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

Inventor： Steven A. Best ,  Jesse Randal Wiseman ,  Hugh Christopher VanValkenburgh ,  John R. Lowell

IPC: B64C1/26 ,  B64D37/08 ,  B64C3/34

CPC classification number: B64C1/26 ,  B64C3/34 ,  B64D37/08 ,  B64D37/32 ,  B64F5/10

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.

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

IPC: F16J15/00 ,  B64C3/00 ,  B64F5/00

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.

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

Inventor： Steven A. Best ,  Jesse Randal Wiseman ,  Hugh Christopher VanValkenburgh ,  John R. Lowell

IPC: B64C1/26 ,  B64C3/34 ,  B64D37/08 ,  B64F5/10 ,  B64D37/32

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.