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公开(公告)号：US10259018B2
公开(公告)日：2019-04-16
申请号：US15066027
申请日：2016-03-10
Applicant: The Boeing Company
Abstract: A method and apparatus for sealing a fastener element. A structure may be positioned over a seal cap that has been adhered and sealed to the fastener element. A number of projections associated with the structure may be moved along an interface formed between the seal cap and an object in which the fastener element has been installed such that the number of projections removes at least a portion of excess material around the seal cap while moving along the interface between the seal cap and the object.
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公开(公告)号：US20210262568A1
公开(公告)日：2021-08-26
申请号：US16800791
申请日：2020-02-25
Applicant: The Boeing Company
Inventor： Steven Kuan-Chi Wu , Ian Edward Schroeder , Mark Edmond Shadell , Melissa A. Uhlman , Jesse Randal Wiseman , Tho Ngoc Dang , Richard Bruce Tanner , Melinda Dae Miller , Kristopher William Talcott
Abstract: A seal arrangement is provided for sealing an exposed edge of a composite laminate part having a fay surface configured to be joined to a structure. The seal arrangement includes a precured edge seal covering the exposed edge and a cover covering the edge seal. A seal bead located within a recess in the fay surface of the part forms a seal between the part and the structure.
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公开(公告)号：US20170259306A1
公开(公告)日：2017-09-14
申请号：US15066027
申请日：2016-03-10
Applicant: The Boeing Company
Abstract: A method and apparatus for sealing a fastener element. A structure may be positioned over a seal cap that has been adhered and sealed to the fastener element. A number of projections associated with the structure may be moved along an interface formed between the seal cap and an object in which the fastener element has been installed such that the number of projections removes at least a portion of excess material around the seal cap while moving along the interface between the seal cap and the object.
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公开(公告)号：US20170152949A1
公开(公告)日：2017-06-01
申请号：US14954270
申请日：2015-11-30
Applicant: THE BOEING COMPANY
Inventor： Jesse Randal Wiseman , Shane S. Park , Donald K. Crenshaw , Kjersta Larson-Smith , Geoffrey Eric Towle , Hugh Christopher VanValkenburgh , Karen A. Schultz , Solomon T. Atsebha
CPC classification number: F16J15/002 , B64C3/00 , B64F5/10 , F16J15/14
Abstract: A sealant containment assembly is configured to bound at least a portion of a fastener pattern between at least two components, such as components used to form at least a portion of an aircraft. The sealant containment assembly includes at least one sealant containment member that is configured to sealingly engage peripheral portions of components. The sealant containment member(s) is configured to form a sealing chamber around at least a portion of the fastener pattern. Fluid sealant is configured to flow into the sealing chamber and cure to seal fasteners within the fastener pattern that connect the components together.
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公开(公告)号：US20170361916A1
公开(公告)日：2017-12-21
申请号：US15187408
申请日：2016-06-20
Applicant: THE BOEING COMPANY
Abstract: A dry bay sealing assembly is provided that includes a first end plate and a second end plate that are configured to be disposed on respective opposite first and second sides of a structural member proximate to a joint defined between the structural member and a fitting. The first end plate and the second end plate are configured to define an interior volume therebetween containing at least a portion of a fastener joining the structural member and the fitting. The first end plate and the second end plate are configured to cooperate with the structural member to seal the interior volume from an exterior volume.
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Patent Agency Ranking
公开(公告)号：US09789971B2
公开(公告)日：2017-10-17
申请号：US14722117
申请日：2015-05-26
Applicant: The Boeing Company
Inventor： Jesse Randal Wiseman , Kevin Darrell Pate , Matthew G. Chaney
IPC: F16J15/02 , F16J15/14 , F16J15/10 , B64D37/02 , B64D37/06 , H01M8/0276 , H01M8/0286 , B60K15/03
CPC classification number: B64D37/06 , B60K2015/03447 , B64D37/02 , F16J15/022 , F16J15/104 , F16J15/14 , H01M8/0276 , H01M8/0286 , H01M2250/20 , Y02T90/32
Abstract: An aircraft fuel cell seal and methods of its use. The disclosed seal takes the form of a pre-cured, partially hollow elongate member that does not subtend a complete circle, but rather leaves an elongate gap in the member that can be placed over an edge or fillet of a fuel cell. In some cases, chambers within the member may be filled with wet sealant to provide redundant protection against EME effects.
