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101. 发明授权

US06241188B1 Aircraft seats 有权
标题翻译：飞机座椅
公开(公告)号：US06241188B1
公开(公告)日：2001-06-05
申请号：US09324215
申请日：1999-06-02
申请人： Leslie James Simpson , Geoffrey Harcourt
发明人： Leslie James Simpson , Geoffrey Harcourt
IPC分类号： B64D2504
CPC分类号： B64D11/0638 , B60N2/6027 , B60N2/7005 , B60N3/004 , B64D11/06 , B64D11/0647 , B64D11/0649
摘要： An aircraft seat has a frame assembly onto which is attached a shaped front cover by means of clips, each having a socket component and a plug component. The plug and socket components are repeatedly engageable and disengageable, enabling the front cover to be repeatedly removed from and refitted to the frame assembly, for example for cleaning of the front cover. The clips ensure accurate and precise fitting and location of the seat cover with respect to the frame assembly.
摘要翻译：飞机座椅具有框架组件，通过夹具将成形的前盖连接到框架组件上，每个夹具具有插座部件和插头部件。插头和插座部件可重复地接合和脱离接合，使得前盖能够被重复地从框架组件移除并重新安装到框架组件上，例如用于清洁前盖。夹子确保座椅盖相对于框架组件的准确和精确的配合和定位。

102. 发明授权

US5921629A Aircraft divan 失效
标题翻译：飞机沙发
公开(公告)号：US5921629A
公开(公告)日：1999-07-13
申请号：US840431
申请日：1997-04-29
申请人： Roger Koch , Michael L. Oleson , Daryl Soderman
发明人： Roger Koch , Michael L. Oleson , Daryl Soderman
IPC分类号： B64D11/06 , A47C5/04 , A47C7/02 , B60N2/04
CPC分类号： B64D11/0696 , B64D11/06 , B64D11/0649 , Y02T50/46
摘要： An aircraft divan, for use within a passenger compartment of an aircraft, that includes a strong rigid base structure adapted to be secured to a support surface within the aircraft and including a plurality of substantially strong, yet lightweight frame members. A plurality of substantially strong, yet lightweight connectors, each one of the connectors being structured and disposed to connectingly receive at least two of the frame members, including an exterior wall structure defining at least one interior cavity and at least two frame member receiving openings, and comprising a first interlocking segment and a second interlocking segment, the first interlocking segment structured to at least partially receive the second interlocking segment and the first and second interlocking segments being structured to be interlockingly connected with one another in sandwiching relation about at least one end zone of the frame members. Moreover, each of the frame member receiving openings is structured and disposed to receive and surround one of the end zones of one of the frame members therethrough and to maintain the end zone of the frame member fastened in a secured, fixed position within the interior cavity of the connector.
摘要翻译：用于在飞行器的乘客舱内使用的飞机沙发，其包括适于固定到飞行器内的支撑表面的强刚性基座结构，并且包括多个基本坚固且轻便的框架构件。多个基本上坚固且轻便的连接器，每个连接器被构造和设置成连接地容纳至少两个框架构件，包括限定至少一个内腔和至少两个框架构件接收开口的外壁结构，并且包括第一互锁段和第二互锁段，所述第一互锁段被构造成至少部分地接收所述第二互锁段，并且所述第一和第二互锁段被构造成彼此互锁地连接，框架成员的区域。此外，每个框架构件接收开口被构造和设置成容纳和围绕一个框架构件的一个端部区域通过其中，并且将框架构件的端部区域固定在内部空腔内的固定的固定位置的连接器。

