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11.发明授权公开(公告)号：US09440744B2
公开(公告)日：2016-09-13
申请号：US14228554
申请日：2014-03-28
Applicant: THE BOEING COMPANY
Inventor： Thomas Seth Perkins , Allan A. Loken , Robert J. Christian , James Pease , Sara Beth Cromyak
CPC classification number: B64D13/00 , B64C1/18 , B64C2001/009
Abstract: Decompression panel assemblies and methods of equalizing air pressure differential are provided. The decompression panel assembly includes a panel comprising an opening defined therein, a vent cover coupled across the opening, and a latching mechanism. The vent cover is configured to move between a first position and a second position. The latching mechanism is configured to maintain the vent cover in the first position when a pressure differential across the panel is below a predetermined value and facilitate the vent cover moving to the second position when the pressure differential across the panel exceeds the predetermined value.
Abstract translation: 提供减压板组件和均压气压差的方法。 减压面板组件包括包括限定在其中的开口的面板，跨过开口连接的通气盖以及闭锁机构。 通气盖构造成在第一位置和第二位置之间移动。 闭锁机构构造成当跨越面板的压差低于预定值时将通气盖保持在第一位置，并且当跨越面板的压力差超过预定值时，便于通气盖运动到第二位置。
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公开(公告)号：US09233747B2
公开(公告)日：2016-01-12
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 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: 用于飞行器组件的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：US20150115104A1
公开(公告)日：2015-04-30
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 is provided. The decompression panel 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: 提供了一种用于飞机组件的减压板。 减压板包括主体部分，其包括顶部边缘和底部边缘，以及与前表面相对的前表面和后表面。 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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14.发明申请公开(公告)号：US20150108274A1
公开(公告)日：2015-04-23
申请号：US14228554
申请日：2014-03-28
Applicant: THE BOEING COMPANY
Inventor： Thomas Seth Perkins , Allan A. Loken , Robert J. Christian , James Pease , Sara Beth Cromyak
IPC: B64D13/00
CPC classification number: B64D13/00 , B64C1/18 , B64C2001/009
Abstract: Decompression panel assemblies and methods of equalizing air pressure differential are provided. The decompression panel assembly includes a panel comprising an opening defined therein, a vent cover coupled across the opening, and a latching mechanism. The vent cover is configured to move between a first position and a second position. The latching mechanism is configured to maintain the vent cover in the first position when a pressure differential across the panel is below a predetermined value and facilitate the vent cover moving to the second position when the pressure differential across the panel exceeds the predetermined value.
Abstract translation: 提供减压板组件和均压气压差的方法。 减压面板组件包括包括限定在其中的开口的面板，跨过开口连接的通气盖以及闭锁机构。 通气盖构造成在第一位置和第二位置之间移动。 闭锁机构构造成当跨越面板的压差低于预定值时将通气盖保持在第一位置，并且当跨越面板的压力差超过预定值时，便于通气盖运动到第二位置。
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