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公开(公告)号：US20180194451A1
公开(公告)日：2018-07-12
申请号：US15405246
申请日：2017-01-12
Applicant: Bell Helicopter Textron Inc.
Inventor： Ross D. Cosby , Carl A. May , Richard Theodore Perryman , Michael Stephen Deslatte
CPC classification number: B64C1/20 , B64C1/12 , B64C1/22 , B64C2001/0072 , B64D11/0601 , B64D11/0696 , F16B2/12 , F16B5/01 , Y02T50/46
Abstract: In one embodiment, an apparatus may comprise an attachment device configured to be embedded in a structure, wherein the attachment device comprises: a body comprising a first flange and a second flange, wherein the body is configured such that the first flange and the second flange are coupled together internally within the body when the attachment device is embedded in the structure; an attachment fitting for coupling a component to the structure in which the attachment device is embedded.
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公开(公告)号：US09347473B2
公开(公告)日：2016-05-24
申请号：US14035031
申请日：2013-09-24
Applicant: BELL HELICOPTER TEXTRON INC.
Inventor： James D. Hethcock , Rodney H. Jones , Carl A. May
CPC classification number: F16B11/006 , F16B5/0266 , Y10T403/32991 , Y10T403/45 , Y10T403/47
Abstract: An apparatus for joining a first member and a second member includes fasteners for joining the first member and the second member, a shear transfer layer for transferring shear loads between the first member and the second member separate from the fasteners for joining the first member and the second member. An assembly includes a first member, a second member, and fasteners for joining the first member and the second member. The assembly further includes a shear transfer layer for transferring shear loads between the first member and the second member separate from the fasteners for joining the first member and the second.
Abstract translation: 用于接合第一构件和第二构件的装置包括用于接合第一构件和第二构件的紧固件，用于在第一构件和第二构件之间传递剪切载荷的剪切传递层，与用于接合第一构件和第二构件的紧固件分离， 第二名成员 组件包括第一构件，第二构件和用于接合第一构件和第二构件的紧固件。 组件还包括用于在第一构件和第二构件之间传递剪切载荷的剪切传递层，其与用于接合第一构件和第二构件的紧固件分开。
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公开(公告)号：US10933969B2
公开(公告)日：2021-03-02
申请号：US15405246
申请日：2017-01-12
Applicant: Bell Helicopter Textron Inc.
Inventor： Ross D. Cosby , Carl A. May , Richard Theodore Perryman , Michael Stephen Deslatte
Abstract: In one embodiment, an apparatus may comprise an attachment device configured to be embedded in a structure, wherein the attachment device comprises: a body comprising a first flange and a second flange, wherein the body is configured such that the first flange and the second flange are coupled together internally within the body when the attachment device is embedded in the structure; an attachment fitting for coupling a component to the structure in which the attachment device is embedded.
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公开(公告)号：US09038952B2
公开(公告)日：2015-05-26
申请号：US13744484
申请日：2013-01-18
Applicant: Bell Helicopter Textron Inc.
Inventor： William A. Amante , Carl A. May
CPC classification number: B61C1/00 , B64C1/00 , B64C1/1492 , B64C27/04
Abstract: According to one embodiment, a windshield attachment device for coupling a windshield to a body includes a fastener portion, a bolt, and an elastomeric load isolator. The fastener portion has an opening therethrough. The bolt is configured to extend through the opening of the fastener portion and couple the fastener portion to the body. The elastomeric load isolator surrounds at least a portion of the fastener portion and separating the fastener portion from the windshield.
Abstract translation: 根据一个实施例，用于将挡风玻璃联接到主体的挡风玻璃附接装置包括紧固件部分，螺栓和弹性体负载隔离器。 紧固件部分具有穿过其的开口。 螺栓构造成延伸穿过紧固件部分的开口并将紧固件部分联接到主体。 弹性体负载隔离器围绕紧固件部分的至少一部分并将紧固件部分与挡风玻璃分开。
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公开(公告)号：US20140077029A1
公开(公告)日：2014-03-20
申请号：US14088506
申请日：2013-11-25
Applicant: BELL HELICOPTER TEXTRON INC.
Inventor： William D. Dennison , Carl A. May
IPC: B64C5/02
CPC classification number: B64C5/02 , B64C1/26 , B64C27/04 , Y10T29/49716
Abstract: An easily removable and lightweight horizontal stabilizer configured to provide aerodynamic stability for a rotorcraft. The horizontal stabilizer comprising a spar removably coupled to a tailboom with a removable spar attachment means, the spar being located transversely through a tailboom opening and configured to provide structural support for at least a first horizontal airfoil and a second horizontal airfoil. The first and second horizontal airfoils are configured to fittingly receive the spar so that the spar fits at least partially inside the first and second horizontal airfoils. The first and second horizontal airfoils extend outboard from the tailboom to provide aerodynamic pitch stability.
Abstract translation: 一种易于拆卸和轻便的水平稳定器，其配置为为旋翼航空器提供空气动力学稳定性。 所述水平稳定器包括可拆卸地联接到具有可移除的翼梁连接装置的尾梁的翼梁，所述翼梁横向设置在尾梁开口处并且构造成为至少第一水平翼型件和第二水平翼型件提供结构支撑。 第一和第二水平翼型件构造成适合地接收翼梁，使得翼梁至少部分地配合在第一和第二水平翼型内。 第一和第二水平翼型件从尾翼向外延伸，以提供空气动力学俯仰稳定性。
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Patent Agency Ranking
公开(公告)号：US20140023431A1
公开(公告)日：2014-01-23
申请号：US14035031
申请日：2013-09-24
Applicant: Bell Helicopter Textron Inc.