103. 发明授权

US5836547A Attenuated seat back assembly for an aircraft passenger seat 失效
标题翻译：用于飞机乘客座椅的减震座椅靠背组件
公开(公告)号：US5836547A
公开(公告)日：1998-11-17
申请号：US630009
申请日：1996-04-08
申请人： Roger Koch , Ronald Grilliot , Mark Larson
发明人： Roger Koch , Ronald Grilliot , Mark Larson
IPC分类号： B60N2/42 , B60R21/04 , B64D11/06 , B64D25/04 , B60R21/055 , B64D25/00
CPC分类号： B64D11/0619 , B60N2/4221 , B60N2/4249 , B64D11/06 , B64D11/0649 , B64D25/04 , B60R21/04
摘要： An attenuated aircraft seat back assembly for use on an aircraft passenger seat of the type which includes a seat back frame with a front side and a rear side, the attenuated assembly comprising a mount assembly structured to be secured at the rear side of the seat back frame, preferably at an upper end thereof, and an impact absorbent, generally rigid material panel fixedly secured thereto. The mount assembly is structured to securely maintain the rigid material panel in a generally parallel orientation relative to the seat back frame, and spaced apart from the seat back frame by a predetermined distance. The rigid material panel, which is sized and configured to shield an upper region of the seat back frame, is substantially lightweight and includes a honeycomb interior core structured and disposed to substantially resist the force of a direct impact thereto, while still yielding sufficiently so that an object impacting the rigid material panel will have a Head Injury Criteria (HIC) value which is acceptable under current Federal Aviation Administration regulations. Preferably, an energy absorbent, resilient material panel is adhered to a front face of the rigid material panel, and together have a combined thickness of generally about two inches, while being spaced apart from the seat back frame in assembled form so as to minimize an overall thickness of the assembly.
摘要翻译：一种用于在包括具有前侧和后侧的座椅靠背框架的类型的飞机乘客座椅上的减弱的飞行器座椅靠背组件，所述减弱组件包括安装组件，该安装组件构造成固定在座椅靠背的后侧框架，优选地在其上端，以及抗冲击吸收剂，通常为刚性的材料面板固定地固定到其上。安装组件构造成将刚性材料面板相对于座椅靠背框架以大致平行的方向牢固地保持，并且与座椅靠背框架隔开预定距离。尺寸和构造以屏蔽座椅靠背框架的上部区域的刚性材料面板基本上是轻质的，并且包括被构造和设置为基本上抵抗直接冲击力的蜂窝内部芯，同时仍充分产生，使得影响刚性材料面板的物体将具有头部损伤标准（HIC）值，这在当前的联邦航空管理局法规中是可以接受的。优选地，吸收能量的弹性材料板粘附到刚性材料板的前表面，并且一起具有大致约2英寸的组合厚度，同时以组装的形式与座椅靠背框架间隔开，以便最小化组件的总厚度。

104. 发明授权

US5743592A Leg for an aircraft seat, a leg assembly including such a leg, and a seat including such a leg assembly 失效
标题翻译：用于飞机座椅的腿部，包括这种腿部的腿部组件和包括这种腿部组件的座椅
公开(公告)号：US5743592A
公开(公告)日：1998-04-28
申请号：US655567
申请日：1996-05-30
申请人： Pierre-Francois Bedouch
发明人： Pierre-Francois Bedouch
IPC分类号： B64D11/06 , B64D25/04 , B60N2/42
CPC分类号： B64D11/0619 , B64D11/06 , B64D11/0649 , B64D11/0696 , B64D25/04 , Y02T50/46
摘要： A leg for the leg assembly of an aircraft seat presents over at least a portion of its length, at least one segment whose cross-section has at least a portion that is generally U-shaped defined by a web extending in a transverse direction and two flanges extending in a longitudinal direction, the opening of the U-shape facing in a longitudinal direction, said segment serving to contribute to absorbing energy.
摘要翻译：用于飞行器座椅的腿部组件的腿在其长度的至少一部分上呈现，至少一个部分的横截面具有至少一部分，该部分大致为U形，该部分由沿横向方向延伸的腹板限定，沿纵向方向延伸的凸缘，U形开口沿纵向方向，所述段用于吸收能量。

