| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 141 | Assembly for Guiding the Longitudinal Sliding Movement of a Sub-Assembly | US12093142 | 2006-11-09 | US20080229547A1 | 2008-09-25 | Dominique Michel |
| An improved arrangement for a transverse dividing element includes an upper cross beam (32), each free end of the cross beam being guided longitudinally by way of an associated guiding structure. The guiding structure includes a slide having a groove in which a free end (34) of the cross beam (32) can slide longitudinally, the free end being equipped with guiding (92, 100) and a locking (102, 104) element. The transverse dividing element can be used to guide an upper cross beam supporting a transverse element that is used to divide the internal space of an aircraft cabin. | ||||||
| 142 | AIRCRAFT ARCHWAY ARCHITECTURE | US12031747 | 2008-02-15 | US20080128551A1 | 2008-06-05 | David A. Young; Richard Fraker; R. Klaus Brauer; Peter S. Guard |
| An architectural archway for an aircraft. The archways can be positioned individually, or in pairs or other sets along the length of an aircraft fuselage. The archways are used to run or connect various transport elements, such as electrical wiring, water lines, and environmental control system conduits, between the upper crown, lower bay and passenger cabin of the aircraft. The invention simplifies installation complexity and eliminates the installation and variability associated with running transport elements between the various sections of the aircraft. | ||||||
| 143 | Holder for a Ceiling Sign | US11660717 | 2005-09-14 | US20080034630A1 | 2008-02-14 | Markus Horst; Stephan Ropke |
| A holding device for attaching a ceiling sign to a ceiling structure contains a base for attaching the ceiling elements and an adapter part for attaching the ceiling sign, the adapter part can be folded down from the base together with the ceiling sign in order to remove the ceiling elements. | ||||||
| 144 | Aircraft archway | US11302823 | 2005-12-14 | US07293739B2 | 2007-11-13 | David A. Young; Richard Fraker; R. Klaus Brauer; Peter S. Guard |
| An architectural archway for an aircraft. The archways can be positioned individually, or in pairs or other sets along the length of an aircraft fuselage. The archways are used to run or connect various transport elements, such as electrical wiring, water lines, and environmental control system conduits, between the upper crown, lower bay and passenger cabin of the aircraft. The invention simplifies installation complexity and eliminates the installation and variability associated with running transport elements between the various sections of the aircraft. | ||||||
| 145 | Aircraft partition designed to separate a cargo part from a cockpit or from a passenger compartment | US10978368 | 2004-11-02 | US07258303B2 | 2007-08-21 | Eric Bouchet; Benjamin Mahieu; Lionel Juillen; Frederic Vinches |
| An aircraft includes a partition designed to separate a cargo part from a cockpit or a passenger compartment. The partition includes a corrugated structure, defining several corrugations with an approximately omega section extending along the direction of the height of the partition. The partition also includes one or several stiffener elements. | ||||||
| 146 | Aircraft archway architecture | US10688624 | 2003-10-17 | US07252267B2 | 2007-08-07 | David A. Young; Richard Fraker; R. Klaus Brauer; Peter S. Guard |
| An architectural archway for an aircraft. The archways can be positioned individually, or in pairs or other sets along the length of an aircraft fuselage. The archways are used to run or connect various transport elements, such as electrical wiring, water lines, and environmental control system conduits, between the upper crown, lower bay and passenger cabin of the aircraft. The invention simplifies installation complexity and eliminates the installation and variability associated with running transport elements between the various sections of the aircraft. | ||||||
| 147 | Arrangement of a first and a second furnishing | US11365323 | 2006-03-01 | US20060202085A1 | 2006-09-14 | Hermann Schotte; Johannes Gonnsen |
| An arrangement, includes a first furnishing and a second furnishing, at least one part of the first furnishing being movable in the direction of the second furnishing, and at least one part of the second furnishing being movable to free a space for receiving the at least one part of the first furnishing. | ||||||
| 148 | Aircraft archway | US11300020 | 2005-12-14 | US20060102787A1 | 2006-05-18 | David Young; Richard Fraker; R. Brauer; Peter Guard |
| An architectural archway for an aircraft. The archways can be positioned individually, or in pairs or other sets along the length of an aircraft fuselage. The archways are used to run or connect various transport elements, such as electrical wiring, water lines, and environmental control system conduits, between the upper crown, lower bay and passenger cabin of the aircraft. The invention simplifies installation complexity and eliminates the installation and variability associated with running transport elements between the various sections of the aircraft. | ||||||
