| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 161 | APPARATUS AND METHODS TO ATTACH AN OBJECT TO AN OVERHEAD SECTION OF A CABIN OF AN AIRCRAFT | US15589576 | 2017-05-08 | US20180319502A1 | 2018-11-08 | William Maclay; Peter Zarkowskyj |
| Apparatus and methods to attach an object to an overhead section of a cabin of an aircraft. An example apparatus includes a bracket to be positioned between rails in a cabin of an aircraft. The bracket includes edges having first attachment points to align with second attachment points of each of the rails. The bracket is positionable along a length of the rails by aligning the first attachment points of the bracket with a portion of the second attachment points of the rails. The bracket also includes flanges disposed between the edges. The flanges have respective third attachment points and fourth attachment points aligned to receive fasteners for hanging a device used in the cabin of the aircraft. | ||||||
| 162 | Aircraft having a self-erecting partition element in a compartment inside the fuselage | US14706476 | 2015-05-07 | US10059425B2 | 2018-08-28 | Ferdinand Vetter; Stefan Loebel |
| An aircraft comprising a fuselage defining a longitudinal axis and an interior compartment. Along the axis, in cross-section perpendicular to the axis, the compartment is enclosed by a floor, sidewall and ceiling structure. The aircraft further comprises an environmental control system comprising a conduit system through which a pressurized fluid is supplied, at least one first terminal disposed inside the compartment and in fluid communication with the conduit system, and a selectively inflatable and deflatable partition element. The partition element comprises at least one second terminal and is constructed such that it is inflatable from a deflated condition into an inflated condition by establishing a fluid communication between the second terminal and the first terminal. In the inflated condition the partition element completely closes the cross-section of the compartment, thereby dividing it into two portions, and in the deflated condition collapses and at least partially unblocks the cross section. | ||||||
| 163 | FORWARD INTERIOR SPACE ARRANGEMENT FOR AN AIRCRAFT | US15878019 | 2018-01-23 | US20180208316A1 | 2018-07-26 | Roland LANGE; Andreas HEIDTMANN |
| An interior space for an aircraft includes a cockpit, a cockpit wall separating the cockpit from the remaining interior space, a cabin door arranged directly behind the cockpit wall for accessing the interior space of the aircraft from outside the fuselage, a modular installation space for installation equipment, a plurality of seat rows, a longitudinal aisle extending along the interior space through the seat rows to separate adjacent groups of seats from each other, and an access path for the cabin door. The access path extends from the cabin door to the longitudinal aisle to create an intersection region between the access path and the longitudinal aisle. The modular installation space is arranged directly forward of the seat rows. The access path extends at an angle of at least 100° to the longitudinal aisle in a forward direction. | ||||||
| 164 | AIRCRAFT CABIN AND PARTITION ASSEMBLY THEREFOR | US15736532 | 2016-06-21 | US20180194472A1 | 2018-07-12 | Michel TREMBLAY; Jenifer TRAM |
| A partition assembly (16) for an aircraft cabin, including a bulkhead (18) with first (28) and second (30) internal compartments having respective first (32) and second (34) open ends defined in a same side of the bulkhead (18), one of the compartments being located aft of the other, a sliding door (36) slidingly supported within the first compartment (28) and slidable out of the first compartment (28) through the first open end (32), and a curtain (42) slidingly engaged to a curtain rail (40), the curtain receivable in the second compartment (30) and slidable along the curtain rail (40) out of the second compartment (30) through the second open end (34). An aircraft curtain rail is also described where the curtain rail and curtain track each have a non-rectilinear profile when viewed in a first plane and when viewed in a second plane perpendicular to the first plane. A method of manufacturing a curtain rail is also discussed. | ||||||
| 165 | MOBILE CLASS DIVIDER FOR AIRCRAFT CABIN | US15576505 | 2016-05-27 | US20180148172A1 | 2018-05-31 | Jérôme Verbeque; Romain Breyne; Jean-Claude Bourgade |
| A mobile class divider transversely partitions the interior space of a cabin of an aircraft. The divider is delimited by ceiling trim panels, at least two lateral rows of overhead luggage compartments extending longitudinally near to the ceiling trim panels, lateral walls and a floor. The divider slidably mountable to guide rails arranged between the overhead luggage compartments and the ceiling trim panels. The divider includes a transverse main framework extending on either side of the lateral walls, at least two guide blocks supported by the framework, and an adjustment feature. The length of the divider is adjustable to adapt to the distance, in the transverse direction, that separates said guide rails of said cabin. | ||||||
| 166 | CONTOURED CLASS DIVIDER | US15720615 | 2017-09-29 | US20180022457A1 | 2018-01-25 | Robert Papke; Shawn Caflin; Jefferey McKee; Trevor Skelly; Mario Diliani |
| A contoured class divider for dividing an aircraft cabin includes a panel positioned between an aft seat and a forward seat, the panel having a 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 multiple panel portions that are coupled together and articulate relative to one another. The contoured class divider may include an articulation system to articulate the panel portions with respect to one another 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. | ||||||
| 167 | System and method for integrated magnetic slider assembly for hanging partition | US14825168 | 2015-08-12 | US09856695B2 | 2018-01-02 | Todd J. Leadens, II; Jing (Kelly) Zhang; Ada Mbata; Will J. Roach |
