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公开(公告)号：US09751609B2
公开(公告)日：2017-09-05
申请号：US15336397
申请日：2016-10-27
Applicant: The Boeing Company
Inventor： Thomas Perkins , Michael J. Olliges , Allan A. Loken , Hannah Rebecca Arm , Jeremy Ryan Glaze Tatum
CPC classification number: B64C1/069 , B32B3/06 , B64C1/18 , B64C2001/009 , B64F5/10 , Y10T428/24777
Abstract: A method of installing and replacing a plurality of decompression panels into a sidewall assembly of an aircraft includes coupling a first decompression panel to at least one of a sidewall and a floor panel of the sidewall assembly. The method also includes inserting a tab of the first decompression panel into a slot of a second decompression panel. The slot is defined by a flange extending along a surface of the second decompression panel. The method further includes coupling the second decompression panel to at least one of a sidewall and a floor panel of the sidewall assembly.
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公开(公告)号：US20150115102A1
公开(公告)日：2015-04-30
申请号：US14228524
申请日：2014-03-28
Applicant: The Boeing Company
Inventor： Thomas Perkins , Michael J. Olliges , Allan A. Loken , Hannah Rebecca Arm , Jeremy Ryan Glaze Tatum
CPC classification number: B64C1/069 , B32B3/06 , B64C1/18 , B64C2001/009 , B64F5/10 , Y10T428/24777
Abstract: A decompression panel includes a body portion having a first end and a second end opposing the first end. The decompression panel also includes a tab extending along the first end and a flange coupled to the body portion. The flange defines a slot adjacent the second end. The decompression panel is secured in an airplane cabin by the tab and slot features, such that unwanted access to areas behind such panels is prevented.
Abstract translation: 减压板包括主体部分，其具有第一端和与第一端相对的第二端。 减压面板还包括沿着第一端延伸的突出部和连接到主体部分的凸缘。 凸缘限定了与第二端相邻的槽。 减压板通过突片和槽特征固定在飞机机舱中，使得不期望地进入这些面板后面的区域。
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公开(公告)号：US10071795B2
公开(公告)日：2018-09-11
申请号：US14228492
申请日：2014-03-28
Applicant: The Boeing Company
Inventor： Thomas Perkins , Michael J. Olliges , Allan A. Loken , Hannah Rebecca Arm , Jeremy Ryan Glaze Tatum
CPC classification number: B64C1/18 , B64C2001/009 , B64D11/02 , F16B2/12 , F16B5/0635 , F16B5/0685 , Y10T29/49948 , Y10T403/7067
Abstract: A clamp device includes a clamp portion defining a threaded opening therein. The clamp portion is configured to contact a first side of a beam. The clamp device also includes a threaded fastener configured for insertion into the threaded opening via a hole defined within the decompression panel. The clamp device causes the decompression panel to contact a second side of the beam when the threaded fastener is tightened within the threaded opening.
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公开(公告)号：US09499251B2
公开(公告)日：2016-11-22
申请号：US14228524
申请日：2014-03-28
Applicant: The Boeing Company
Inventor： Thomas Perkins , Michael J. Olliges , Allan A. Loken , Hannah Rebecca Arm , Jeremy Ryan Glaze Tatum
CPC classification number: B64C1/069 , B32B3/06 , B64C1/18 , B64C2001/009 , B64F5/10 , Y10T428/24777
Abstract: A decompression panel includes a body portion having a first end and a second end opposing the first end. The decompression panel also includes a tab extending along the first end and a flange coupled to the body portion. The flange defines a slot adjacent the second end. The decompression panel is secured in an airplane cabin by the tab and slot features, such that unwanted access to areas behind such panels is prevented.
Abstract translation: 减压板包括主体部分，其具有第一端和与第一端相对的第二端。 减压面板还包括沿着第一端延伸的突出部和连接到主体部分的凸缘。 凸缘限定了与第二端相邻的槽。 减压板通过突片和槽特征固定在飞机机舱中，使得不期望地进入这些面板后面的区域。
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Patent Agency Ranking
公开(公告)号：US09566759B2
公开(公告)日：2017-02-14
申请号：US14471161
申请日：2014-08-28
Applicant: The Boeing Company
Inventor： Thomas Perkins , Jeremy Ryan Glaze Tatum , Allan A. Loken , Hannah Rebecca Arm
CPC classification number: B32B3/266 , B64C1/18 , B64C2001/009 , Y10T29/49622 , Y10T428/24273
Abstract: A decompression panel for use in an aircraft assembly that includes a body portion including a top edge and a bottom edge, and a front surface and a rear surface opposing the front surface. A plurality of openings are formed in the body portion, and a first stiffening member is formed on the rear surface below the plurality of openings. The first stiffening member extends from the rear surface towards the top edge such that the plurality of openings are at least partially obstructed by the first stiffening member.
