| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 101 | Work area in an aircraft | JP2011549539 | 2010-02-09 | JP2012517381A | 2012-08-02 | ヴェッセル，アーニャ; シュタイン，ハルトムート; デティシ，マーク; ベッカー，ホルスト; モリス，リチャード |
| 【課題】航空機の機内の空間を有効活用する。
【解決手段】本発明は、乗務員の作業エリアに関するものであり、乗組員が着替えをすることができるよう、セントラルモジュールを備え、可閉領域を形成する。 セントラルモジュールは航空機機室の後部に設けられ、台車を収容するのに用いられる。 上記エリアは側面の扉で閉められ、扉が開いているときは通路として使用される。 |
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| 102 | Rooms of airliner cabin | JP2004246766 | 2004-08-26 | JP4572097B2 | 2010-10-27 | シュプレンガー ヴィルフリート; レースナー ベルント |
| 103 | Aircraft toilet facilities | JP2010507001 | 2008-04-23 | JP2010525991A | 2010-07-29 | クリストファー リナス |
| 本発明は、航空機用トイレ設備、特に、単一の客室デッキを有する航空機のトイレ設備に関する。 本発明は、航空機の客室デッキの床13の下方空間113内に少なくとも部分的に配置される第１トイレユニット105と、前記客室デッキの天井104の上方空間114内に少なくとも部分的に配置される第２トイレユニット108とを備える。 第１トイレユニット105は、第２トイレユニット108に近接して配置され、第１、第２トイレユニットの両方が、客室デッキから接近可能である。 | ||||||
| 104 | Aircraft cabin module for passengers | JP2004522240 | 2003-07-15 | JP4474280B2 | 2010-06-02 | サン−ジヤルム，ブリユノ |
| 105 | Module for aircraft | JP2008547897 | 2006-12-27 | JP2009522148A | 2009-06-11 | ミッシェル カレ; ジェイソン ザネボーニ; ブルーノ サン−ジャルメ; マルクス シュ−マッハー; コルド ハーク; アンドリュー ムイン; アンドレ レザーク |
| 【課題】本発明は航空機用モジュールに関する。
【解決手段】航空機は胴体構造（６）および床要素（５）を有し、前記床要素（５）は床面を定め、前記モジュールはフレーム装置（２）を有し、前記フレーム装置（２）は機能要素（４）を載置するように構成され、前記フレーム装置（２）は前記機能要素（４）の重心を取り囲むように構成され、前記フレーム装置（２）は前記床面の第１位置（７）で前記航空機の前記床要素（５）への連結するように構成され、前記フレーム装置（２）は第２位置（７'）で前記航空機の前記胴体構造（６）への連結するように構成され、前記第２位置（７'）は前記床面にないことを特徴とするモジュールである。 【選択図】図１ |
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| 106 | Improved facilities structure for privatization airliner | JP2008513394 | 2006-05-25 | JP2009506917A | 2009-02-19 | ジェイムズ ギブソン，ダリル; ルーベン トムソン，ジョン; ブラウン，ワーウィック; ポーター，グレン |
| 複合構造の少なくとも一つのモノコック構造部品から製造される、航空機用設備構造体。 | ||||||
| 107 | Long-haul aircraft | JP2008514141 | 2006-05-29 | JP2008542105A | 2008-11-27 | ゲラン、ベルナール |
| 本発明にかかる本航空機は、操縦室(８)の下に配置される貨物室(１１)内に私用休憩室(１４)を備えている。 この私用休憩室(１４)は操縦室(８)の床(２Ａ)につくられた少なくとも１つの開口部(１２)を通じて操縦室(８)とつながっている。
【選択図】 図１ |
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| 108 | Archway structure of the aircraft | JP2006535618 | 2004-10-13 | JP2007508980A | 2007-04-12 | ガード，ピーター・エス; ブラウワー，アール・クラウス; フレイカー，リチャード; ヤング，デイビッド・エイ |
| 航空機のためのアーチ道構造である。 アーチ道は、航空機の胴体の長さに沿って、個々に、または対もしくは他の組になって位置決めされ得る。 航空機の上部頭頂部、下部ベイ、および客室の間に、たとえば電気配線、水用ライン、および環境制御システム導管などのさまざまな搬送要素を走らせるか、または接続するために、アーチ道が使用される。 この発明は、設置の複雑さを単純化し、航空機のさまざまな部分の間に搬送要素を走らせることに関連する設置およびばらつきをなくす。 | ||||||
| 109 | Aircraft cabin module for passengers | JP2004522240 | 2003-07-15 | JP2005532951A | 2005-11-04 | サン−ジヤルム，ブリユノ |
| 本発明は、１つの長手方向キャビン壁４から長手方向通路８へ延伸する２つの横断方向壁１２と、透明部４４を含む少なくとも１つの横断方向壁１２と、キャビンモジュールを通路８から分離する長手方向壁と、横断方向中間面に対してほぼ対称に２つの横断方向壁１２間に配置５され、かつ２つの連続する個人スペースをモジュールの壁で画定する、少なくとも１つのサービスモジュール１４と、通路から各個人スペースへの入口１６と、各個人スペース内の少なくとも１つの座席１８とを備え、各座席が、少なくとも１つの構造体を有することによってキャビン壁４に平行に方向付けられ、各個人スペースが少なくとも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を含む、航空機キャビンモジュールに関する。 | ||||||
| 110 | Passenger compartment in aircraft cabin | JP2004246766 | 2004-08-26 | JP2005067600A | 2005-03-17 | SPRENGER WILFRIED; ROESSNER BERND |
| PROBLEM TO BE SOLVED: To provide a multifacedly available passenger compartment in an aircraft cabin capable of inexpensively adapting the outline of the passenger compartment to each using purpose especially without requiring additional space. SOLUTION: The passenger compartment in the aircraft cabin has a function supply used for a different purpose, has a size spatially substantially equivalent to the size of a lavatory for disabled persons, and has a front wall, a back wall, and sidewalls. The passenger compartment 1 has multiple-purpose using elements 26, 28 and 33 according to the purpose, and has at least one sheet elements 13 and 14 adaptable according to using form, a changeable table/sheet element 12, and a storage chamber 15. COPYRIGHT: (C)2005,JPO&NCIPI | ||||||
| 111 | Supersonic carrying device | JP2002226125 | 2002-08-02 | JP2003054498A | 2003-02-26 | VAN DER VELDEN ALEXANDER; STOCKFLETH HOLGER |