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公开(公告)号：US20160276679A1
公开(公告)日：2016-09-22
申请号：US14722117
申请日：2015-05-26
Applicant: The Boeing Company
Inventor： Jesse Randal Wiseman , Kevin Darrell Pate , Matthew G. Chaney
IPC: H01M8/0276 , F16J15/02 , F16J15/14 , H01M8/0286
CPC classification number: B64D37/06 , B60K2015/03447 , B64D37/02 , F16J15/022 , F16J15/104 , F16J15/14 , H01M8/0276 , H01M8/0286 , H01M2250/20 , Y02T90/32
Abstract: An aircraft fuel cell seal and methods of its use. The disclosed seal takes the form of a pre-cured, partially hollow elongate member that does not subtend a complete circle, but rather leaves an elongate gap in the member that can be placed over an edge or fillet of a fuel cell. In some cases, chambers within the member may be filled with wet sealant to provide redundant protection against EME effects.
Abstract translation: 飞机燃料电池密封及其使用方法。 所公开的密封采取预固化的部分中空的细长构件的形式，其不对着完整的圆，而是在构件中留下可以放置在燃料电池的边缘或圆角上的细长间隙。 在某些情况下，成员内的室可以填充湿密封剂，以提供对EME效应的冗余保护。
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公开(公告)号：US11543029B2
公开(公告)日：2023-01-03
申请号：US16800791
申请日：2020-02-25
Applicant: The Boeing Company
Inventor： Steven Kuan-Chi Wu , Ian Edward Schroeder , Mark Edmond Shadell , Melissa A. Uhlman , Jesse Randal Wiseman , Tho Ngoc Dang , Richard Bruce Tanner , Melinda Dae Miller , Kristopher William Talcott
Abstract: A seal arrangement is provided for sealing an exposed edge of a composite laminate part having a fay surface configured to be joined to a structure. The seal arrangement includes a precured edge seal covering the exposed edge and a cover covering the edge seal. A seal bead located within a recess in the fay surface of the part forms a seal between the part and the structure.
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公开(公告)号：US10556665B2
公开(公告)日：2020-02-11
申请号：US15187408
申请日：2016-06-20
Applicant: THE BOEING COMPANY
Abstract: A dry bay sealing assembly is provided that includes a first end plate and a second end plate that are configured to be disposed on respective opposite first and second sides of a structural member proximate to a joint defined between the structural member and a fitting. The first end plate and the second end plate are configured to define an interior volume therebetween containing at least a portion of a fastener joining the structural member and the fitting. The first end plate and the second end plate are configured to cooperate with the structural member to seal the interior volume from an exterior volume.
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公开(公告)号：US09295367B2
公开(公告)日：2016-03-29
申请号：US13886557
申请日：2013-05-03
Applicant: The Boeing Company
IPC: B32B7/08 , B29C65/00 , B32B37/00 , B32B38/10 , F02F1/06 , B32B38/04 , A47L13/02 , A47L17/06 , A47L23/22 , F16B1/00 , F16B37/14 , A47L13/08 , B05C17/005 , B05C17/10 , B29C65/48 , B05C11/02 , B64D45/02 , F16B33/00
CPC classification number: A47L13/08 , B05C11/02 , B05C17/00503 , B05C17/10 , B29C65/48 , B29C66/032 , B64D45/02 , F16B33/004 , Y10T156/10 , Y10T156/17
Abstract: A method and apparatus for sealing a fastener element. A structure may be positioned over a seal cap that has been adhered and sealed to the fastener element. A number of projections associated with the structure may be moved along an interface formed between the seal cap and an object in which the fastener element has been installed such that the number of projections removes at least a portion of excess material around the seal cap while moving along the interface between the seal cap and the object.
Abstract translation: 一种用于密封紧固元件的方法和装置。 结构可以被定位在已经被粘附并密封到紧固件元件的密封帽上。 与结构相关联的多个突起可以沿着形成在密封帽和其中安装有紧固件元件的物体之间的界面移动，使得突起的数量在移动的同时移除密封盖周围的多余材料的至少一部分 沿着密封盖和物体之间的界面。
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