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公开(公告)号：US10160028B2
公开(公告)日：2018-12-25
申请号：US14612824
申请日：2015-02-03
Applicant: Bell Helicopter Textron Inc.
Inventor： Mark Mays , Brian S. Modrzejewski , Dan Brungs , Doug Wylin
Abstract: A flexible bladder can be expanded to insert a tool by implementing a tool assembly that includes an elongated hollow member including a hollow portion to receive at least one of a flexible bladder or a tool. An inlet member is attached to an end of the elongated hollow member. The inlet member receives at least one of the flexible bladder or the tool. A port is positioned on the elongated hollow member to apply vacuum inside the elongated hollow member.
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Patent Agency Ranking
公开(公告)号：US20200047879A1
公开(公告)日：2020-02-13
申请号：US16056610
申请日：2018-08-07
Applicant: Bell Helicopter Textron Inc.
IPC: B64C27/473 , B29C70/30 , B29C70/54 , B32B1/08 , B32B5/12 , B32B5/02 , B32B5/26 , B32B37/18 , B32B38/18
Abstract: Embodiments are directed to systems and methods for creating a tubular composite structure. In one embodiment, a device comprises multiple layers of cured composite fabric bonded together to form a tubular composite structure, wherein alternating groups of the multiple layers comprise on-axis fabric and off-axis fabric. The tubular composite structure may form a spar for an aerodynamic component. The composite fabric may comprise one or more of carbon, fiberglass, or other composite materials, or a combination of materials. One or more stacks of the fabric wrap completely around the tubular composite structure, and other stacks of fabric may not wrap completely around the tubular composite structure.
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公开(公告)号：US20200031086A1
公开(公告)日：2020-01-30
申请号：US16048869
申请日：2018-07-30
Applicant: Bell Helicopter Textron Inc.
Inventor： Jared Mark Paulson , Mark Mays , Michael Christopher Burnett
IPC: B32B1/08 , B64C27/473 , B64C3/18 , B32B27/08
Abstract: Embodiments are directed to systems and methods for two or more cured composite assemblies that are bonded together to form a tubular composite structure, wherein each of the cured composite assemblies do not have a tubular shape. The tubular composite structure may form a spar for an aerodynamic component, for example. The two or more cured composite assemblies may comprise carbon or fiberglass composite materials or a combination of materials. Each of the cured composite assemblies may further comprise axial edges that are configured to be bonded to another of the cured composite assemblies, wherein the axial edges have a sloped shape. An adhesive agent may be applied on the axial edges for bonding two cured composite assemblies. Alternatively, or additionally, one or more fasteners may be used to attach the axial edges of at least two cured composite assemblies.
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公开(公告)号：US11565800B2
公开(公告)日：2023-01-31
申请号：US16048869
申请日：2018-07-30
Applicant: Bell Helicopter Textron Inc.
Inventor： Jared Mark Paulson , Mark Mays , Michael Christopher Burnett
Abstract: Embodiments are directed to systems and methods for two or more cured composite assemblies that are bonded together to form a tubular composite structure, wherein each of the cured composite assemblies do not have a tubular shape. The tubular composite structure may form a spar for an aerodynamic component, for example. The two or more cured composite assemblies may comprise carbon or fiberglass composite materials or a combination of materials. Each of the cured composite assemblies may further comprise axial edges that are configured to be bonded to another of the cured composite assemblies, wherein the axial edges have a sloped shape. An adhesive agent may be applied on the axial edges for bonding two cured composite assemblies. Alternatively, or additionally, one or more fasteners may be used to attach the axial edges of at least two cured composite assemblies.
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公开(公告)号：US11440652B2
公开(公告)日：2022-09-13
申请号：US16056610
申请日：2018-08-07
Applicant: Bell Helicopter Textron Inc.
IPC: B29C70/30 , B64C27/473 , B29C70/54 , B32B1/08 , B32B5/12 , B32B5/02 , B32B5/26 , B32B37/18 , B32B38/18 , B29C70/32 , B29C53/56 , B64C11/26 , B29K105/08 , B29K105/24 , B29L31/08
Abstract: Embodiments are directed to systems and methods for creating a tubular composite structure. In one embodiment, a device comprises multiple layers of cured composite fabric bonded together to form a tubular composite structure, wherein alternating groups of the multiple layers comprise on-axis fabric and off-axis fabric. The tubular composite structure may form a spar for an aerodynamic component. The composite fabric may comprise one or more of carbon, fiberglass, or other composite materials, or a combination of materials. One or more stacks of the fabric wrap completely around the tubular composite structure, and other stacks of fabric may not wrap completely around the tubular composite structure.
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公开(公告)号：US20160221062A1
公开(公告)日：2016-08-04
申请号：US14612824
申请日：2015-02-03
Applicant: Bell Helicopter Textron Inc.
Inventor： Mark Mays , Brian S. Modrzejewski , Dan Brungs , Doug Wylin
IPC: B21D39/20
CPC classification number: B21D39/203 , B29C33/3821 , B29C43/3642 , B29C45/14467 , B29C70/44 , B29C70/443
Abstract: A flexible bladder can be expanded to insert a tool by implementing a tool assembly that includes an elongated hollow member including a hollow portion to receive at least one of a flexible bladder or a tool. An inlet member is attached to an end of the elongated hollow member. The inlet member receives at least one of the flexible bladder or the tool. A port is positioned on the elongated hollow member to apply vacuum inside the elongated hollow member.
Abstract translation: 可以通过实施包括细长的中空构件的工具组件来扩展柔性气囊以插入工具，该中空构件包括中空部分以容纳柔性气囊或工具中的至少一个。 入口构件附接到细长型中空构件的端部。 入口构件容纳柔性气囊或工具中的至少一个。 端口位于细长的中空构件上，以在细长的中空构件内部施加真空。
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