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公开(公告)号：US20220009638A1
公开(公告)日：2022-01-13
申请号：US16926437
申请日：2020-07-10
申请人： B/E AEROSPACE, INC.
发明人： Charles Zurian , Dean Sears , Lazaro Martinez , Richard Kelley
摘要： A system may include a surface, a pocket member, and spring members. The pocket member may have a top portion, a bottom portion, an exterior side, and an interior side. Each spring member may be positioned vertically between the surface and the interior side of the pocket member. Each spring member may have a spring top portion and a spring bottom portion. Each of the spring top portions may be attached to the top portion of the pocket member. Each of the spring bottom portions may be attached to the surface at a location corresponding to a vertical position of the bottom portion of the pocket member. The surface, the pocket member, and the spring members may form a pocket configured to at a given time be one of: open at the top portion of the pocket member, open at the bottom portion of the pocket member, or closed.
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公开(公告)号：US20210339870A1
公开(公告)日：2021-11-04
申请号：US17238011
申请日：2021-04-22
申请人： B/E Aerospace, Inc.
发明人： Ian L. Frost , Daniel I. Udriste , Charles Zurian , Mark Vaughan
摘要： An aircraft tray table may include a body with a defined interior cavity, a personal electronic device support, and a magnification lens. The personal electronic device support may be configured to hold a personal electronic device when the personal electronic device support is in a support deployed position. The magnification lens may be configured to fit within the interior cavity when the magnification lens is in a lens stowed position. The magnification lens may include a lens configured to magnify content displayed on the personal electronic device held by the personal electronic device support when the magnification lens is in a lens deployed position. The personal electronic device support may be parallel to the magnification lens when the personal electronic device is in the support deployed position and the magnification lens is in the lens deployed position.
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公开(公告)号：US12122520B2
公开(公告)日：2024-10-22
申请号：US18198065
申请日：2023-05-16
申请人： B/E Aerospace, Inc.
CPC分类号： B64D11/0647 , B60N2/7041 , B60N2/7058
摘要： A spring-based seat diaphragm may include at least one support diaphragm component. The at least one support diaphragm component may be transversely coupled to the first structural beam and the second structural beam. The spring-based seat diaphragm may include at least one spring. The at least one spring may be proximate to the at least one support diaphragm component. The at least one spring may be parallel to or positioned transverse to the at least one support diaphragm component between the first primary spreader and the second primary spreader. The at least one spring may include a plurality of bends configured to distribute user weight applied to a cushion installed on the aircraft seat over the spring-based seat diaphragm. The spring-based seat diaphragm may be configured to support an aft portion of the cushion. The first structural beam may be configured to support a forward portion of the cushion.
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公开(公告)号：US11192652B1
公开(公告)日：2021-12-07
申请号：US16931320
申请日：2020-07-16
申请人： B/E AEROSPACE, INC.
发明人： Daniel Udriste , Neil Ralph , Charles Zurian , Lazaro Martinez
摘要： A dress cover installable over a seatback of a passenger seat and having an integrated adjustable lumbar support device is disclosed. In embodiments, the dress cover includes a fabric outer shell and a seat cushion within the outer shell. The lumbar support device is disposed inside a pocket set into the dress cover and corresponding to the lumbar area of the seat occupant. The pocket extends laterally between left-side and right-side slots, each slot held closed by a zipper within which a slider tracks up and down to adjust the lumbar support device. As the slider tracks along the zipper it opens and closes the zipper within the body of the slider, maintaining its slot in a closed configuration. By adjusting the sliders up or down, the occupant may adjust the position of the lumbar support device through the dress cover.
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公开(公告)号：US11172765B1
公开(公告)日：2021-11-16
申请号：US17009444
申请日：2020-09-01
申请人： B/E Aerospace, Inc.
发明人： Charles Zurian
摘要： An aircraft seat may include a support system including a seat frame, a cushion including at least one surface configured to conform to a corresponding surface of the support system, a seat cover configured to fit over a portion of the cushion, and a seat cover attachment system configured to secure the seat cover to the seat frame. The seat cover attachment system may include a seat frame element of the seat frame. The seat cover attachment system may include a seat cover extrusion element configured to couple to the at least one seat frame element. The seat cover attachment system may include a seat cover retain element configured to couple to the seat cover extrusion element. A portion of the seat cover may be secured between the seat cover extrusion element and the seat cover retain element.
