| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 121 | Hexagonal Floor and Ceiling System for a Vehicle | US15913666 | 2018-03-06 | US20180251206A1 | 2018-09-06 | Andrew Zahasky |
| The present invention achieves technical advantages as a vehicle cabin, comprising a floor system formed of removable and reconfigurable floor segments extending from a vehicle frame, and a ceiling system formed of removable and reconfigurable ceiling segments disposed in the ceiling of the vehicle cabin. Floor segments that can be positioned to form a floor channel, therebetween. A fixture interface adapted to releasably secure a fixture to the floor system. The fixture can be slidably repositioned within the vehicle along the floor channel. One of the ceiling segments includes one or more of a lighting module, a ventilation outlet, a ventilation inlet, a display screen, or a touch control panel. The ceiling segments can be hexagonal. | ||||||
| 122 | SLEEPING BOX, SLEEPING BOX ARRANGEMENT AND AIRCRAFT AREA | US15925347 | 2018-03-19 | US20180208315A1 | 2018-07-26 | Frank Roese; Carsten Putensen |
| A sleeping box for installation in an aircraft includes a casing which is suitable for accommodating a person located in a reclining position parallel to a longitudinal axis of the casing and which has an access aperture in the area of a front side which extends perpendicularly to the longitudinal axis of the casing. The sleeping box also includes a fastening apparatus which is configured to fasten the sleeping box within a passenger cabin of the aircraft in such a way that the longitudinal axis of the casing extends perpendicularly to a longitudinal axis of the passenger cabin and the access aperture of the casing borders on an aisle which is present within the passenger cabin. | ||||||
| 123 | BENDABLE ELEMENT THAT CAN BE BENT BY INFLATING AN ENVELOPE, BENDABLE BATTEN AND STRUCTURE COMPRISING SUCH AN ELEMENT AND ASSOCIATED BENDING METHODS | US15847090 | 2017-12-19 | US20180178894A1 | 2018-06-28 | Bernard Guering; Laurent SAINT-MARC |
| A bendable element is formed at least from an inflatable envelope, a first bendable, elongate base plate attached to a first face of the inflatable envelope, a second bendable, elongate base plate, attached to a second face of the inflatable envelope and shorter than the first base plate, and links connecting the first base plate to the second base plate. The links are slack when the inflatable envelope is in a deflated state. The action of inflating the inflatable envelope causes the first and second base plates to bend in a direction of curvature extending from the first base plate to the second base plate, by means of the tensioning of the links such that the links extend along radii of curvature common to the first and second base plates while keeping the second base plate centered longitudinally relative to the first base plate. | ||||||
| 124 | INTEGRATED CENTERLINE LAVATORY MONUMENT | US15878220 | 2018-01-23 | US20180148175A1 | 2018-05-31 | Scott SAVIAN; Zhao JIN |
| A monument configured to be positioned in the interior of an aircraft that includes first, second, third and fourth sides and first and second lavatories spaced apart from one another by at least a portion of a galley storage section that is open to the first side. The first and second sides are opposite to one another and the third and fourth sides are opposite to one another. The first lavatory defines a first lavatory interior and includes a first toilet therein and the second lavatory defines a second lavatory interior and includes a second toilet therein. | ||||||
| 125 | Lavatory with recessed flight attendant seat | US14993929 | 2016-01-12 | US09981747B2 | 2018-05-29 | Scott Savian; Ian Geoffrey Scoley; Ralph Burrows; Christoph Goeschel; John Higgins; Thomas Lee; Herman Schotte |
| A 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 enclosure that defines a lavatory interior, a door positioned on one of the first, second, third, or fourth walls, and an opening on the fourth side that is open to an exterior of the enclosure. A seat is at least partially positioned in the opening. The seat includes a seat back and a seat portion that is pivotal between a storage position and a deployed position. In the deployed position the seat portion extends outside of the opening. | ||||||
| 126 | TOILET MODULE FOR A VEHICLE AND A VEHICLE INCLUDING A TOILET MODULE | US15857309 | 2017-12-28 | US20180118348A1 | 2018-05-03 | Ralf SCHLIWA; Volker LUDERER; Florian SCHUEPHAUS; Roland LANGE; Michael ECKERT |
| A toilet module and a vehicle including a toilet module are provided. An exemplary toilet module includes a toilet unit and a housing. The housing includes a front wall with an access opening, a first functional wall arranged opposite the front wall and supporting the toilet unit, and a second functional wall perpendicular to the front wall and extending between the front wall and the first functional wall. Further, the toilet module includes a storage shelf attached to the housing and a swivable table attached to the housing and movable to an extended configuration. The swivable table overlaps the storage shelf when in the extended configuration. | ||||||
| 127 | Access device provided with independent mobile walls enabling secure communication between at least two zones of an enclosure | US15150507 | 2016-05-10 | US09944380B2 | 2018-04-17 | Bernard Guering |