105. 发明授权

US5636901A Aircraft passenger seat frame 失效
标题翻译：飞机乘客座椅框架
公开(公告)号：US5636901A
公开(公告)日：1997-06-10
申请号：US490791
申请日：1995-06-15
申请人： Ronald Grilliot , Patrick Murphy
发明人： Ronald Grilliot , Patrick Murphy
IPC分类号： B60N2/015 , B60N2/68 , B64D11/06 , A47C7/02
CPC分类号： B60N2/68 , B60N2/015 , B64D11/06 , B64D11/0649 , Y02T50/46
摘要： An aircraft seat frame including a seat back portion, a seat foundation portion, and a seat base portion, the seat back portion having a pair of generally vertically disposed side rails composed of three interconnected segments, a leading and a trailing edge segments of which are perpendicularly disposed on opposing sides of an interior segment, thereby substantially minimizing an overall weight of the side rails and maximizing the side rails resistance to horizontal bending across a plane of the leading and trailing segments. Further, the seat frame includes a load transference member spanning the side rails so as to evenly distribute a load exerted on only a single of the side rails over both side rails and over the corresponding seat side rails to which the seat back side rails are connected. Further, the frame includes a seat base portion having a pair of seat side rails with support members pivotally secured at opposite ends thereof, the support members being fixedly secured to an underlying support surface.
摘要翻译：一种包括座椅靠背部分，座椅基座部分和座椅底座部分的飞行器座椅框架，座椅靠背部分具有由三个互连的段组成的一对大致垂直设置的侧轨，其前缘和后缘段垂直地布置在内部段的相对侧上，从而基本上最小化侧轨的总体重量并最大化侧轨对跨越前段和后段的平面的水平弯曲的抵抗力。此外，座椅框架包括跨越侧轨的负载转移构件，以便均匀地分配在两个侧轨上仅施加在单个侧轨上的负载，并且在座椅靠背侧导轨连接到的相应座椅侧轨上方。此外，框架包括具有一对座椅侧轨的座椅底座部分，支撑构件在其相对端枢转地固定，支撑构件固定地固定到下面的支撑表面。

106. 发明授权

US4898426A Passenger seat for an airplane 失效
标题翻译：乘客座位为飞机
公开(公告)号：US4898426A
公开(公告)日：1990-02-06
申请号：US321991
申请日：1989-03-10
申请人： Thilo Schulz , Karl-Heinz Schmitz , Thomas Schneider
发明人： Thilo Schulz , Karl-Heinz Schmitz , Thomas Schneider
IPC分类号： B32B3/12 , B64D11/06
CPC分类号： B64D11/0647 , B64D11/06 , B64D11/0649 , Y02T50/46 , Y10S108/901 , Y10T156/103
摘要： To make the passenger seat for the airplane as light as possible while satisfying safety requirements, some or all the essential components are made with a sandwich-like structure, especially from sandwich panels. These sandwich panels can be made from a plurality of covering layers with a light but strong supporting core (e.g. with a honeycomb structure) interposed between pairs of covering layers.
摘要翻译：为了使飞机的乘客座椅尽可能轻，同时满足安全要求，部分或全部必要部件采用三明治结构制成，特别是夹心板。这些夹层板可以由多个覆盖层制成，其具有插入在成对的覆盖层之间的具有坚固的支撑芯（例如具有蜂窝结构）。

107. 发明授权

US4277103A Aircraft seat with pelvic pad 失效
标题翻译：飞机座椅与骨盆垫
公开(公告)号：US4277103A
公开(公告)日：1981-07-07
申请号：US42329
申请日：1979-05-25
申请人： Kirby B. Weik
发明人： Kirby B. Weik
IPC分类号： A47C7/02 , B60N2/68 , B64D11/06 , A47C7/16 , A47C7/22
CPC分类号： B64D11/0649 , A47C7/022 , B60N2/686 , B64D11/06 , Y02T50/46
摘要： A vehicular seat comprising a seat portion made from a sheet of aluminum or the like, including a first substantially horizontally extending portion at the front of the seat, a second rearwardly declining portion defining the rear portion of the seat, a "V" shaped channel joining the first and second portions, and a strip of aluminum having a width selected to be wider than the opening of the "V" shaped channel and secured to the first and second portions along either side of the channel.
摘要翻译：一种车座，其包括由铝板等制成的座部，所述座部在座椅的前部包括第一大致水平延伸的部分，限定座椅后部的第二后退部分，“V”形通道连接第一和第二部分，以及一个宽度选择为比“V”形通道的开口宽的铝的条，并且沿通道的任一侧固定到第一和第二部分。

