| 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 | CURTAIN CLIP | US15381543 | 2016-12-16 | US20170172332A1 | 2017-06-22 | Alexandre Legault; Lindsay Willcox; Markus Andreas Hetzler |
| The present invention is a combination of a curtain clip and a curtain slide. The curtain clip includes a socket portion connected to a tab portion. The socket portion has a socket for receiving the ring of the curtain slide when the socket and ring are urged together. Resilient fingers in the clip socket define a slot for receiving the ring shank of the ring of the curtain slide. The body of the curtain clip has a tab portion for fastening to a curtain, either by sewing the tab to curtain, or inserting the tab portion in a pocket in the curtain. | ||||||
| 102 | COVER PANEL FOR A STRUCTURAL COMPONENT | US15363847 | 2016-11-29 | US20170152043A1 | 2017-06-01 | Bastian SCHAEFER; Stefan HOLST; Anna WENGORRA |
| A cover panel for a core panel of a structural aircraft component includes a protection cover having an outer shape corresponding to the outer shape of the core panel and including at least one cutout aperture, and at least one fabric panel mounted to the protection cover and covering the at least one cutout aperture. | ||||||
| 103 | Modular cabin segment, cabin for a vehicle and vehicle with a cabin | US15010387 | 2016-01-29 | US09656751B2 | 2017-05-23 | 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. | ||||||
| 104 | Method and apparatus for establishing an environmentally isolated volume | US13773049 | 2013-02-21 | US09556667B2 | 2017-01-31 | 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. | ||||||
| 105 | Device for separating two zones of a passenger cabin | US14067269 | 2013-10-30 | US09550572B2 | 2017-01-24 | Soenke Jacobsen; Monika Michel |
| A device for separating two zones of a passenger cabin including a frame element and an area element which is fastened to said frame element and includes, at least in certain sections, a flexible stretch material. The separating device is detachably fastenable in such a way to a passenger seat installed in the passenger cabin, that the area element extends substantially in one plane with a backrest of the passenger seat and that the section of the area element which includes of a flexible material is transferrable from a non-tensioned physical state into a flexibly stretched physical state in the event of the backrest of the passenger seat being adjusted from an upright position into a reclined position. | ||||||
| 106 | SELF-ADJUSTING DOOR JAMB FOR AN AIRCRAFT DOOR | US14792231 | 2015-07-06 | US20170008608A1 | 2017-01-12 | Robert J. Telmos |
| The disclosed embodiments relate to an aircraft having an interior door with a self-adjusting door jamb. The self-adjusting door jamb includes a door jamb configured to receive the interior door and a bias mechanism coupled to the door jamb and facilitating movement of the door jamb along an axis. Additionally, an angular translating mechanism coupled to the bias mechanism and facilitating angular displacement of the door jamb relative to the axis. | ||||||
| 107 | Access Device Provided With Independent Mobile Walls Enabling Secure Communication Between At Least Two Zones Of An Enclosure | US15150507 | 2016-05-10 | US20160332717A1 | 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 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. | ||||||
| 108 | MODULAR AIRCRAFT CLOSET | US15098890 | 2016-04-14 | US20160304204A1 | 2016-10-20 | Jefferey McKee |
| A modular aircraft closet including a structural frame having a top, a bottom, an inboard sidewall, an outboard sidewall, an open forward face and an open aft face. A forward panel attaches to the structural frame to cover the open forward face and an aft panel attaches to the structural frame to cover the open aft face. The forward and aft panels can be equipped with an exterior panel feature to customize, brand, reconfigure or retrofit the closet. | ||||||
| 109 | Unique System and Method of Creating Scenes Within a Moving Vehicle Such as an Aircraft | US14645101 | 2015-03-11 | US20160264243A1 | 2016-09-15 | Jagdish T. Madhav |
| A vehicle projection system that includes a projector positioned adjacent a first portion of a ceiling of the vehicle, the projector being configured to project a first image on the first portion of the ceiling. The image may be a moving image or may be various natural sky scenes such as a starry sky. The projector may be a pico-projector or a micro-projector. The vehicle may be an aircraft with the projector positioned on an overhead portion of the cabin. The projector may be positioned between two overhead bins. A second projector positioned on an overhead portion of the cabin may be configured to project a second image on a second portion of the ceiling. The projectors may be positioned on curtain headers within the aircraft. The system may include a control panel that controls the operation of the projectors in conjunction with an onboard sound system, if any. | ||||||
| 110 | Modular cabin segment, cabin for a vehicle and vehicle with a cabin | US13968855 | 2013-08-16 | US09376211B2 | 2016-06-28 | Ralf Schliwa; Maria Strasdas |
| A modular cabin segment for a vehicle includes a first lateral segment module that accommodates a first toilet arrangement with at least one toilet compartment and a second lateral segment 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 at least one 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. | ||||||
| 111 | LIGHT-LIMITING HEADER ASSEMBLY FOR A TRANSITION AREA WITHIN AN INTERIOR CABIN OF AN AIRCRAFT | US14835850 | 2015-08-26 | US20160167786A1 | 2016-06-16 | William H. Maclay; Kevan Withers; Peter J. Zarkowskyj; Charles C. Jensen; Mark E. Wentland; Alexandru Iaszfalvi |