| 149 | Aircraft archway | US11302823 | 2005-12-14 | US20060091259A1 | 2006-05-04 | David Young; Richard Fraker; R. Brauer; Peter Guard |
| An architectural archway for an aircraft. The archways can be positioned individually, or in pairs or other sets along the length of an aircraft fuselage. The archways are used to run or connect various transport elements, such as electrical wiring, water lines, and environmental control system conduits, between the upper crown, lower bay and passenger cabin of the aircraft. The invention simplifies installation complexity and eliminates the installation and variability associated with running transport elements between the various sections of the aircraft. | ||||||
| 150 | Device for holding a partition wall on a wall in the interior of a vehicle | US11185863 | 2005-07-21 | US20060032155A1 | 2006-02-16 | Stefan Thomassin; Rolf Broelemann |
| The device for holding a partition wall on a wall in the interior of a vehicle, particularly on a ceiling paneling of an airplane cabin, comprises a holding element (24; 24′; 24″) to be attached to the vehicle and having at least one recess (34; 34″), and a slider (36; 36″) arranged on the holding element (24; 24′; 24″) and formed with a receiving opening (38; 38″) for receiving an receivable element (26; 26″) of the partition wall (18; 18″). The slider (36; 36″) is supported on the holding element (24; 24′; 24″) for movement on a moving path between a cover position in which the slider (36; 36″) closes the recess (34; 34″) of the holding element (24; 24′; 24″), and an open position in which the receiving opening (38; 38″) is arranged within the recess (34; 34″) of the holding element (24; 24′; 24″). | ||||||
| 151 | Passenger aircraft | US10252590 | 2002-09-24 | US06676079B2 | 2004-01-13 | Yoshihito Takeshima |
| A passenger aircraft so arranged that complete partition wall(s) is/are disposed in the manned space (e.g. a flight deck and a passenger cabin) of the aircraft fuselage so as to completely partition the manned space into at least two manned space sections which are completely isolated from each other. Hence, any hijacker is prevented by the partition wall(s) from his or her access to the manned space. Further, doors and lavatory are provided in the aircraft at points corresponding to such at least two isolated manned space sections, so that pilots, crews, flight attendants and passengers may not only find their own ways for egress from the aircraft and ingress thereto, but also have a wash and relieve themselves, for instance. | ||||||
| 152 | Spacecraft sleeping berth | US09644935 | 2000-08-23 | US06467221B1 | 2002-10-22 | Robert T. Bigelow |
| The present invention provides an improved sleeping berth for space modules that can be expanded from a collapsed position to provide greater passenger comfort in a larger living space. The extension of the berth is accomplished using expandable gas inflated bellows between two hard surface housings. The berth can be retracted into its closed position simply by removing the air pressure from the bellows. The berth's retracted position may still accommodate a passenger and may be used in this position when space is unavailable for the berth's extension. | ||||||
| 153 | Fitting for an aircraft bulkhead | US180154 | 1994-01-11 | US5520357A | 1996-05-28 | David L. Payne; Augusto M. Limcangco |
| A fitting for attaching a galley wall or bulkhead to the interior of an aircraft is disclosed. The fitting uses a separable attachment plate and an anchor, to which an anchor bolt can be attached from above the attachment plate. | ||||||
| 154 | Vehicle bulkhead safety system | US083999 | 1993-06-25 | US5482230A | 1996-01-09 | Michael S. Bird; Andreas Demopolous |
| A safety system for reducing the risk of injury during a survivable crash of a high-speed passenger vehicle. The safety system includes at least one bulkhead support base mounted to a vehicle within a passenger compartment and a bulkhead panel mounted to a portion of the bulkhead support base. In addition, the device includes energy-absorbing means associated with the bulkhead panel for absorbing the energy of a passenger impacting on the bulkhead panel. In this manner, the system minimizes injury to a passenger striking upon a bulkhead wall or class-divider wall within the vehicle. A triggering system is also provided for electronically activating the safety system when necessary. | ||||||
| 155 | Support mechanism for room dividers | US547977 | 1990-07-02 | US5086540A | 1992-02-11 | Markus Schumacher |