| There is provided a system for an integrated magnetic slider assembly. The system has the integrated magnetic slider assembly with a slider portion, a hanger portion coupled to or integrated with the slider portion, and one or more magnets coupled to the hanger portion. The system further has a longitudinal hanging device configured for coupling to and suspending the slider portion of the integrated magnetic slider assembly. The system further has at least one hanging partition configured for coupling to the hanger portion of the integrated magnetic slider assembly, the at least one hanging partition having a plurality of pleats. All the magnets in a plurality of integrated magnetic slider assemblies are vertically aligned with respect to each other to cause a magnetic attraction between adjacent magnets in order to hold the plurality of pleats together, when the at least one hanging partition is in a retracted position. | ||||||
| 168 | EXPANDABLE CARGO STORAGE, TRANSPORTATION MEANS SECTION, TRANSPORTATION MEANS AND METHOD OF OPERATING A CARGO STORAGE, A TRANSPORTATION MEANS SECTION, OR A TRANSPORTATION MEANS | US15622347 | 2017-06-14 | US20170361932A1 | 2017-12-21 | Claus-Peter GROSS |
| An expandable cargo storage for a transportation means, comprising a first storage wall and a second storage wall opposite of the first storage wall, and a plurality of foldable walls arranged between the first and the second storage wall, each of the plurality of foldable walls being foldable between a first position in which the respective foldable wall is arranged essentially in parallel with the second storage wall, and a second position in which the foldable wall is arranged essentially perpendicularly to the second storage wall, wherein, when each of the foldable walls is arranged in its first position, the cargo storage is in a first operational state enclosing a first volume, and when each of the foldable walls is in its second position, the cargo storage is in a second operational state enclosing a second volume which is larger than the first volume. | ||||||
| 169 | Amenity Monument for Aircraft Cabins | US15477044 | 2017-04-01 | US20170283063A1 | 2017-10-05 | Glenn A. Johnson; Mark P. Dowty |
| Preferred embodiments relate to an amenity monument installed in the middle of a cabin space that absorbs “dead-space” in a seating layout while simultaneously providing features and amenities that are desirable to passengers. In preferred embodiments, this may substantially enhance the array of seating options and configurations available to an aircraft interior designer. In certain embodiments, the amenity monument may be equipped with dimmable panels that are set to a transparent condition during taxi, take-off and landing. During flight, the dimmable panels may be set to a translucent or opaque condition that provides privacy for the passenger utilizing the amenity monument as well as passengers seated nearby. In some embodiments, the monuments may provide enhanced amenities like curved, surround-view screens and which display gaming, advertising, multimedia and/or retail content. | ||||||
| 170 | BULKHEAD ASSEMBLY WITH POCKET DOOR FOR AIRCRAFT INTERIOR | US15310314 | 2015-05-06 | US20170274975A1 | 2017-09-28 | Constantin BOBARU |
| The present disclosure describes a bulkhead assembly for an aircraft interior comprising a pocket door mechanism (48) for supporting and guiding the movement of a pocket door; and a structural member (50) to which the pocket door mechanism is attached. The structural member is attached to a structure of the aircraft and provides support for the pocket door relative to the aircraft structure independently of any decorative member (32, 34) covering the structural member. | ||||||
| 171 | METHOD AND APPARATUS FOR ESTABLISHING AN ENVIRONMENTALLY ISOLATED VOLUME | US15411352 | 2017-01-20 | US20170129609A1 | 2017-05-11 | William Robert Clos |
| A method and apparatus are provided for at least partially environmentally isolating a volume, such as by environmentally isolating the cargo compartment from the passenger compartment of an aircraft. In the context of an apparatus, a barrier curtain is provided that partially defines the volume. The apparatus also includes a cable extending along one or more walls that partially define the volume. The barrier curtain is supported by the cable. The apparatus may also include a cable release mechanism. The cable is held in place by the cable release mechanism and the cable release mechanism is configured to detach the cable at a predetermined load, thereby permitting the barrier curtain to drop in response to a decompression event. | ||||||
| 172 | Panel and Associated Closeout Method | US14856824 | 2015-09-17 | US20170080670A1 | 2017-03-23 | Michael S. Lewis |
| A panel having a layered structure including a core defining a first edge and a face sheet connected to the core, the face sheet including a protruding portion defining a second edge, wherein the second edge protrudes outward a distance from the first edge, and a trim piece connected to the layered structure, the trim piece including a trim member and a flange member extending from the trim member, the trim member defining a visible surface and a trim edge, wherein the trim member is positioned over the first edge, wherein the trim edge is connected to the protruding portion, and wherein the flange member is connected to the layered structure. | ||||||
| 173 | BUFFER ZONE FOR INTERIOR AIRCRAFT FEATURES | US15306241 | 2015-04-20 | US20170043855A1 | 2017-02-16 | Bruce MALEK; Stefan HOLOWKA; Nikolas BEAUDIN |
| Several embodiments of buffer zones are provided that are contemplated to be disposed with respect to two or more adjacent elements on an aircraft. The buffer zones adjust for dynamic spacing between the elements to help control different gapping requirements between the elements installed in the aircraft. Embodiments include an aircraft interior panel configuration, an aircraft interior wall panel configuration, an adjustable width aircraft bulkhead, and an aircraft personal service unit. | ||||||