Inventor： James D. Hethcock , Rodney H. Jones , Carl A. May
IPC: F16B11/00
CPC classification number: F16B11/006 , F16B5/0266 , Y10T403/32991 , Y10T403/45 , Y10T403/47
Abstract: An apparatus for joining a first member and a second member includes means for joining the first member and the second member, means for transferring shear loads between the first member and the second member separate from the means for joining the first member and the second member, and means for providing a compression preload to the means for transferring shear loads between the first member and the second member. An assembly includes a first member, a second member, and means for joining the first member and the second member. The assembly further includes means for transferring shear loads between the first member and the second member separate from the means for joining the first member and the second member and means for providing a compression preload to the means for transferring shear loads between the first member and the second member.
Abstract translation: 一种用于接合第一构件和第二构件的装置包括用于接合第一构件和第二构件的装置，用于在第一构件和第二构件之间传递剪切载荷的装置与用于接合第一构件和第二构件的装置分离， 以及用于向所述用于在所述第一构件和所述第二构件之间传递剪切载荷的装置提供压缩预载荷的装置。 组件包括第一构件，第二构件和用于接合第一构件和第二构件的装置。 组件还包括用于在第一构件和第二构件之间传递剪切载荷的装置，其与用于接合第一构件和第二构件的装置分开，以及用于向第一构件和第二构件之间传递剪切载荷的装置提供压缩预载荷的装置 第二名成员
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公开(公告)号：US10513324B2
公开(公告)日：2019-12-24
申请号：US15424095
申请日：2017-02-03
Applicant: Bell Helicopter Textron Inc.
Inventor： David G. Carlson , John R. McCullough , Paul K. Oldroyd , Carl A. May , James E. Kooiman
Abstract: In one aspect, there is a rib assembly for an aircraft wing including a rib web having a top and a bottom, the rib web includes a first laminate, a second laminate, and a honeycomb panel having an array of large cells disposed between the first laminate and the second laminate, each cell having a width of at least 1 cm; and a plurality of skin flanges for fixedly attaching the rib web to a skin of the wing, each skin flange has a base member having a first portion and a second portion and a vertical member extending from the base member. The plurality of skin flanges can be attached to the top and the bottom of the rib web such that the second portion of the base member and the vertical member are attached to the rib web.
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公开(公告)号：US20180194473A1
公开(公告)日：2018-07-12
申请号：US15405284
申请日：2017-01-12
Applicant: Bell Helicopter Textron Inc.
Inventor： Joshua Emrich , Ross D. Cosby , Carl A. May , Richard Theodore Perryman
CPC classification number: B64D11/064 , B64C1/18 , B64C27/00 , B64C27/04 , B64D11/0601 , B64D11/0639 , B64D11/0696 , B64D25/04 , Y02T50/46
Abstract: In one embodiment, an apparatus may comprise: a floor panel for a rotorcraft; and a plurality of passenger seats coupled to the floor panel, wherein: the plurality of passenger seats is arranged into a plurality of seating rows; and the plurality of passenger seats comprises one or more foldover seats arranged to facilitate access to one or more exits of the rotorcraft.
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公开(公告)号：US20170225766A1
公开(公告)日：2017-08-10
申请号：US15424095
申请日：2017-02-03
Applicant: Bell Helicopter Textron Inc.
Inventor： David G. Carlson , John R. McCullough , Paul K. Oldroyd , Carl A. May , James E. Kooiman
Abstract: In one aspect, there is a rib assembly for an aircraft wing including a rib web having a top and a bottom, the rib web includes a first laminate, a second laminate, and a honeycomb panel having an array of large cells disposed between the first laminate and the second laminate, each cell having a width of at least 1 cm; and a plurality of skin flanges for fixedly attaching the rib web to a skin of the wing, each skin flange has a base member having a first portion and a second portion and a vertical member extending from the base member. The plurality of skin flanges can be attached to the top and the bottom of the rib web such that the second portion of the base member and the vertical member are attached to the rib web.
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公开(公告)号：US08882031B2
公开(公告)日：2014-11-11
申请号：US14088506
申请日：2013-11-25
Applicant: Bell Helicopter Textron Inc.
Inventor： William D. Dennison , Carl A. May
CPC classification number: B64C5/02 , B64C1/26 , B64C27/04 , Y10T29/49716
Abstract: An easily removable and lightweight horizontal stabilizer configured to provide aerodynamic stability for a rotorcraft. The horizontal stabilizer comprising a spar removably coupled to a tailboom with a removable spar attachment means, the spar being located transversely through a tailboom opening and configured to provide structural support for at least a first horizontal airfoil and a second horizontal airfoil. The first and second horizontal airfoils are configured to fittingly receive the spar so that the spar fits at least partially inside the first and second horizontal airfoils. The first and second horizontal airfoils extend outboard from the tailboom to provide aerodynamic pitch stability.
Abstract translation: 一种易于拆卸和轻便的水平稳定器，其配置为为旋翼航空器提供空气动力学稳定性。 所述水平稳定器包括可拆卸地联接到具有可移除的翼梁连接装置的尾梁的翼梁，所述翼梁横向设置在尾梁开口处并且构造成为至少第一水平翼型件和第二水平翼型件提供结构支撑。 第一和第二水平翼型件构造成适合地接收翼梁，使得翼梁至少部分地配合在第一和第二水平翼型内。 第一和第二水平翼型件从尾翼向外延伸，以提供空气动力学俯仰稳定性。
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