| An access device enables controlled or secure communication between different areas of an enclosure and, in the example illustrated in the present application of an aircraft, while providing reduced size. The access device includes at least three mobile walls able to move, independently from one another, to form a closed cylinder, the walls thus being in a so-called security vestibule position, and to overlap at least in twos in order to close off access to one or more areas while concealing the security vestibule, the walls thus being in a so-called retracted position. By overlapping at the access level of said areas that the walls allow to close, the device frees up the adjoining cabin space. | ||||||
| 128 | Integrated centerline lavatory galley monument | US14861856 | 2015-09-22 | US09896212B2 | 2018-02-20 | Scott Savian; Zhao Jin |
| A monument configured to be positioned in the interior of an aircraft that includes first, second, third and fourth sides and first and second lavatories spaced apart from one another by at least a portion of a galley storage section that is open to the first side. The first and second sides are opposite to one another and the third and fourth sides are opposite to one another. The first lavatory defines a first lavatory interior and includes a first toilet therein and the second lavatory defines a second lavatory interior and includes a second toilet therein. | ||||||
| 129 | PIVOT BIN BUCKET WITH SLOT FOR RECEIVING PIVOT AXLE | US15727479 | 2017-10-06 | US20180029709A1 | 2018-02-01 | Scott Savian |
| A bucket for use with an aircraft storage bin that includes a bottom and first and second opposing side walls extending upwardly from the bottom. The first and second side walls each include a top edge. The first side wall includes a first slot that is open to the top edge of the first side wall and is configured to receive a first pivot axle therein, and the second side wall includes a second slot that is open to the top edge of the second side wall and is configured to receive a second pivot axle therein. | ||||||
| 130 | Aircraft Service Trolley and Galley Enclosure Therefor | US15647193 | 2017-07-11 | US20180016013A1 | 2018-01-18 | Peter John Leslie Burd; Neil R. Elshaw; Sam Foster; Venkata Prasanth Suman Neti; Allan Coombs; Donna Charlene Brownlie; Merv Davidson; Elizabeth M. Payne |
| In an illustrative embodiment, a retaining assembly secures an equipment item within an aircraft galley compartment. The retaining assembly may include a turn button assembly including a turn button connected to a front edge of the galley compartment to secure the equipment item within the galley compartment. The turn button rotates between a first position for allowing insertion or release of the equipment item from the galley compartment and a second position for securing the equipment item within the galley compartment. A turn button recess on an inner surface of a panel door that is coupled to an edge of an opening for the galley compartment receives the turn button of the turn button assembly when the turn button is in the second position to allow the panel door to fully close over the opening for the galley compartment. | ||||||
| 131 | LARGE SELF-CARRYING MONUMENT ASSEMBLY FOR AN AIRCRAFT AND AN AIRCRAFT HAVING SUCH A MONUMENT ASSEMBLY | US15718899 | 2017-09-28 | US20180016010A1 | 2018-01-18 | Hermann BENTHIEN; Matthias HEGENBART; Andreas POPPE; Wolfram SCHOPENHAUER; Ralf SCHLIWA; Thomas LERCHE; Cord HAACK; Ralph STURM; Matthias RADNY; Jon RUETER |
| A monument assembly for an aircraft includes at least one component of a primary structure of the aircraft, in particular a fuselage stiffening element, and a plurality of interconnected framework elements for creating a self-carrying three-dimensional framework. The at least one fuselage stiffening element is attachable to a skin of the aircraft and includes at least one bracket, wherein the framework is mechanically supported on the at least one bracket of the at least one component of the primary structure of the aircraft and wherein the framework comprises a plurality of compartments accessible from an interior region of the aircraft. The compartments are adapted for receiving and holding cabin equipment modules. | ||||||
| 132 | AIRCRAFT COCKPIT MODULE, AIRCRAFT COMPRISING SUCH A MODULE AND METHOD FOR INSTALLING THE MODULE IN A COCKPIT | US15643793 | 2017-07-07 | US20180009532A1 | 2018-01-11 | Olivier CAZALS; Jaime GENTY DE LA SAGNE |
| An aircraft cockpit module (10) that incorporates, on the one hand, a single pilot seat (12) and, on the other hand, at least a part of the piloting equipment and controls necessary for flying an aircraft, the module (10). The aircraft cockpit module forms an assembly which can be moved unitarily and to be incorporated in a single operation in an aircraft cockpit. The module is dedicated to a single pilot and makes it possible to simplify the integration of the cockpit. | ||||||
| 133 | Modular lavatory system optimized for narrow body commercial aircraft | US14677626 | 2015-04-02 | US09862491B2 | 2018-01-09 | Jefferey McKee; Trevor Skelly |