| 174 | Mounting system for mounting an object in a space of a transportation means and transportation means with a space and at least one such mounting system | US14464033 | 2014-08-20 | US09522734B2 | 2016-12-20 | Seraj Mazidi; Frank Quatmann |
| A mounting system for objects in a transportation system includes a profile rail, at least one locking device with a base body that is bringable in surface contact with a supporting surface of the profile rail and at least one locking body which is interlockable with the profile rail, as well as an actuating device with an actuating element that extends parallel to the profile rail and a clamping body that is connected to the actuating element. The clamping body is realized in such a way that it exerts a compressive force, which results in the locking body being interlocked, upon a component of the locking device during a motion of the actuating element in a first direction parallel to the profile rail and releases the interlock during a motion of the actuating element in a second, opposite direction. | ||||||
| 175 | Systems and methods for positioning a section divider assembly within a vehicle | US14682197 | 2015-04-09 | US09499271B2 | 2016-11-22 | Brent Clarence Walton; William F. Herold; Hung Quang Nguyen; Kevin Duane Bass; Christopher L. Schwitters |
| A section divider system is configured to separate sections within an internal cabin of a vehicle. The section divider system may include a first rail secured to a fixed panel within the internal cabin. A closeout panel may be secured to the fixed panel. The closeout panel extends between the fixed panel and a passenger service unit (PSU) within the internal cabin. A clearance space is formed between a portion of the closeout panel and the PSU. The closeout panel is configured to prevent access to an interior of the PSU. A bracket is secured to the first rail. One or more connecting beams extend from the bracket through the clearance space. A section divider assembly is connected to the connecting beam(s). | ||||||
| 176 | Access Device Provided With A Folding Door Enabling Secure Communication Between At Least Two Zones Of An Enclosure | US15150674 | 2016-05-10 | US20160332718A1 | 2016-11-17 | 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 a folding door which, when in folded position, allows at least one of said openings to be closed and, when in deployed position, forms a security vestibule with at least one movable shutter allowing said opening created by the deployment of said folding door to be closed. By superimposing the main components of the security vestibule that said components allow to close, the device frees up the adjoining cabin space when the security vestibule is not in use. | ||||||
| 177 | Expandable aircraft monument | US14278310 | 2014-05-15 | US09428274B2 | 2016-08-30 | Sabrina Moje; Matthias Breuer |
| An aircraft monument for installation in an aircraft cabin including a first functional module, the first functional module including a side wall for delimiting the first functional module from a region of the aircraft cabin adjacent to the first functional module and/or from a region of the aircraft monument adjacent to the first functional module. The side wall is movable between a first and a second operational position and comprises a side-wall region which merely in the second operational position of the side wall serves for delimiting the first functional module from a region of the aircraft cabin adjacent to the first functional module, so that a movement of the side wall out of its first operational position into its second operational position results in an enlargement of a base area of the first functional module. | ||||||
| 178 | MODULAR CABIN SEGMENT, CABIN FOR A VEHICLE AND VEHICLE WITH A CABIN | US15010387 | 2016-01-29 | US20160144962A1 | 2016-05-26 | Ralf Schliwa; Maria Strasdas |
| A modular cabin segment for a vehicle includes a first lateral segment module accommodating a first toilet arrangement with a toilet compartment, a second lateral segment module, and at least one central module, wherein in each case an outer lateral face of the first segment module and of the second lateral segment module is designed to adapt in each case to an inner wall of a cabin of the vehicle so as to correspond to the aforesaid. At least one of the modules includes a cabin attendant seat that on one side is held on the at least one module so that it can be pivoted on an axis. In this manner very good integration of many different functions in the manner of a construction kit is achieved in order to be able to accommodate a greater number of passenger seats elsewhere within the limited space provided in a cabin. | ||||||
| 179 | DOOR FOR AN AIRCRAFT | US14900973 | 2014-07-11 | US20160144944A1 | 2016-05-26 | William A. GOINGS; Eric LONG |
| 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. | ||||||
| 180 | Toilet arrangement for a vehicle | US14165700 | 2014-01-28 | US09346548B2 | 2016-05-24 | Ralf Schliwa; Andreas Barber; Maria Strasdas |
| A toilet arrangement for a vehicle includes a first toilet compartment, an adjacent second toilet compartment and a partition wall situated between the first toilet compartment and the second toilet compartment, wherein the partition wall is movably supported and designed for being transferred into an open position, in which the partition between the first toilet compartment and the second toilet compartment is removed. This makes it possible to convert two relatively small toilet compartments into a larger toilet compartment that is suitable for use by persons with limited mobility. | ||||||
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