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公开(公告)号：US20230286656A1
公开(公告)日：2023-09-14
申请号：US18198065
申请日：2023-05-16
申请人： B/E Aerospace, Inc.
CPC分类号： B64D11/0647 , B60N2/7041 , B60N2/7058
摘要： A spring-based seat diaphragm may include at least one support diaphragm component. The at least one support diaphragm component may be transversely coupled to the first structural beam and the second structural beam. The spring-based seat diaphragm may include at least one spring. The at least one spring may be proximate to the at least one support diaphragm component. The at least one spring may be parallel to or positioned transverse to the at least one support diaphragm component between the first primary spreader and the second primary spreader. The at least one spring may include a plurality of bends configured to distribute user weight applied to a cushion installed on the aircraft seat over the spring-based seat diaphragm. The spring-based seat diaphragm may be configured to support an aft portion of the cushion. The first structural beam may be configured to support a forward portion of the cushion.
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公开(公告)号：US11691738B2
公开(公告)日：2023-07-04
申请号：US17121667
申请日：2020-12-14
申请人： B/E Aerospace, Inc.
CPC分类号： B64D11/0647 , B60N2/7041 , B60N2/7058
摘要： A spring-based seat diaphragm may include at least one support diaphragm component. The at least one support diaphragm component may be transversely coupled to the first structural beam and the second structural beam. The spring-based seat diaphragm may include at least one spring. The at least one spring may be proximate to the at least one support diaphragm component. The at least one spring may be parallel to or positioned transverse to the at least one support diaphragm component between the first primary spreader and the second primary spreader. The at least one spring may include a plurality of bends configured to distribute user weight applied to a cushion installed on the aircraft seat over the spring-based seat diaphragm. The spring-based seat diaphragm may be configured to support an aft portion of the cushion. The first structural beam may be configured to support a forward portion of the cushion.
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公开(公告)号：US11319075B1
公开(公告)日：2022-05-03
申请号：US17198120
申请日：2021-03-10
申请人： B/E Aerospace, Inc.
发明人： Jeremy F. Malecha , Charles Zurian
IPC分类号： B64D11/06
摘要： A compressible cushion may include a base structure and a plurality of foam layers positioned on a seat pan of the aircraft seat. The plurality of foam layers may include a first foam layer stacked on the base structure, and at least a second foam layer stacked on the first foam layer. A density of the at least a second foam layer may be less than a density of the first foam layer. The first foam layer and the at least a second foam layer may be cut at a length corresponding to a length of the seat pan when in an extended position. The first foam layer and the at least a second foam layer each may include a plurality of cuts, which may be configured to compress when the seat pan actuates between the extended position and a retracted position.
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公开(公告)号：US11952124B2
公开(公告)日：2024-04-09
申请号：US17238011
申请日：2021-04-22
申请人： B/E Aerospace, Inc.
发明人： Ian L. Frost , Daniel I. Udriste , Charles Zurian , Mark Vaughan
CPC分类号： B64D11/0638 , B64D11/00152
摘要： An aircraft tray table may include a body with a defined interior cavity, a personal electronic device support, and a magnification lens. The personal electronic device support may be configured to hold a personal electronic device when the personal electronic device support is in a support deployed position. The magnification lens may be configured to fit within the interior cavity when the magnification lens is in a lens stowed position. The magnification lens may include a lens configured to magnify content displayed on the personal electronic device held by the personal electronic device support when the magnification lens is in a lens deployed position. The personal electronic device support may be parallel to the magnification lens when the personal electronic device is in the support deployed position and the magnification lens is in the lens deployed position.
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公开(公告)号：US20220185482A1
公开(公告)日：2022-06-16
申请号：US17121667
申请日：2020-12-14
申请人： B/E Aerospace, Inc.
摘要： A spring-based seat diaphragm may include at least one support diaphragm component. The at least one support diaphragm component may be transversely coupled to the first structural beam and the second structural beam. The spring-based seat diaphragm may include at least one spring. The at least one spring may be proximate to the at least one support diaphragm component. The at least one spring may be parallel to or positioned transverse to the at least one support diaphragm component between the first primary spreader and the second primary spreader. The at least one spring may include a plurality of bends configured to distribute user weight applied to a cushion installed on the aircraft seat over the spring-based seat diaphragm. The spring-based seat diaphragm may be configured to support an aft portion of the cushion. The first structural beam may be configured to support a forward portion of the cushion.
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