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公开(公告)号：US10301033B2
公开(公告)日：2019-05-28
申请号：US15275338
申请日：2016-09-24
Applicant: The Boeing Company
Inventor： Kevin O'Brien Gaw
Abstract: A fuel tank system comprising a fuel tank, a number of fasteners, and a number of covers. The number of fasteners has a number of ends extending into an interior of the fuel tank. The number of covers is configured to cover the number of ends of the number of fasteners. A cover in the number of covers comprises a housing configured to cover an end of a fastener in the number of ends, a deformable material associated with an interior side of the cover, and cells that are present within the deformable material. The deformable material is configured to contain energy within the cover in which the energy is caused by an electromagnetic event.
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公开(公告)号：US20180056554A1
公开(公告)日：2018-03-01
申请号：US15250297
申请日：2016-08-29
Applicant: THE BOEING COMPANY
Inventor： Kevin O'Brien Gaw , Michael A. Nill , Gary Anthony Booker , Stephen Dark , Laura Fournier , Randy J. Grove , David John Barene , Jeston Lingelbach , Kory Shaffer , David W. Foutch , Michael H. Larson
Abstract: A compression molding assembly for molding a honeycomb core, including a plurality of cells defined by a plurality of walls, of a blocker door is provided. The compression molding assembly includes a ram plate comprising a plurality of openings defined therethrough and a plurality of core inserts coupled to the ram plate such that the plurality of core inserts are configured to form the honeycomb core of the blocker door. Each core insert is removably coupled with a respective opening of the plurality of openings such that each core insert is configured to form a respective cell of the plurality of cells.
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公开(公告)号：US10406729B2
公开(公告)日：2019-09-10
申请号：US15250297
申请日：2016-08-29
Applicant: THE BOEING COMPANY
Inventor： Kevin O'Brien Gaw , Michael A. Nill , Garry Anthony Booker , Stephen R. Dark , Laura Fournier , Randy J. Grove , David John Barene , Jeston Lingelbach , Kory Shaffer , David W. Foutch , Michael H. Larson
IPC: B29C43/36 , B29C43/18 , B29C43/50 , B29C33/00 , B29C33/30 , B29D99/00 , F02K1/00 , F02K1/72 , B29K101/12 , B29L31/00 , B29C33/44 , B29L31/60 , B64D29/00
Abstract: A compression molding assembly for molding a honeycomb core, including a plurality of cells defined by a plurality of walls, of a blocker door is provided. The compression molding assembly includes a ram plate comprising a plurality of openings defined therethrough and a plurality of core inserts coupled to the ram plate such that the plurality of core inserts are configured to form the honeycomb core of the blocker door. Each core insert is removably coupled with a respective opening of the plurality of openings such that each core insert is configured to form a respective cell of the plurality of cells.
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公开(公告)号：US20180058373A1
公开(公告)日：2018-03-01
申请号：US15250253
申请日：2016-08-29
Applicant: THE BOEING COMPANY
Inventor： Kevin O'Brien Gaw , Dylan E. Jones , Michael H. Larson , Belur N. Shivashankara , Randy J. Grove , David John Barene , Jeston Lingelbach , Kory Shaffer , David W. Foutch
Abstract: A blocker door assembly for use in a gas turbine engine includes a facesheet including a plurality of openings to facilitate noise attenuation and a body portion coupled to the facesheet. The body portion includes a backsheet integrally formed with a honeycomb core, wherein the body portion is molded from a thermoplastic material.
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公开(公告)号：US20160167092A1
公开(公告)日：2016-06-16
申请号：US14570870
申请日：2014-12-15
Applicant: The Boeing Company
Inventor： Kevin O'Brien Gaw
Abstract: A system for electrostatically cleaning surfaces includes an electrostatically chargeable brush, having conductive polymer bristles, moveably disposed adjacent to a solid surface to be cleaned. The system also includes an actuator, configured to linearly move a solid element toward and through sliding contact along the solid surface, the brush being positioned to contact at least one of the solid surface and the solid element prior to the sliding contact, to electrostatically remove dust and the like therefrom.
Abstract translation: 用于静电清洁表面的系统包括具有导电聚合物刷毛的静电电荷刷，可移动地设置成与要清洁的固体表面相邻。 该系统还包括致动器，其构造成沿着固体表面线性地移动固体元件并穿过滑动触点，刷子定位成在滑动接触之前接触固体表面和固体元件中的至少一个，以静电除去 灰尘等。
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Patent Agency Ranking
公开(公告)号：US09169029B2
公开(公告)日：2015-10-27
申请号：US13747732
申请日：2013-01-23
Applicant: The Boeing Company
Inventor： Kevin O'Brien Gaw , Nathan Michael Kelley , John Thomas Axtell , James Patrick Irwin , David William Minteer , Diego A. Velasco
CPC classification number: B64D45/02 , B60R16/06 , B63B43/00 , F16L9/14 , F16L21/065 , F16L25/01 , F16L25/025 , F16L25/026 , F17D1/00 , F17D5/08 , H05F1/00 , Y10T137/8593
Abstract: A method and apparatus for conducting an electrical current between a first transport member and a second transport member. In one illustrative embodiment, a coupling assembly comprises a first fitting associated with a first end of a first transport member, a second fitting associated with a second end of a second transport member, and a seal. The seal is configured for placement around the first fitting and the second fitting when the first end of the first transport member is positioned relative to the second end of the second transport member. The seal is further configured to seal an interface between the first transport member and the second transport member. The seal is comprised of a material configured such that the seal has a level of conductivity within a selected range and such that a conductive pathway is formed between the first transport member and the second transport member.