108. 发明申请

US20190217958A1 COLLAPSIBLE BACKREST 审中-公开
公开(公告)号：US20190217958A1
公开(公告)日：2019-07-18
申请号：US16365305
申请日：2019-03-26
申请人： AMI Industries, Inc.
发明人： Jacob W. Kirkley , Chad R. Pacheco
IPC分类号： B64D11/06
CPC分类号： B64D11/0698 , B64D11/064 , B64D11/0647 , B64D11/0649 , B64D11/0691
摘要： A collapsible backrest may include a cover and a back panel retained within a first compartment of the cover. A base panel flexibly coupled to the back panel and retained within a second compartment of the cover with the central panel and the base panel defining a notch. A central panel may be flexibly coupled to the base panel and retained within a third compartment of the cover. An end panel may also be flexibly coupled to the central panel and retained within a fourth compartment of the cover. The central panel and the end panel define a cavity. The base panel, the central panel, and the end panel form a triangular support structure in a deployed position. The base panel, the central panel, and the end panel may also be arranged end-to-end and substantially parallel to the back panel in a stowed position.

109. 发明授权

US10035433B2 Frameless transit seat 有权
公开(公告)号：US10035433B2
公开(公告)日：2018-07-31
申请号：US14999270
申请日：2016-04-15
申请人： FREEDMAN SEATING COMPANY
发明人： Vitaliy Viktorovich Muraiti , Paul I. Vidri , David Alan Klopp , Vladislav Balef
IPC分类号： B60N2/01 , B60N2/20 , B64D11/06
CPC分类号： B60N2/01 , B60N2/20 , B64D11/0647 , B64D11/0648 , B64D11/0649 , B64D11/0696 , Y02T50/46
摘要： A frameless transit seat is used for carrying passengers in a transit vehicle. The transit seat is comprised of at least two pedestals which connect the seating portion to the vehicle floor and which distribute the weight of the seat and its passenger(s). Under the passenger, at least two side supports are affixed on top of the pedestals, and one or more crossbars or stabilizers, without any rack frame structures connecting the pedestals. A variant of the transit seat has two seats and uses a mounting plate to connect the two inner side supports to a central pedestal. The components of the transit seat include hollow beams, bent sheet metal, and other components optimized to decrease mass while retaining maximum strength. Optionally, the seat may recline and be upholstered in a variety of covering options.

110. 发明申请

US20180029715A1 SYSTEM AND METHOD FOR AIRCRAFT PASSENGER SEATING 审中-公开
公开(公告)号：US20180029715A1
公开(公告)日：2018-02-01
申请号：US15221595
申请日：2016-07-28
申请人： Ron Larabie , Dave Miller
发明人： Ron Larabie , Dave Miller
IPC分类号： B64D11/06
CPC分类号： B64D11/0639 , A47C7/021 , A47C7/383 , A47C7/402 , A47C7/546 , B23P6/00 , B64D11/06 , B64D11/0649 , B64D11/0693 , B64D11/0696 , B64F5/40
摘要： A system and method for aircraft passenger seating allows traditional passenger seats, which have fixed configurations, to meet new specifications. A bottom frame and backrest frame from a traditional passenger seat is used to form a new passenger seat. Features, such as improved cushioning, telescopic or fixed headrests, rotatable or fixed footrests and improve armrest assemblies may be added as part of the new passenger seat.

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