| A header assembly is configured to be secured between an inboard structure and an outboard structure within an internal cabin of an aircraft. The header assembly may include a main body including a first panel connected to an opposed second panel by a base panel. The main body is configured to limit light from passing therethrough. At least three anchoring members are configured to securely connect the main body to at least three reciprocal structures of the inboard and outboard structures. | ||||||
| 112 | Aircraft having a self-erecting partition element in a compartment inside the fuselage | US14706476 | 2015-05-07 | US20150321744A1 | 2015-11-12 | 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. | ||||||
| 113 | DEPLOYABLE FLOOR PANEL ARRANGEMENT FOR AIRCRAFT CABIN AREA | US14699401 | 2015-04-29 | US20150307179A1 | 2015-10-29 | Bernd Ehlers; Mark Herzog |
| A deployable floor panel arrangement for an aircraft cabin area comprising a substantially planar floor panel with at least one foldable seat arrangement mounted thereto. The seat arrangement comprises at least one backrest which is configured to be moveable between a stowed position in which it extends at an angle of approximately 0° to 40° to the plane of the floor panel and a deployed position in which it extends at an angle of approximately 80° to 180° to the plane of the floor panel. | ||||||
| 114 | Divider curtain | US13712854 | 2012-12-12 | US09139301B2 | 2015-09-22 | Kenneth M Slyter; Paul W Morcom |
| A curtain divider for an aircraft interior containing pivot stow bins includes a first fabric curtain, having an outboard end and an inboard end, which is attachable to the aircraft interior only at the outboard and inboard ends. The first fabric curtain includes a vertical portion, and a horizontal portion. The vertical portion has a substantially straight bottom edge, and an arcuate top edge defining a space sufficient for opening the pivot stow bins. The horizontal portion is flexibly attached to the vertical portion along the top edge and extends from the outboard end to the inboard end, having a substantially continuous curvature. The horizontal portion is adapted to impart forward and aft stability to the curtain support member at the top edge. | ||||||
| 115 | Deployable barrier arrangement for selectively blocking a passage in an aircraft cabin | US14538437 | 2014-11-11 | US20150136907A1 | 2015-05-21 | Michael Lau |
| A deployable barrier arrangement for selectively blocking a passage in an aircraft cabin, wherein the barrier arrangement comprises a substantially longitudinal barrier member and a joint unit for fixing the barrier member to an inner wall of the aircraft cabin. The joint unit is configured to allow for a movement of the barrier member between a stowed position in which the barrier member extends substantially parallel to the inner wall of the aircraft cabin and a deployed position in which the barrier member extends at an angle of approximately 60° to 120° to the inner wall of the aircraft cabin. The joint unit is further configured to allow for a rotational movement of the barrier member about a longitudinal axis of the barrier member. | ||||||
| 116 | AIRCRAFT CABIN PARTITION MONUMENT WITH STOWAGE COMPARTMENT | US14470175 | 2014-08-27 | US20150069891A1 | 2015-03-12 | 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. | ||||||
| 117 | 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 | US20150053838A1 | 2015-02-26 | Seraj Mazidi; Frank Quatmann |
| A mounting system for objects in a transportation means 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. | ||||||
| 118 | Method and apparatus for establishing an environmentally isolated volume | US13781004 | 2013-02-28 | US08857762B2 | 2014-10-14 | Brad A. Kauffman |
| 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 attached to a respective wall. The cable is carried by the cable release mechanism and the cable release mechanism is configured to fail at a predetermined load, thereby permitting the barrier curtain to drop in response to a decompression event. | ||||||
| 119 | Aircraft class divider | US13426451 | 2012-03-21 | US08814088B2 | 2014-08-26 | Ralph Martin Burrows |
| Disclosed herein is a divider providing part of a separation between sections of a passenger cabin of a commercial aircraft, the divider comprising several components. One component may be a support arm connected to the frame of an aircraft above a passenger seat, the support arm having an outer edge facing the aisle of the passenger cabin, and an inner edge which is adjacent the face of a luggage compartment when the bucket is in an open position. Another component may be a curtain attached to a lower edge of the support arm and projecting vertically below the support arm. Yet another component may be a rigid view block adjacent the face of the compartment and configured to reposition such that the view block is adjacent the face of the compartment while the compartment is in a closed position, and repositions when the compartment is opened. | ||||||
| 120 | DIVIDER CURTAIN | US13712854 | 2012-12-12 | US20140158310A1 | 2014-06-12 | Kenneth M. Slyter; Paul W. Morcom |
| A curtain divider for an aircraft interior containing pivot stow bins includes a first fabric curtain, having an outboard end and an inboard end, which is attachable to the aircraft interior only at the outboard and inboard ends. The first fabric curtain includes a vertical portion, and a horizontal portion. The vertical portion has a substantially straight bottom edge, and an arcuate top edge defining a space sufficient for opening the pivot stow bins. The horizontal portion is flexibly attached to the vertical portion along the top edge and extends from the outboard end to the inboard end, having a substantially continuous curvature. The horizontal portion is adapted to impart forward and aft stability to the curtain support member at the top edge. | ||||||
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