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公开(公告)号：US12037832B2
公开(公告)日：2024-07-16
申请号：US17832751
申请日：2022-06-06
Applicant: THE BOEING COMPANY
Inventor： Richard A. Skilton , Michael A. Fleming
CPC classification number: E05F15/63 , B64C1/143 , B64C1/20 , E05Y2201/434 , E05Y2201/624 , E05Y2201/686 , E05Y2400/40 , E05Y2900/502
Abstract: An access system for a vehicle includes a door moveably coupled to a portion of a fuselage. The door is configured to be moved between an open position in which an opening of an internal chamber is opened, and a closed position in which the opening of the internal chamber is closed. One or more actuators are secured to the door. The one or more actuators are configured to move the door between the open position and the closed position.
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公开(公告)号：US11014691B2
公开(公告)日：2021-05-25
申请号：US16530004
申请日：2019-08-02
Applicant: The Boeing Company
Inventor： Robert W. Murray , Richard A. Skilton
Abstract: A method of making an aircraft includes steps of: assembling a subfloor assembly, including a panel support and plurality of transport elements; coupling a wheel well assembly to an airframe of the aircraft to form a nose landing gear bay of the aircraft; forming a pressure boundary delimiting a pressurized space and a non-pressurized space with the wheel well assembly and the airframe; coupling the subfloor assembly to the wheel well assembly, in the pressurized space, to form a portion of a floor of the aircraft so that the plurality of transport elements is located between the panel support and the wheel well assembly; and coupling the plurality of transport elements to at least one high-level system of the aircraft.
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公开(公告)号：US20210031948A1
公开(公告)日：2021-02-04
申请号：US16530004
申请日：2019-08-02
Applicant: The Boeing Company
Inventor： Robert W. Murray , Richard A. Skilton
Abstract: A method of making an aircraft includes steps of: assembling a subfloor assembly, including a panel support and plurality of transport elements; coupling a wheel well assembly to an airframe of the aircraft to form a nose landing gear bay of the aircraft; forming a pressure boundary delimiting a pressurized space and a non-pressurized space with the wheel well assembly and the airframe; coupling the subfloor assembly to the wheel well assembly, in the pressurized space, to form a portion of a floor of the aircraft so that the plurality of transport elements is located between the panel support and the wheel well assembly; and coupling the plurality of transport elements to at least one high-level system of the aircraft.
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公开(公告)号：US11420731B2
公开(公告)日：2022-08-23
申请号：US16529931
申请日：2019-08-02
Applicant: The Boeing Company
Inventor： Robert W. Murray , Richard A. Skilton
Abstract: A nose structure of an aircraft includes an airframe. A wheel well assembly is coupled to the airframe and forms a portion of a nose landing gear bay. The wheel well assembly includes a pressure deck that extends from a right side of the airframe to a left side of the airframe and that forms a portion of a pressure boundary delimiting a pressurized space and a non-pressurized space. A floor-panel support is supported by the pressure deck in the pressurized space. The pressure deck and the floor-panel support form a portion of a flight deck floor of a flight deck of the aircraft. A plurality of transport elements is located between the floor-panel support and the pressure deck. The plurality of transport elements is associated with at least one high-level system of the aircraft.
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公开(公告)号：US20210031903A1
公开(公告)日：2021-02-04
申请号：US16529931
申请日：2019-08-02
Applicant: The Boeing Company
Inventor： Robert W. Murray , Richard A. Skilton
Abstract: A nose structure of an aircraft includes an airframe. A wheel well assembly is coupled to the airframe and forms a portion of a nose landing gear bay. The wheel well assembly includes a pressure deck that extends from a right side of the airframe to a left side of the airframe and that forms a portion of a pressure boundary delimiting a pressurized space and a non-pressurized space. A floor-panel support is supported by the pressure deck in the pressurized space. The pressure deck and the floor-panel support form a portion of a flight deck floor of a flight deck of the aircraft. A plurality of transport elements is located between the floor-panel support and the pressure deck. The plurality of transport elements is associated with at least one high-level system of the aircraft.