Abstract translation: 一种用于在第一输送构件和第二输送构件之间进行电流的方法和装置。 在一个说明性实施例中，联接组件包括与第一输送构件的第一端相关联的第一配件，与第二输送构件的第二端相关联的第二配件和密封件。 当第一输送构件的第一端相对于第二输送构件的第二端定位时，密封件构造成围绕第一配件和第二配件放置。 密封件进一步构造成密封第一输送构件和第二输送构件之间的界面。 密封件由构造成使得密封件具有在所选范围内的导电率水平并且使得在第一输送构件和第二输送构件之间形成导电通路的材料构成。
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公开(公告)号：US11613680B2
公开(公告)日：2023-03-28
申请号：US16570935
申请日：2019-09-13
Applicant: The Boeing Company
Inventor： Kevin O'Brien Gaw , James Daniel Whitt , Erdal Bayseckin , Robert Francis McDevitt
IPC: C09J167/00 , C09J5/00 , C09J175/04 , C09J163/00 , C09J7/10 , C09J7/22 , B32B37/12 , B32B37/00 , B32B38/10
Abstract: A method of applying an adhesive to a non-planar surface. The method includes providing a segmented film adhesive. The segmented film adhesive comprises: (i) a liner; and (ii) an adhesive layer on the liner, the adhesive layer comprising a plurality of contiguous, discrete adhesive segments. The segmented film adhesive is positioned on a non-planar surface of a first adherend so that a first portion of the discrete adhesive segments are in contact with the non-planar surface and a second portion of the discrete adhesive segments are not in contact with the non-planar surface. The liner is removed from the non-planar surface, wherein only the first portion of the discrete adhesive segments remain on the non-planar surface of the first adherend.
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公开(公告)号：US10538019B2
公开(公告)日：2020-01-21
申请号：US14720071
申请日：2015-05-22
Applicant: The Boeing Company
Inventor： Kevin O'Brien Gaw , Michael Harris Larson
IPC: B29C43/36 , C09D179/08 , B29C43/02 , B29L23/00
Abstract: The surface of a tooling insert is coated with a polymer layer having a low surface energy in order to cover surface irregularities and thereby provide a smooth surface against which a composite part may be compression molded.
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9.发明申请公开(公告)号：US20200010745A1
公开(公告)日：2020-01-09
申请号：US16570935
申请日：2019-09-13
Applicant: The Boeing Company
Inventor： Kevin O'Brien Gaw , James Daniel Whitt , Erdal Bayseckin , Robert Francis McDevitt
IPC: C09J167/00 , C09J5/00 , C09J175/04 , C09J163/00
Abstract: A method of applying an adhesive to a non-planar surface. The method includes providing a segmented film adhesive. The segmented film adhesive comprises: (i) a liner; and (ii) an adhesive layer on the liner, the adhesive layer comprising a plurality of contiguous, discrete adhesive segments. The segmented film adhesive is positioned on a non-planar surface of a first adherend so that a first portion of the discrete adhesive segments are in contact with the non-planar surface and a second portion of the discrete adhesive segments are not in contact with the non-planar surface. The liner is removed from the non-planar surface, wherein only the first portion of the discrete adhesive segments remain on the non-planar surface of the first adherend.
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10.发明申请公开(公告)号：US20180112108A1
公开(公告)日：2018-04-26
申请号：US15299020
申请日：2016-10-20
Applicant: The Boeing Company
Inventor： Kevin O'Brien Gaw , James Daniel Whitt , Erdal Bayseckin , Robert Francis McDevitt
IPC: C09J7/02 , C09J5/00 , C09J175/04 , C09J163/00 , C09J167/00
CPC classification number: C09J167/00 , C08G2170/40 , C09J5/00 , C09J7/10 , C09J7/22 , C09J163/00 , C09J175/04 , C09J2201/28 , C09J2201/606 , C09J2400/283 , C09J2463/00 , C09J2467/00 , C09J2475/00
Abstract: A segmented film adhesive comprises a liner having a first major surface and a second major surface opposing the first major surface. An adhesive layer is on the liner. The adhesive layer comprises a plurality of contiguous, discrete adhesive segments on the first major surface of the liner.
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