Abstract translation: 一种用于飞机组件的减压板，包括：主体部分，其包括顶部边缘和底部边缘;以及前表面和与前表面相对的后表面。 多个开口形成在主体部分中，第一加强构件形成在多个开口下方的后表面上。 第一加强构件从后表面朝向顶部边缘延伸，使得多个开口至少部分地被第一加强构件阻挡。
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7.发明申请公开(公告)号：US20150117945A1
公开(公告)日：2015-04-30
申请号：US14228492
申请日：2014-03-28
Applicant: THE BOEING COMPANY
Inventor： Thomas Perkins , Michael J. Olliges , Allan A. Loken , Hannah Rebecca Arm , Jeremy Ryan Glaze Tatum
CPC classification number: B64C1/18 , B64C2001/009 , B64D11/02 , F16B2/12 , F16B5/0635 , F16B5/0685 , Y10T29/49948 , Y10T403/7067
Abstract: A clamp device includes a clamp portion defining a threaded opening therein. The clamp portion is configured to contact a first side of a beam. The clamp device also includes a threaded fastener configured for insertion into the threaded opening via a hole defined within the decompression panel. The clamp device causes the decompression panel to contact a second side of the beam when the threaded fastener is tightened within the threaded opening.
Abstract translation: 夹紧装置包括在其中限定螺纹开口的夹紧部分。 夹持部分构造成接触梁的第一侧。 夹紧装置还包括螺纹紧固件，该螺纹紧固件经由限定在减压板内的孔插入螺纹开口中。 当螺纹紧固件在螺纹开口内紧固时，夹紧装置使减压板接触梁的第二侧。
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公开(公告)号：US20150115103A1
公开(公告)日：2015-04-30
申请号：US14228576
申请日：2014-03-28
Applicant: The Boeing Company
Inventor： Thomas Perkins , Nicole Catherine Zarfos , Allan A. Loken , Michael J. Olliges , Jeremy Ryan Glaze Tatum
CPC classification number: B64C1/069 , B32B3/266 , B64C1/18 , B64C2001/009 , Y10T29/49995 , Y10T428/24273
Abstract: A decompression panel for use in an aircraft assembly is provided. The decompression panel includes a body portion including a top end and a bottom end, and an array of openings formed in the body portion. The openings in the array progressively decrease in size along a height of the body portion from the bottom end towards the top end.
Abstract translation: 提供了一种用于飞机组件的减压板。 减压板包括主体部分，其包括顶端和底端，以及形成在主体部分中的开口阵列。 阵列中的开口沿主体部分的高度从底端向顶端逐渐减小。
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公开(公告)号：USD817851S1
公开(公告)日：2018-05-15
申请号：US29586806
申请日：2016-12-07
Applicant: The Boeing Company
Designer： Thomas Perkins , Jeremy Ryan Glaze Tatum , Allan A. Loken , Hannah Rebecca Arm
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公开(公告)号：US20170043856A1
公开(公告)日：2017-02-16
申请号：US15336397
申请日：2016-10-27
Applicant: The Boeing Company
Inventor： Thomas Perkins , Michael J. Olliges , Allan A. Loken , Hannah Rebecca Arm , Jeremy Ryan Glaze Tatum
CPC classification number: B64C1/069 , B32B3/06 , B64C1/18 , B64C2001/009 , B64F5/10 , Y10T428/24777
Abstract: A method of installing and replacing a plurality of decompression panels into a sidewall assembly of an aircraft includes coupling a first decompression panel to at least one of a sidewall and a floor panel of the sidewall assembly. The method also includes inserting a tab of the first decompression panel into a slot of a second decompression panel. The slot is defined by a flange extending along a surface of the second decompression panel. The method further includes coupling the second decompression panel to at least one of a sidewall and a floor panel of the sidewall assembly.
Abstract translation: 将多个减压板安装和更换为飞行器的侧壁组件的方法包括将第一减压面板联接到侧壁组件的侧壁和底板中的至少一个。 该方法还包括将第一解压面板的突片插入第二减压板的槽中。 槽由沿着第二减压板的表面延伸的凸缘限定。 该方法还包括将第二减压面板耦合到侧壁组件的侧壁和底板中的至少一个。
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