| 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 | AIRCRAFT MODULAR LAVATORY SYSTEM | US15288823 | 2016-10-07 | US20170021929A1 | 2017-01-26 | Jefferey MCKEE; Trevor SKELLY |
| In a preferred embodiment, a modular lavatory system for replacing a conventional lavatory monument in an aircraft cabin includes a base lavatory module including a fore sidewall, an aft sidewall, and an aisle wall that form a housing enclosing a toilet unit. A first sidewall of the fore sidewall and the aft sidewall may include a widening region positioned above a passenger seat headrest height. The modular lavatory system may include at least two interchangeable modules configured for mounting against the other sidewall of the base lavatory module. A footprint of the base lavatory module may be smaller than the conventional lavatory monument footprint, such that an extra cabin space is created proximate the other sidewall of the base lavatory module after replacement of the conventional lavatory monument with the modular lavatory system. The at least two interchangeable modules may each be dimensioned for installation within the extra space. | ||||||
| 142 | DUAL MODULAR LAVATORY WITH ALCOVES | US15257618 | 2016-09-06 | US20170001728A1 | 2017-01-05 | 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. | ||||||
| 143 | INTERIOR TRIM PART AND SET OF PREFABRICATED PARTS FOR AN AIRCRAFT CELL | US15038421 | 2014-11-20 | US20160362170A1 | 2016-12-15 | Martin Weger; Wolfgang Burger |
| The invention relates to an interior trim part (2, 3, 4, 5, 6) for the planar installation with similar interior trim parts for producing a wall covering inside an aircraft cell, wherein the interior trim part (2, 3, 4, 5, 6) can be rigidly connected to the aircraft cell. The interior trim part has a support structure (20, 21, 22, 23), wherein at least one holding position (9) is provided, which is designed to bear a load in the interior. | ||||||
| 144 | MONUMENT FOR A CABIN OF A VEHICLE, AND FASTENING ARRANGEMENT | US15099074 | 2016-04-14 | US20160304183A1 | 2016-10-20 | Tim von AHLEN; Daniel HIEBING; Ansgar Josef FENNEN; Falk BAJORAT; Christian LÜBBERING |
| A monument for a cabin of a vehicle, in particular of an aircraft or spacecraft, having an outer housing side and a fastening rail for fastening connection elements in a longitudinal direction of the fastening rail in order to fix the monument in position inside the cabin, wherein the fastening rail has a receiving space extending in the longitudinal direction of the fastening rail, which space is designed to receive and fasten mounting feet of the connection elements to the fastening rail, and wherein the fastening rail is integrated in the outer housing side. | ||||||
| 145 | Modifiable aircraft monument | US14277304 | 2014-05-14 | US09457903B2 | 2016-10-04 | Sabrina Moje; Matthias Breuer |
| An aircraft monument for installation in an aircraft cabin comprising a first functional module, a second functional module and a side wall for delimiting the first module from at least one of a region of the aircraft cabin adjacent to the first module and a region of the aircraft monument adjacent to the first module. The side wall is movable between a first and a second operational position and comprises a first side-wall region separating the first and second functional modules and in the second operational position, the side wall is displaced in the direction of the second module relative to its position in the first operational position, so that a movement of the side wall from its first operational position into its second operational position results in an enlargement of a base area of the first module and a corresponding diminution of a base area of the second module. | ||||||
| 146 | LAYERED MODULAR CONSTRUCTS AND PROCESSES THEREFOR | US15168125 | 2016-05-30 | US20160272322A1 | 2016-09-22 | Kristofer Laméy |
| Modular constructs are disclosed wherein a plurality of structural members, most often parallel to one another, form spaced-apart layers. Clamping force, applied in some embodiments approximately perpendicularly to a face of each structural member through use of one or more tension assembly comprising a cable, rope, wire, rod, or the like, in association with one or more tubular spacer, is used to draw the structural members into alignment and to provide structural integrity of the modular construct. The subject matter of the present disclosure further relates to processes for creating such layered modular constructs. The subject matter of the present disclosure may find particular application within modular structures, such as, but not limited to, those for aircraft, boats, and other means of transportation, buildings, storage spaces, furniture and cabinetry, modular support systems for electronic equipment, support structures, interfaces, prosthetics, rack systems, modular work partitions, and the like. | ||||||
| 147 | Installation system for aft aircraft monument assembly | US14928931 | 2015-10-30 | US09428275B2 | 2016-08-30 | Nabih Najd; Harry Ta |
