| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 81 | Modular wall construction system for aircraft cabin | JP2007521898 | 2005-07-20 | JP2008506591A | 2008-03-06 | クラウス クルベール; ヘルマン ショッテ; オリバー デベルティン; ゲロルト フッペリッヒ |
| 航空機で現在使用される個々のルームユニット、例えば、乗務員の休憩室等は通常、固定した設備であり、乗客の座席を、要求に応じて迅速にこのようなルームユニットへと改造することについては、修理格納庫で長い時間をかけて改造してのみ実現可能とされる。 本発明の実施の形態の一例によると、航空機客室用のモジュール式壁構築システムが提供され、このシステムは、追加の工具なしで接続要素により迅速に設置されるように構成された、個々の作成済み壁構築用パネル（７０１、７０２、７０３）を備える。 この結果、個々の大きさや形状をもったルームユニット（１）による部屋が１つ以上形成される。
【選択図】図２ |
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| 82 | Design structure of archway for aircraft, structural member pair of archway for aircraft, and aircraft | JP2006123697 | 2006-04-27 | JP2006306388A | 2006-11-09 | GUARD PETER S; YOUNG DAVID A |
| <P>PROBLEM TO BE SOLVED: To provide a design structure of an archway for an aircraft. <P>SOLUTION: The archway structure can be positioned, individually or in pairs or other sets, along the length of the interior of the aircraft, for example, such as a commercial airliner. The archway extends across the ceiling of the interior of a cabin and downwardly extends to a point adjacent a baggage bins. In order to conform an end of the archway with the internal baggage bins, an end cap is provided. According to the design structure, a unique "look and feel" and architectural configuration are provided and no seat loss takes place. <P>COPYRIGHT: (C)2007,JPO&INPIT | ||||||
| 83 | Cabin module for aircraft | JP2004522241 | 2003-07-15 | JP2005532952A | 2005-11-04 | サン−ジヤルム，ブリユノ |
| 本発明は、２つの小壁によって連結される２つの大壁１２と、モジュール１０を通路８から分離する１つの壁に沿って配置されるサービスモジュール１４と、１つの小壁に設けられる開口部に取り付けられたドア１６と、航空機の移動方向に対して長手方向に方向付けられる少なくとも１つの構造体を有する少なくとも１つの座席１８とを備える、長い矩形形状の航空機キャビンモジュールに関する。 各モジュールは、少なくとも１人の乗客のベッド面を構成するように作られた要素２４、２８を備える。 | ||||||
| 84 | Apparatus for receiving the transport chamber of the cargo airplane | JP20153189 | 1989-08-04 | JP2588435B2 | 1997-03-05 | ROOBERUTO FUINKENBAINERU |
| 85 | DOOR FOR AN AIRCRAFT | PCT/US2014046327 | 2014-07-11 | WO2015006678A2 | 2015-01-15 | GOINGS WILLIAM A; LONG ERIC |
| A door for an aircraft includes a first panel divisible into at least two first slats that are releasably connected to one another, a first tensioning cable attached between the at least two first slats, and a first tensioner connected to the first tensioning cable and being operative to apply a first tension thereto, thereby permitting the first tensioning cable to hold the at least two first slats together to form the first panel and to release the first tension in the first tensioning cable upon occurrence of a release action, thereby permitting the at least two first slats to dissociate from one another so that the first panel fragments. | ||||||
| 86 | WORK AREA IN AN AIRCRAFT | PCT/EP2010051580 | 2010-02-09 | WO2010092047A3 | 2011-01-20 | BECKER HORST; STEIN HARTMUT; WESSELS ANJA; DETISI MARK; MORRIS RICHARD |
| The invention relates to a work area for members of a flight crew, which comprises a central module (104), which borders an area (117) adapted for being closed intended for use by crewmembers to change clothes. The central module is arranged in the tail area of the aircraft cabin, and can be used for stowing trolleys. The area is closed by lateral doors (118, 119), and can be used as a passageway when the doors are open. | ||||||
| 87 | COUPLING DEVICE WITH ADJUSTMENT PLATE | PCT/FR2009050762 | 2009-04-24 | WO2009138673A3 | 2010-01-21 | DAOUK ANTAR |
| The invention relates to a device (1) for coupling equipment to a rail in a vehicle, said device (1) comprising both a main body (2) designed to be attached to the rail, and a connecting member (3) attached to the main body (2) and designed to be connected to said equipment, said device (1) being characterized in that the connecting member (3) comprises, as a minimum, both a first plate (4) mounted movably on the main body (2), and a first adjustment means (8) designed to allow a user to adjust, by manipulating the first adjustment means (8), the position of the first plate (4) relative to the main body (2). Coupling devices. | ||||||
| 88 | STRUCTURAL ASSEMBLY AND METHOD | US15856019 | 2017-12-27 | US20190195259A1 | 2019-06-27 | Bejan Banihashemi; Alex de Marne; Russell Keck; Roland Mair |
| A structural assembly includes a first member and a second member. The first member has at least one fastener receptacle and at least one shear pocket formed in the member side. The Shear pocket has a pocket cross-section. The second member has at least one shear boss protruding outwardly from the second member, the shear boss has a boss cross-section shaped complementary to the pocket cross-section. The shear boss is configured to be received with the shear pocket and transfer only shear load between the first member and the second member. The structural assembly includes a tension fastener configured to engage the fastener receptacle and couple the first member to the second member and transfer only tension load therebetween at least during an initial transfer of the shear load between the first member and the second member by the shear boss. | ||||||
| 89 | SEPARABLE VEHICLE CABIN PRIVACY PARTITION ASSEMBLIES WHICH ALLOW FOR EMERGENCY EGRESS | US15926135 | 2018-03-20 | US20180297707A1 | 2018-10-18 | Beenal GHARIA; Brian RAHN; Janyce WYNTER; Jay BEEVER; Joshua REA; Paulo Celso PIRES |