| A support mechanism for room dividers is constructed to support room divider curtain rods, for example, to divide an aircraft cabin into several cabin sections. For this purpose a carrier crossbeam is formed of two beam elements hinged to each other in scissors fashion so that the beam elements can buckle downwardly when an interlocking device is released through an operating handle. The end of each beam element is formed as a wall engaging member, such as a T-shaped mounting foot. Each beam element has an extension, whereby a hinge plate is connected between the beam element and its extension. The operating handle which operates the interlocking device is arranged at the end of the extension. At least one locking device and operating handle units, preferably two such units, are used. | ||||||
| 156 | Device for intercepting and retaining cargo in a transport space | US390621 | 1989-08-07 | US5085382A | 1992-02-04 | Robert Finkenbeiner |
| A device for separating a space for cargo in a vehicle, for example in an aircraft cabin or compartment, is constructed for keeping pieces of cargo, for example baggage, in place and to even intercept cargo pieces that may have gotten loose. Such a structure is secured to the vehicle, e.g. an aircraft body, by ceiling brackets and floor mountings. The wall itself is a multilayer structure with different layers provided for different purposes. At least one layer or strut structure is arranged for taking up impact energy effective in a direction in which impact forces are effective, primarily in the travel direction of the vehicle. | ||||||
| 157 | Aircraft partition mounting device | US483899 | 1990-02-23 | US5082224A | 1992-01-21 | Joseph H. Hayward |
| An invention for facilitating the installation and removal of a partition or similar wall-like structure from the interior sections of an aircraft, including a support member, which is attached to any solid or structural section of the aircraft, and a partition fitting, which is secured along any edge of the partition or wall-like structure. The partition is then mountable within any area inside the aircraft by engaging the respective components in joined connection and securing them using any conventional means. The support member comprises a base plate and a section extending vertically from the base diminishing in thickness to form a shank member adaptable for releasable engagement with the partition fitting component of the device. The partition fitting includes a peripheral channel defined by parallel face opposed elements and is adaptable for connection along any edge of the partition or wall-like unit intended to be installed inside the aircraft. | ||||||
| 158 | Aircraft mid-cabin divider | US655521 | 1984-09-28 | US4597549A | 1986-07-01 | James M. Ryan |
| An aircraft mid-cabin divider comprises a double-bulkhead, a vertical wrapping-post within the double-bulkhead, and a wrap-around door having a series of parallel vertical panels flexibly interconnected wherein the first vertical panel is hingeably secured to the vertical wrapping post and a second vertical panel on the substantially opposite end of the door from the first one includes a handle and latch for directing the movement of the tambour door and latching the same about an opposing edge. To be placed in its stowed or open position, the tambour door is rolled backwards around the vertical wrapping-post and drawn between the double bulkheads. A passageway is provided within one of the double-bulkheads through which the door handle may be traversed while the door is inside of the bulkheads. | ||||||
| 159 | Aircraft partition mounting assembly | US886364 | 1978-03-14 | US4185799A | 1980-01-29 | Edward W. Richards, Jr. |
| An anchor fitting assembly for attaching a full width partition, having a door opening, to the fuselage structure of an airplane for dividing a passenger area into two or more compartments. During installation of the partition, provisions are made to allow the lower attachments, of the partition to the seat tracks in the floor of the compartment, to have a certain amount of freedom of movement in both the inboard/outboard and up/down directions. This floating action in the attachment is required for absorbing fuselage deflections due to flight loads imposed on the floor beams and in some cases due to torsional deflections of the wing torque box to which the seat track is fixedly attached, in order to maintain a square door opening. | ||||||
| 160 | Privacy panel with video monitor function for vehicle passenger seating unit | US15092924 | 2016-04-07 | US10124895B2 | 2018-11-13 | Jayson C. Simeon; Nathan E. Careless; Steven K. Brown; Nathan P. Wang; Mark W. Foohey; Heather D. Benoit; Daniel J. Yee; Jens P. Johnson; Terry L. Branson |
| A vehicle passenger seating unit of the type having at least first and second seats facing each other. A privacy panel is provided that includes first and second video monitors positioned between the first and second seats and selectively moveable between respective stowed positions. When both video monitors are stowed, visual interaction is permitted between seat occupants in the first and second seats. When moved to respective deployed positions between the first and second seats, privacy is provided to the seat occupants in the first and second seats. | ||||||
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