| A method of positioning a monument within an aircraft. The method includes positioning first and second tracks having first and second carriages thereon on the floor. The first and second carriages are initially in a first position. The method includes positioning a floor of a first monument section with a first fitting on the carriage of the first track, positioning a floor of a second monument section with a second fitting on the carriage of the second track, moving the first and second monument sections with the carriages to a second position, aligning the first fittings with a connection point on the aircraft floor, raising the floors of the first and second monument sections and removing the first and second tracks, lowering the floors of the first and second monument sections, securing the first and second fittings to the connection points associated therewith. | ||||||
| 148 | Aircraft monument having a sanitary module and a galley module | US14170017 | 2014-01-31 | US09422056B2 | 2016-08-23 | Bernd Ehlers; Carsten Putensen |
| An aircraft monument for installation in an aircraft cabin comprising a sanitary module having a sanitary fitment, and a galley module arranged adjacent to the sanitary module. The galley module comprises a trolley parking place and a work surface. The trolley parking place is separated from the sanitary module by a partition wall. | ||||||
| 149 | Passenger service unit pod assembly | US14612044 | 2015-02-02 | US09365291B2 | 2016-06-14 | Scott Savian |
| A personal service unit pod assembly configured to be positioned in the interior of an aircraft. The personal service unit pod assembly includes a personal service unit pod and a panel positioned directly above and affixed to the personal service unit pod. The pod includes a housing with a lens assembly and a pod interior, a first reading light positioned within the pod interior and configured to shine light below the bottom of the housing, and cabin lighting positioned in the housing and configured to shine light through the lens assembly and above the housing. The panel includes connectors that are configured to secure the personal service unit pod assembly to a component within the aircraft. | ||||||
| 150 | Aircraft galley | US14596820 | 2015-01-14 | US09352838B2 | 2016-05-31 | William J. Godecker; Peter John Leslie Burd; William D. Aronson; Nicolaas J. van Zwieten; Sebastian Petry; Christopher I. Pirie; Mike Kemery; Aaron Hawkins; Erik Nilsen; Eddie Goh |
| An aircraft galley is disclosed having a stand-alone beverage station and a stand-alone food preparation station. Each station is equipped with extendable work decks and integrated equipment for plug and play exchange. The beverage station is equipped with brewing stations and a top loading refuse compartment, and the food preparation station is configured with multiple ovens and refrigeration units. The galley further includes a side refrigeration unit which can be used as a self-service beverage area for passengers, and both stations may further be configured with LED displays for communicating with passengers. | ||||||
| 151 | Aircraft lavatory unit and disposition configuration therefor | US14380621 | 2013-02-21 | US09340289B2 | 2016-05-17 | Eita Minegishi; Takashi Koyama; Susumu Matono |
| Provided is an aircraft lavatory unit that advantageously allows for a reduced number of parts, simplified assembly, and reduced costs while ensuring convenience. First and second lavatories are provided adjacent to one another within a structural frame. Respective sinks of the lavatories are disposed by being attached to the partition wall. A trash insertion port is provided on a wall surface of each base. A single storage chamber provided within the bases of the sinks of the lavatories extends into the bases of the sinks of the lavatories through an opening provided in the partition wall. A trash can device has a single trash can housed in the storage chamber and a single fire extinguisher. A water heater is singularly provided, which is disposed within the base of one of the sinks. | ||||||
| 152 | Aircraft cabin partition monument with stowage compartment | US14470175 | 2014-08-27 | US09227728B2 | 2016-01-05 | Alex Schimanowski; Soenke Jacobsen |
| An aircraft cabin partition monument comprising a partition wall element and a stowage compartment. The stowage compartment includes a cover plate element and at least one sidewall element. The stowage compartment is convertible between a state of rest, wherein the cover plate and the sidewall element extend substantially parallel to the partition wall element, and a state of operation, wherein the cover plate element and the sidewall element extend relative to the partition wall element such that the cover plate element and the sidewall element define a stowage space arranged adjacent to the partition wall element. | ||||||
| 153 | HIGH DENSITY FULL FLAT BUSINESS CLASS SEAT CABIN | US14650018 | 2013-12-06 | US20150336674A1 | 2015-11-26 | Benjamin Foucher; Philippe Roy |
| Described are arrangements of seats, which include at least one column having rows of pairs of seats (12A,12B), each seat having a chair position and a bed position. A pair of foot wells (34A,34B) are positioned within an aft side of each row and configured to vertically align with the pair of seats in a next-aft row when the pair of seats are positioned in the bed position. The bed position of a first seat (12A) of the pair of seats is vertically offset from the bed position of a second seat (12B) of the pair of seats so that the first seat has a high bed position and the second seat has a low bed position. | ||||||
| 154 | Aircraft Lavatory Unit Installation Method and Aircraft | US14380661 | 2013-02-20 | US20150298810A1 | 2015-10-22 | Takashi Koyama |