| An optimized, multi-configuration cabin and lavatory arrangement for a single aisle aircraft that adds either another row of seating or increases cabin space without sacrificing performance or function of the existing components. The invention includes a space efficient lavatory that may incorporate various design configurations to meet the needs of airlines seeking to generate additional revenue. The configuration of the present invention uses a reduction in the lavatory floor plan with the option for a modular flex wall area to provide a customizable combination that gains extra cabin space for carriers that can be utilized for additional revenue streams. | ||||||
| 134 | Vehicle Body and Method for Assembling a Vehicle Body | US15407510 | 2017-01-17 | US20170297713A1 | 2017-10-19 | Matthias Hegenbart; Detlev Konigorski; Peter Linde |
| A vehicle body includes a primary vehicle structure and interior vehicle fittings as well as a coupling device for fastening the interior vehicle fittings to the primary vehicle structure. The coupling device is configured to generate a magnetic field, so as to fasten the interior vehicle fittings to the primary vehicle structure without contact. Methods for assembling a vehicle body as well as an edifice are also described. | ||||||
| 135 | Passenger service module with integrated cabin lighting | US14175660 | 2014-02-07 | US09789962B2 | 2017-10-17 | Bernd Ehlers; Mark Herzog |
| A service module for supplying passengers in a passenger space of a means of transport, in particular of an aircraft, and to a service system having a service channel and a plurality of such service modules. The service module comprises at least one service component arrangement having one or more service components for individually supplying one or more passengers, and a cabin lighting unit for illuminating the passenger space of the means of transport, in particular of the aircraft. | ||||||
| 136 | COMMERCIAL AIRCRAFT INTERIOR MONUMENT PROTECTION SYSTEM | US15092428 | 2016-04-06 | US20170291725A1 | 2017-10-12 | Ryan Nelson Marcelo Abelon; Cory M. Hitchcock; Toai Dac Tran; Thomas Ralph Smith, JR.; Jon Burton Shaw |
| A method of protecting a monument during manufacturing of a vehicle. The method includes attaching a plurality of brackets to the monument prior to installation in the vehicle, each of the plurality of brackets having corresponding fasteners facing outwardly relative to the monument. The method also includes connecting a blanket to the corresponding fasteners. The method also includes installing the monument in the vehicle, disconnecting the blanket, and removing the plurality of brackets from the monument. | ||||||
| 137 | HINGE FOR ENLARGING THE VOLUME OF AN AIRCRAFT STORAGE BIN | US15477071 | 2017-04-01 | US20170283058A1 | 2017-10-05 | Robert Papke; Shawn Claflin |
| In a preferred embodiment, a retrofit storage bin door hinge includes an extension member than increases the storage volume of the bin by at least 5 percent or 10 percent, thereby permitting the storage of larger carry-on bags. Required access to the ceiling panels during maintenance operations is preserved by the hinges pivotable attachment to a pivot mount attached to the ceiling of a storage bin. In this manner, the hinge assembly and door may be readily translated downwardly to provide full access to the ceiling panels during a maintenance operation. | ||||||
| 138 | Aircraft interior component system and method for mounting an interior component system in an aircraft | US13954734 | 2013-07-30 | US09708051B2 | 2017-07-18 | Jens Voss; Patrique Doemeland; Markus Horst |
| An aircraft interior component system includes an aircraft interior component, a first structure holder fastened to an element of the aircraft structure, and a first component holder fastened to the aircraft interior component. The first component holder is fastened to the aircraft interior component in a first region thereof which faces an aircraft cabin ceiling when the aircraft interior component is mounted in an aircraft. The first structure holder and the first component holder attach the aircraft interior component in a suspended manner to the element, such that a mounting gap is present, at least in a second region of the aircraft interior component facing an aircraft cabin floor when the aircraft interior component is mounted in an aircraft, between a rear side of the aircraft interior component and an aircraft component opposite the rear side of the aircraft interior component. | ||||||
| 139 | System and method for mounting aircraft system components in the crown area of an aircraft | US14444098 | 2014-07-28 | US09644765B2 | 2017-05-09 | Matthias Breuer; Wei-Chung Tuan; Frank Klepka |
| A system for mounting aircraft system components in the crown area of an aircraft comprising a first longitudinal carrier element, a second longitudinal carrier element and a bridging element which connects the first longitudinal carrier element to the second longitudinal carrier element. The system is mountable in the crown area of an aircraft in such a way that the first and the second longitudinal carrier elements extend substantially parallel to the longitudinal axis of the aircraft. A plurality of cable ducts for accommodating electrical lines is provided on the first and/or the second longitudinal carrier elements. | ||||||
| 140 | LAMINATE STRUCTURES WITH ENHANCED DAMPING PROPERTIES | US15219664 | 2016-07-26 | US20170028687A1 | 2017-02-02 | 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 structure 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. | ||||||
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