| Separable partition assemblies provide privacy between adjoining vehicle cabin sections, e.g., between a main passenger cabin section and a section having an emergency exit and a belted toilet seat such as may be provided in executive aircraft. According to the disclosed embodiments, the partition assembly includes a bulkhead structure defining a bulkhead passageway opening to allow passenger egress from one vehicle cabin section to an adjoining vehicle cabin section. At least one panel is provided which is sized and configured to close the bulkhead passageway opening defined in the bulkhead structure. A nonpermanent mounting system mounts the at least one panel to an inboard edge of the bulkhead structure to allow the at least one panel to be separably uncoupled from the bulkhead structure in response to exertion of a force of predetermined magnitude thereagainst, the mounting system having separable mounting elements (e.g., two-part magnetic or hook and loop fabric connectors) to allow the at least one main panel to be separably uncoupled from the bulkhead structure when in the closed condition thereof in response to exertion of a force of predetermined magnitude thereagainst to thereby allow unimpeded passenger egress between the adjoining vehicle cabin sections. | ||||||
| 90 | PASSENGER ACCOMMODATION SYSTEMS INCLUDING PARTITION WALLS | US15554160 | 2016-04-04 | US20180265201A1 | 2018-09-20 | Victor Carlioz; Hugo Jamson; Lito Karatsoli; Luke Miles |
| Passenger accommodation systems are described. An example passenger accommodation system can be disposed in an aircraft and can include a passenger seating deck, a plurality of passenger seats disposed within the passenger seating deck, and a partition wall disposed within the passenger seating deck so as to separate the plurality of passenger seats into a first set of passenger seats and a second set of passenger seats. The partition wall can be aligned with a longitudinal axis extending in the direction of travel of the aircraft. Movement of passengers between the first set of seats and the second set of seats may not impeded by the partition wall. | ||||||
| 91 | Panel assembly with crush section | US14788255 | 2015-06-30 | US10059423B2 | 2018-08-28 | Tyler Smithson; Rakibul Islam; Richard Morrison; Monique Le Roux; Aamir Jafri |
| A panel assembly that includes a front skin having a front surface, a back surface and at least one crush section portion, a core assembly that includes first, second, third, fourth and fifth layers laminated together, and at least a first crush section. The first, second, third, fourth and fifth layers each include a front surface, a back surface and at least one crush section portion. The front surface of the first layer of the core assembly includes a plurality of scores defined therein. The second layer includes a plurality of elongated voids defined therein and the fourth layer includes a plurality of elongated voids defined therein. | ||||||
| 92 | CONTOURED CLASS DIVIDER | US15944310 | 2018-04-03 | US20180222589A1 | 2018-08-09 | Robert PAPKE; Shawn Claflin; Jefferey McKee; Trevor Skelly; Mario Diliani |
| An implementation of a contoured class divider for dividing an aircraft cabin includes a panel positioned between an aft seat and a forward seat, the panel having an aft-facing convex contour closely matching an aft-facing contour of a seatback of the forward seat and configured to enhance space utilization. The contoured class divider may include an articulation system to articulate at least a portion of the panel from a first position (normal operation) to a second position (emergency landing). The contoured class divider may provide up to an additional 12 inches of space which can be used to reduce seat pitch (and thereby enhance passenger comfort) or increase the number of rows of seats on a given aircraft. | ||||||
| 93 | AIRCRAFT DIVIDER ASSEMBLY | US15441051 | 2017-02-23 | US20180194471A1 | 2018-07-12 | Joseph Merrick; Ian Geoffrey Scoley; Eric Heimbach; Jean-Claude Bourgade; Didier Poho |
| A divider assembly that includes a main body portion having a lower section and an upper section and a removable panel having front and back surfaces. The upper section tapers in width in an upward direction and the main body portion includes front and back surfaces. The removable panel is removably secured to the upper section on the front surface of the main body portion. | ||||||
| 94 | Divider element for an aircraft cabin | US14677424 | 2015-04-02 | US09868528B2 | 2018-01-16 | Tobias Mayer |
| A divider element for an aircraft cabin is disclosed including a frame member forming a closed ring wherein the frame member may assume an expanded state and a collapsed state, wherein in the expanded state the frame member extends in a plane and defines a first area which is surrounded by the frame member and wherein in the collapsed state the frame member defines a second area which is surrounded by the frame member, the second area being smaller than the first area, and a flexible sheet member which is fixed to the frame member and dimensioned such that when the frame member is in the expanded state, it extends over the area defined by the frame member. | ||||||
| 95 | Aircraft Interior Surface and Method of Illuminating an Aircraft Interior Surface | US15478568 | 2017-04-04 | US20170283065A1 | 2017-10-05 | Robert Papke; Shawn Claflin; Stephanie Lightbody; Jefferey McKee |