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Patent Agency Ranking
公开(公告)号：US20230392428A1
公开(公告)日：2023-12-07
申请号：US17832751
申请日：2022-06-06
Applicant: THE BOEING COMPANY
Inventor： Richard A. Skilton , Michael A. Fleming
CPC classification number: E05F15/63 , B64C1/20 , B64C1/143 , E05Y2201/434 , E05Y2201/624 , E05Y2201/686 , E05Y2400/40 , E05Y2900/502
Abstract: An access system for a vehicle includes a door moveably coupled to a portion of a fuselage. The door is configured to be moved between an open position in which an opening of an internal chamber is opened, and a closed position in which the opening of the internal chamber is closed. One or more actuators are secured to the door. The one or more actuators are configured to move the door between the open position and the closed position.
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公开(公告)号：US11701796B2
公开(公告)日：2023-07-18
申请号：US17526718
申请日：2021-11-15
Applicant: THE BOEING COMPANY
Inventor： Courtney Michele Fix , Robert Wayne Murray , Paul Diep , Robert E. Lee , Richard A. Skilton , Ronald Leroy McGhee , Zachary Nathaniel Stoddard , Patrick B. Stone , Phillip Andrew Taylor , Nickolas Scott Ellerbeck
CPC classification number: B29C33/485 , B29C33/44 , B29C37/0003 , B64C1/064 , B29L2031/3082
Abstract: A system includes a mandrel contoured to define a tapering tubular shape of a workpiece cured on the mandrel and a demolding tool. The demolding tool is configured to remove the workpiece from the mandrel after the workpiece is cured on the mandrel and cut longitudinally. The demolding tool is configured to remove the workpiece from the mandrel by deforming a first end of the workpiece to at least partially disengage the first end of the workpiece from a first end of the mandrel, and subsequently, deforming a second end of the workpiece to at least partially disengage the second end of the workpiece from a second end of the mandrel. The first end of the workpiece may have a first cross-sectional area that is smaller than a second cross-sectional area of the second end of the workpiece.
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公开(公告)号：US20220193958A1
公开(公告)日：2022-06-23
申请号：US17526718
申请日：2021-11-15
Applicant: THE BOEING COMPANY
Inventor： Courtney Michele Fix , Robert Wayne Murray , Paul Diep , Robert E. Lee , Richard A. Skilton , Ronald Leroy McGhee , Zachary Nathaniel Stoddard , Patrick B. Stone , Phillip Andrew Taylor , Nickolas Scott Ellerbeck
Abstract: A system includes a mandrel contoured to define a tapering tubular shape of a workpiece cured on the mandrel and a demolding tool. The demolding tool is configured to remove the workpiece from the mandrel after the workpiece is cured on the mandrel and cut longitudinally. The demolding tool is configured to remove the workpiece from the mandrel by deforming a first end of the workpiece to at least partially disengage the first end of the workpiece from a first end of the mandrel, and subsequently, deforming a second end of the workpiece to at least partially disengage the second end of the workpiece from a second end of the mandrel. The first end of the workpiece may have a first cross-sectional area that is smaller than a second cross-sectional area of the second end of the workpiece.
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公开(公告)号：US20220234714A1
公开(公告)日：2022-07-28
申请号：US17647186
申请日：2022-01-06
Applicant: The Boeing Company
Inventor： Richard A. Skilton , Stephen T. Dougherty , Daniel Paul Hope Marx
Abstract: A pressure deck for an aircraft comprises a flat composite laminate base panel having integrated tear straps to enhance damage arrestment. The tear straps include a plurality of multi-ply, spaced apart longitudinal and lateral tear straps interspersed with the plies of the base panel.
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公开(公告)号：US11279470B2
公开(公告)日：2022-03-22
申请号：US16530112
申请日：2019-08-02
Applicant: The Boeing Company
Inventor： Robert W. Murray , Richard A. Skilton
Abstract: An aircraft includes an airframe, forming a nose structure of the aircraft, and at least one high-level system. The aircraft also includes a wheel well assembly, coupled to the airframe and forming a portion of a nose landing gear bay. The wheel well assembly includes a pressure deck that extends from a right side of the airframe to a left side of the airframe and that forms a portion of a pressure boundary delimiting a pressurized space and a non-pressurized space. The aircraft further includes a floor-panel support, supported by the pressure deck. The aircraft also includes a plurality of transport elements, located between the floor-panel support and the pressure deck.
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