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公开(公告)号：US10414480B2
公开(公告)日：2019-09-17
申请号：US16177006
申请日：2018-10-31
申请人： The Boeing Company
摘要： Systems and methods are provided for securing aircraft sidewall. One embodiment comprises a hanger for supporting sections of sidewall for an aircraft. The hanger includes an elongated vertical member that attaches to a frame of the aircraft, and sets of keyholes that are each arranged in a vertical pattern along the member and that are each configured to support a corresponding section of sidewall of the aircraft. Each keyhole includes a receptacle dimensioned to receive a fitting from a section of sidewall, and a slot dimensioned to slidably accept the fitting via the receptacle to secure the fitting in place. The slot size of keyholes in each set varies from one end of the vertical pattern to another end of the vertical pattern.
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公开(公告)号：US11370562B2
公开(公告)日：2022-06-28
申请号：US16598179
申请日：2019-10-10
申请人： The Boeing Company
发明人： Cory M. Hitchcock
摘要： Examples include an apparatus for providing a point of attachment to a structural component, the apparatus including: a first grommet comprising: a head; and a shaft that extends from a first side of the head, where the shaft comprises a first attachment component opposite the head; a gasket bonded to a second side of the head that is opposite the first side, where the gasket, the head, and the shaft are aligned and a hole is formed through the gasket, the head, and the shaft; and a second grommet comprising a second attachment component that is configured to engage the first attachment component of the first grommet.
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公开(公告)号：US10737756B2
公开(公告)日：2020-08-11
申请号：US15293064
申请日：2016-10-13
申请人： THE BOEING COMPANY
摘要： A moisture control apparatus for use with a structure within an aircraft, the structure including an upper surface, the moisture control apparatus comprising: a moisture absorbing layer including a moisture absorbing material, the layer including a leading edge, a trailing edge, side edges, an upper surface, and, a lower surface; and, a reverse-bevel defined along the leading edge of the layer, wherein the reverse-bevel and the upper surface of the structure define a gutter configured to retain moisture flowing along the upper surface of the structure.
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公开(公告)号：US20190106191A1
公开(公告)日：2019-04-11
申请号：US15729742
申请日：2017-10-11
申请人： The Boeing Company
IPC分类号： B64C1/06
摘要： Devices and methods to control moisture at a support member in a vehicle. The devices are configured to be attached to the support member and include a moisture absorbing portion and an evaporative portion. Methods of assembling the support member in the vehicle include prefabricating the device and preassembling the device onto the support member prior to the support member being installed in the vehicle.
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公开(公告)号：US10737755B2
公开(公告)日：2020-08-11
申请号：US15293005
申请日：2016-10-13
申请人： THE BOEING COMPANY
发明人： Cory M. Hitchcock
摘要： A moisture control apparatus for use with a structure within an aircraft fuselage, the structure including an upper surface, the apparatus comprising: a moisture absorbing layer including a moisture absorbing material, the layer including a leading edge, a trailing edge, side edges, an upper surface, and, a lower surface; and, a wicking layer disposed in fluid communication with the lower surface of the moisture absorbing layer, the wicking layer including a wicking layer leading edge, a wicking layer trailing edge and a wicking layer upper surface configured for capillary action of moisture from the wicking layer trailing edge towards the wicking layer leading edge, wherein the wicking layer leading edge is offset from the leading edge of the moisture absorbing layer such that an offset portion of the wicking layer is exposed to air to facilitate evaporation of the moisture.
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公开(公告)号：US20190071162A1
公开(公告)日：2019-03-07
申请号：US16177006
申请日：2018-10-31
申请人： The Boeing Company
摘要： Systems and methods are provided for securing aircraft sidewall. One embodiment comprises a hanger for supporting sections of sidewall for an aircraft. The hanger includes an elongated vertical member that attaches to a frame of the aircraft, and sets of keyholes that are each arranged in a vertical pattern along the member and that are each configured to support a corresponding section of sidewall of the aircraft. Each keyhole includes a receptacle dimensioned to receive a fitting from a section of sidewall, and a slot dimensioned to slidably accept the fitting via the receptacle to secure the fitting in place. The slot size of keyholes in each set varies from one end of the vertical pattern to another end of the vertical pattern.
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公开(公告)号：US10137975B2
公开(公告)日：2018-11-27
申请号：US15091962
申请日：2016-04-06
申请人： The Boeing Company
摘要： Systems and methods are provided for securing aircraft sidewall. One embodiment comprises a hanger for supporting sections of sidewall for an aircraft. The hanger includes an elongated vertical member that attaches to a frame of the aircraft, and sets of keyholes that are each arranged in a vertical pattern along the member and that are each configured to support a corresponding section of sidewall of the aircraft. Each keyhole includes a receptacle dimensioned to receive a fitting from a section of sidewall, and a slot dimensioned to slidably accept the fitting via the receptacle to secure the fitting in place. The slot size of keyholes in each set varies from one end of the vertical pattern to another end of the vertical pattern.
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公开(公告)号：US20170291725A1
公开(公告)日：2017-10-12
申请号：US15092428
申请日：2016-04-06
申请人： The Boeing Company
发明人： Ryan Nelson Marcelo Abelon , Cory M. Hitchcock , Toai Dac Tran , Thomas Ralph Smith, JR. , Jon Burton Shaw
CPC分类号： B64F5/50 , B64D2011/0046 , B64F5/10 , Y02T50/46
摘要： A method of protecting a monument during manufacturing of a vehicle. The method includes attaching a plurality of brackets to the monument prior to installation in the vehicle, each of the plurality of brackets having corresponding fasteners facing outwardly relative to the monument. The method also includes connecting a blanket to the corresponding fasteners. The method also includes installing the monument in the vehicle, disconnecting the blanket, and removing the plurality of brackets from the monument.
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公开(公告)号：US11072411B2
公开(公告)日：2021-07-27
申请号：US15729742
申请日：2017-10-11
申请人： The Boeing Company
摘要： Devices and methods to control moisture at a support member in a vehicle. The devices are configured to be attached to the support member and include a moisture absorbing portion and an evaporative portion. Methods of assembling the support member in the vehicle include prefabricating the device and preassembling the device onto the support member prior to the support member being installed in the vehicle.
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公开(公告)号：US20210107686A1
公开(公告)日：2021-04-15
申请号：US16598179
申请日：2019-10-10
申请人： The Boeing Company
发明人： Cory M. Hitchcock
摘要： Examples include an apparatus for providing a point of attachment to a structural component, the apparatus including: a first grommet comprising: a head; and a shaft that extends from a first side of the head, where the shaft comprises a first attachment component opposite the head; a gasket bonded to a second side of the head that is opposite the first side, where the gasket, the head, and the shaft are aligned and a hole is formed through the gasket, the head, and the shaft; and a second grommet comprising a second attachment component that is configured to engage the first attachment component of the first grommet.
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