| A body frame of an aircraft lavatory unit includes a front wall having an entrance opened and closed off by a door, side walls on both sides, and a floor surface. The outer surface of the side wall positioned closer to the front constitutes a wall facing backrests of a rear seat row and extending in a latitudinal direction. The lavatory unit is capable of being disposed at a front position in which the wall is disposed behind and near the backrests of the seats of the rear seat rows with the backrests being in an upright position, and at a rear position in which the wall is disposed behind and near the backrests of the rear seat rows of the seats with the backrests being in a reclining position. | ||||||
| 155 | SLEEPING BOX, SLEEPING BOX ARRANGEMENT AND AIRCRAFT AREA | US14661677 | 2015-03-18 | US20150266581A1 | 2015-09-24 | Frank ROESE; Carsten PUTENSEN |
| A sleeping box for installation in an aircraft comprises 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 comprises 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. | ||||||
| 156 | MODULE FOR AN AIRCRAFT | US14660268 | 2015-03-17 | US20150259067A1 | 2015-09-17 | Bruno Saint-Jalmes; André Rezag; Jason Zaneboni; Markus Schumacher; Andrew Muin; Cord Haack; Michael Carr |
| A module for an aircraft has a fuselage structure and a floor element defining a floor plane. The module includes a frame device adapted for mounting a functional element and the frame device is adapted for attachment to the floor element of the aircraft at a first location in the floor plane. | ||||||
| 157 | OVERSEAS VEHICLE SEGMENTED ENCLOSURE SYSTEM | US14424798 | 2013-09-03 | US20150225973A1 | 2015-08-13 | Dana G. Patoine; Richard Pike; Philip T. Cantin |
| A module of a transportable segmented enclosure system, including a first walled structure encompassing a volume having a longitudinal axis, the walled structure having at least a first opening, the longitudinal axis passing through the first opening, and a seal apparatus located proximate the first opening, wherein the seal apparatus is configured to form a seal between the first walled structure and another module having a walled structure when the seal of the first walled structure is positioned against the another module. | ||||||
| 158 | VEHICLE LAVATORY | US14402025 | 2013-05-03 | US20150166180A1 | 2015-06-18 | Ralf Schliwa; Maria Theresia Strasdas; Florian Schüphaus; Christian Seibt |
| A vehicle lavatory in particular an aircraft lavatory, is described comprising a cabin having a circumferential wall surrounding a cabin interior space and defining a central vertical axis extending through said cabin interior space wherein said circumferential wall includes an entrance wall section and a sanitary wall section spaced from said entrance wall section a washstand unit extending from said sanitary wall section into said cabin interior space, wherein said washstand unit comprises a washstand top plate extending perpendicularly to said central vertical axis wherein said washstand unit further comprises a washbasin arranged in said washstand top plate, and a urinal unit extending from said sanitary wall section into said cabin interior space, wherein said urinal unit comprises a urinal having a urinal opening, wherein said urinal opening faces said central vertical axis and defines a urinal opening plane. | ||||||
| 159 | Module for an aircraft | US12087328 | 2006-12-27 | US09010686B2 | 2015-04-21 | Bruno Saint-Jalmes; André Rezag; Jason Zaneboni; Markus Schumacher; Andrew Muin; Cord Haack; Michael Carr |
| A module for an aircraft having a fuselage structure and a floor element defining a floor plane. The module includes a frame device adapted for mounting a functional element and the frame device is adapted for attachment to the floor element of the aircraft at a first location in the floor plane. The frame device is adapted for attachment to the fuselage structure of the aircraft at a second location, wherein the second location is not in the floor plane. | ||||||
| 160 | MODULAR PASSENGER SERVICE UNITS AND ASSEMBLIES THEREOF | US14455452 | 2014-08-08 | US20150097082A1 | 2015-04-09 | Amauri PAULINO; Sergio Luiz Abdalla GOMIDE; Gustavo Selofite de ARRUDA; Nilmar César FERREIRA; Luciano dos SANTOS RIBEIRO; Demétrio Andrade de CAMPOS; Sergio Augusto Meireles FILHO; Frederico Lara de OLIVEIRA; Douglas Gonçalves de ALBUQUERQUE; Helio ALBINO; André Duarte STEIN; Paul PRIESTMAN; Daniel MACINNES; Luciano Ricardo Magalhães da SILVA; Ricardo Rosa MACÊDO |
| Elongate passenger service unit (PSU) assemblies are comprised of a plurality of modular passenger service units, and a plurality of variable-length modular spacer units. The modular spacer units are positioned between the modular passenger service units in an end-to-end manner so as to provide a desired lengthwise array of the passenger service units along the PSU assembly. Transport category vehicles, e.g., aircraft, may thus be provided with inboard and outboard PSU assemblies. The passenger seats may be arranged in a latitudinally side-by-side arrangement and/or may be arranged in a longitudinally staggered arrangement. By providing variable length modular spacer units, therefore, the individual passenger service units may be arranged directly overhead of each passenger seat. | ||||||
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