| An aircraft interior surface for partitioning, dividing, or establishing privacy within a cabin space includes a transparent material that provides for transmission of light within the aircraft cabin. A graphical design may be applied to the transparent material, the graphical design including indicia arranged in predetermined patterns based on a location or function of the transparent material. A light source located proximate to the transparent material may wash light across a surface of the transparent material such that the graphical design exhibits predetermined properties when illuminated by the light source. The transparent material may be selectively dimmable to increase opacity. | ||||||
| 96 | PASSENGER SEATING WITH MULTI-MODE PRIVACY DOOR | US15474131 | 2017-03-30 | US20170283064A1 | 2017-10-05 | Aaron Robinson |
| Passenger seating comprises rows of seats with a door assembly at the end of each row for improving a seat occupant's privacy. The door assembly includes a door that slides into and out of a base in a primary mode of operation, and which supports a secondary mode of opening. The secondary mode may involve pivoting on hinges. A latch is provided to prevent the door from being opened routinely in the secondary mode. The door assembly is also capable of retracting with respect to the adjacent seat to improve access. | ||||||
| 97 | CONTOURED CLASS DIVIDER | US15291863 | 2016-10-12 | US20170283061A1 | 2017-10-05 | Robert PAPKE; Shawn CAFLIN; Jefferey MCKEE; Trevor SKELLY; Mario DILIANI |
| In a preferred embodiment, a contoured class divider for dividing an aircraft cabin includes a panel positioned between an aft seat and a forward seat, the panel having an aft-facing convex contour closely matching an aft-facing contour of a seatback of the forward seat and configured to enhance space utilization. The contoured class divider may include an articulation system to articulate at least a portion of the panel from a first position (normal operation) to a second position (emergency landing). The contoured class divider may provide up to an additional 12 inches of space which can be used to reduce seat pitch (and thereby enhance passenger comfort) or increase the number of rows of seats on a given aircraft. | ||||||
| 98 | Flight attendant seat, arrangement having a flight attendant seat, and aircraft area | US15616439 | 2017-06-07 | US20170267356A1 | 2017-09-21 | Matthias Breuer; Sabrina Moje |
| A flight attendant seat comprises a carrier device having a first surface, a seat element movably coupled to the carrier device, and a backrest element movably coupled to the carrier device and operatively coupled to the seat element. The seat is movable between an operative position, permitting the use of the seat by a flight attendant, and an inoperative position in which the seat element and the backrest element are positioned, relative to the carrier device, such that they do not protrude from the carrier device first surface. The seat may be positioned in such a way, relative to a passenger seat or a row of passenger seats, that the rear side of the backrest element faces towards the rear side of a backrest of the passenger seat or the rear side of a backrest of at least one passenger seat belonging to the row of passenger seats. | ||||||
| 99 | PARTITION WALL MODULE FOR A CABIN OF A VEHICLE FOR AN OPTICAL AND MECHANICAL SEPARATION OF DIFFERENT CABIN REGIONS | US15459796 | 2017-03-15 | US20170267350A1 | 2017-09-21 | Andreas HEIDTMANN; Jörg WEIFENBACH; Mark HERZOG; Roland LANGE |
| A wall module for a cabin of a vehicle for separation of different cabin regions comprises a lower wall section having at least one first fastening means for fastening the wall module to at least one near-floor structurally fixed component in the cabin, a surface-like rigid upper wall section converging with the lower wall section having at least one second fastening means in a region of the wall module facing away from the lower wall section for fastening the wall module to at least one near-ceiling structurally fixed component in the cabin. The upper wall section at least in a region comprises an arched curvature around a horizontal axis for adapting to the shape of a backrest of a seat. The wall module comprises at least one edge stiffening element, which extends between a near-floor region and a near-ceiling region of the wall module. | ||||||
| 100 | ARRANGEMENT WITH A PARTITIONING DEVICE IN A CABIN OF A VEHICLE AND AIRCRAFT WITH A CABIN AND SUCH AN ARRANGEMENT | US15494051 | 2017-04-21 | US20170225787A1 | 2017-08-10 | Ralf SCHLIWA; Eric STUCHLY |
| An arrangement in the cabin of a vehicle includes a floor, a first equipment component, a second equipment component and a partitioning device. The partitioning device is set up to provide a wall surface between the first equipment component and second equipment component largely perpendicular to the floor. The partitioning device is positionable in at least two positions along a length running between the first equipment component and second equipment component. The partitioning device is lockable in its respective position on at least one of the floor, a cabin ceiling and a cabin lining. | ||||||
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