| PROBLEM TO BE SOLVED: To provide auxiliary equipment for space flight tour or supersonic flight with using an existing driving unit at low cost. SOLUTION: A passenger module 2 as a self-sufficient auxiliary cabin provided with a supply device 6 is combined with a fighter 1 like as a payload container. COPYRIGHT: (C)2003,JPO | ||||||
| 112 | AIRCRAFT INTERIOR COMPONENT SYSTEM AND METHOD FOR MOUNTING AN INTERIOR COMPONENT SYSTEM IN AN AIRCRAFT | PCT/EP2012000421 | 2012-01-31 | WO2012104064A3 | 2012-11-01 | VOSS JENS; DOEMELAND PATRIQUE; HORST MARKUS |
| An aircraft interior component system (10) comprises an aircraft interior component (12), a first structure holder (27), which is fastened to an element (26) of the aircraft structure, and a first component holder (30), which is fastened to the aircraft interior component (12) and is complementary to the first structure holder (27). The first component holder (30) is fastened to the aircraft interior component (12) in a first region (28) of the aircraft interior component (12) which faces an aircraft cabin ceiling when the aircraft interior component (12) is mounted in an aircraft. The first structure holder (27) and the first component holder (30) are designed to attach the aircraft interior component (12) in a suspended manner to the element (26) of the aircraft structure. The aircraft interior component (12) is configured such that, when the aircraft interior component (12) is attached in a suspended manner to the element (26) of the aircraft structure, a mounting gap (40) is present, at least in a second region (32) of the aircraft interior component (12) which faces an aircraft cabin floor (34) when the aircraft interior component (12) is mounted in an aircraft, between a rear side (36) of the aircraft interior component (12) and an aircraft component (38) opposite the rear side (36) of the aircraft interior component (12). | ||||||
| 113 | SANITARY MODULE ARRANGEMENT FOR INSTALLATION IN AN AIRCRAFT CABIN | PCT/EP2011001517 | 2011-03-25 | WO2011116982A3 | 2011-12-15 | EHLERS BERND; HERZOG MARK |
| A sanitary module arrangement (100) suitable for installation in an aircraft cabin comprises a sanitary module (10), the interior (14) of which is separated by a partition wall (12) from an area (16) of the aircraft cabin adjacent to the sanitary module (10). A sanitary appliance (20) and a first trolley parking place (33) to accommodate at least one trolley (40) suitable for holding supplies for the passengers in the aircraft cabin are provided in the interior of the sanitary module (10). A second trolley parking place (39) for accommodating at least one trolley (4) suitable for holding supplies for the passengers in the aircraft cabin is provided adjacent to an outer face (42) of the partition wall (12) outside the sanitary module (10). A trolley fastening device (34) comprises a holder system (36) for detachably fastening a trolley (40) parked at the second trolley parking place (39), wherein the holder system (36) includes a holder (62) attached to the outer face (42) of the partition wall (12). | ||||||
| 114 | 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. | ||||||
| 115 | IMPROVED FACILITY STRUCTURES FOR COMMERCIAL PASSENGER AIRCRAFT | PCT/NZ2006000129 | 2006-05-25 | WO2006126897A2 | 2006-11-30 | BROWN WARWICK; PORTER GLEN; GIBSON DARRYL JAMES; THOMSON JOHN REUBEN |
| A facility structure for an aircraft, manufactured from at least one monocoque structural component of a composite construction. | ||||||
| 116 | LAMINATE STRUCTURES WITH ENHANCED DAMPING PROPERTIES | US16385670 | 2019-04-16 | US20190240958A1 | 2019-08-08 | Michael Edward DeRosa; Jennifer Lynn Lyon; James Robert Matthews; Michael Lesley Sorensen; Arlin Lee Weikel |
