(公告)日：2022-10-25
申请号：US16721741
申请日：2019-12-19
Applicant: The Boeing Company
Inventor： David Leibov , Ryan Scott Carruthers , Mark Ronald McLaughlin , Daniel Cox
Abstract: Pressure decks, aircraft that incorporate the pressure decks, and methods of manufacturing the pressure decks, where the pressure decks include a planar center deck section configured to be attached to a keel beam of the aircraft and a pair of diagonal deck panels each extending inwardly and downwardly from a front wing spar to the planar center deck section. The pressure deck attaches the front wing spar to the keel beam at positions selected to minimize deflection stresses on the pressure deck exerted by relative movement between the front wing spar and the keel beam.
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公开(公告)号：US20210188418A1
公开(公告)日：2021-06-24
申请号：US16721741
申请日：2019-12-19
Applicant: The Boeing Company
Inventor： David Leibov , Ryan Scott Carruthers , Mark Ronald McLaughlin , Daniel Cox
Abstract: Pressure decks, aircraft that incorporate the pressure decks, and methods of manufacturing the pressure decks, where the pressure decks include a planar center deck section configured to be attached to a keel beam of the aircraft and a pair of diagonal deck panels each extending inwardly and downwardly from a front wing spar to the planar center deck section. The pressure deck attaches the front wing spar to the keel beam at positions selected to minimize deflection stresses on the pressure deck exerted by relative movement between the front wing spar and the keel beam.
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