| Described herein are laminate structures with enhanced sound-damping properties and mechanical properties. The laminates are composed of an interlayer stucture disposed between a first glass substrate and a second glass substrate, wherein the interlayer is composed of a polymer layer designed such that sound attenuation or damping by the laminate is optimized. The laminates described herein may be used in vehicles or architectural panels. In one or more embodiments, the laminate may be disposed in an opening of a vehicle body. Where the vehicle body is an automobile, the laminate could be used as a windshield, a side window, sunroof or rear windshield. The body of some embodiments may include railcar body, or an airplane body. In other embodiments, the laminate may be used in architectural panels, which may include a window, an interior wall panel, a modular furniture panel, a backsplash, a cabinet panel, or an appliance panel. | ||||||
| 117 | Active composite panel assemblies, systems, and methods | US15131087 | 2016-04-18 | US10149387B2 | 2018-12-04 | Sesinando P. Macaraeg; Nathanial C. Cuddy |
| An active composite panel assembly is configured to transfer electrical signals from a source to an electrical device. The active composite panel assembly includes a composite layer, and an active layer secured to the composite layer. The active layer is configured to receive and conduct the electrical signals. | ||||||
| 118 | Dual modular lavatory with alcoves | US15257618 | 2016-09-06 | US10093421B2 | 2018-10-09 | Scott Savian |
| A modular lavatory monument assembly configured to be positioned in the interior of an aircraft. The modular lavatory monument assembly includes first, second, third and fourth walls that cooperate to form an outer shell that defines a lavatory interior. The fourth wall includes an alcove extending outwardly therefrom. The assembly also includes a sink module positioned in the alcove, a mirror module positioned above the sink module in the alcove, and a door positioned on one of the second or third walls. | ||||||
| 119 | MULTIFUNCTIONAL CONTAINER SYSTEM FOR PRODUCING A CONTAINER UTILIZABLE IN A CARGO COMPARTMENT OF AN AIRCRAFT | US15916514 | 2018-03-09 | US20180273180A1 | 2018-09-27 | Andreas WIETZKE; Thomas LERCHE; Ralf SCHLIWA |
| A multifunctional container system for producing a container for a cargo compartment of an aircraft includes a first lateral container component, which forms a first lateral surface of the container that is at least partially beveled, a first lower resting surface having first fastening devices and a first top side, a second lateral container component, which forms a second lateral surface of the container that is at least partially beveled, a second lower resting surface having second fastening devices and a second top side, and a floor cladding. The cladding is selectively positionable between the first resting surface and the second resting surface, which enclose a continuous gap to each other and comprise a predetermined distance to each other and to create a protrusion that faces away from the first and second top side. The protrusion extends into a recess of a floor in a cargo compartment. | ||||||
| 120 | Augmented Reality System for Pilot and Passengers | US15913789 | 2018-03-06 | US20180251230A1 | 2018-09-06 | Jeremy Robert Chavez; James R. Williamson; Levi Bilbrey |
| The present invention achieves technical advantages as an aircraft having an augmented reality flight control system integrated with and operable from the pilot seat and an associated pilot headgear unit, wherein the flight control system is supplemented by flight-assisting artificial intelligence and geo-location systems. The present invention includes an augmented reality flight control system incorporating real-world objects with virtual elements to provide relevant data to a pilot during aircraft flight. A translucent substrate is disposed in the pilot's field of view such that the pilot can see therethrough, and observe virtual elements displayed on the substrate. The system includes a headgear that is worn by the pilot. A flight assistance module is configured to receive data related to the aircraft and provide predictive assistance to the pilot during flight based on the received data based in part on a pilot profile having preferences related to the pilot. | ||||||
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