公开(公告)号：WO2016113669A1

公开(公告)日：2016-07-21

申请号：PCT/IB2016/050124

申请日：2016-01-12

Applicant: DRIESSEN AEROSPACE GROUP N.V.

Inventor： WARTENA, Jochem Floris ,  VLAMING, Paul Cornelis

IPC: B32B17/06 ,  B64D11/04 ,  A47B96/20 ,  F21V33/00

CPC classification number: B32B17/10 ,  B32B17/064 ,  B32B17/10137 ,  B32B2307/412 ,  B32B2439/00 ,  B32B2451/00 ,  B32B2457/208 ,  B32B2605/18 ,  B64D11/02 ,  B64D11/04

Abstract: Embodiments of the present invention provide a laminated glass surface (12) for an aircraft or other passenger transportation vehicle surface. Specific features may include a glass substrate (18) that is associated with an adhesive layer (20) to form a laminated glass (12). The glass substrate may be an ultrathin glass substrate and/or a strengthened glass substrate. The laminated glass may then be secured to an aircraft surface.

Abstract translation: 本发明的实施例提供了一种用于飞行器或其他乘客运输车辆表面的夹层玻璃表面（12）。 具体特征可以包括与粘合剂层（20）相关联以形成夹层玻璃（12）的玻璃基板（18）。 玻璃基板可以是超薄玻璃基板和/或加强玻璃基板。 然后可以将夹层玻璃固定到飞机表面。

公开(公告)号：WO2013136279A3

公开(公告)日：2013-09-19

申请号：PCT/IB2013/051993

申请日：2013-03-13

Applicant: DRIESSEN AEROSPACE GROUP N.V.

Inventor： EIJKELENBOOM, Adriaan ,  METZ, Andreas ,  NASTASE, Lucas ,  RATLIFF, Robert

IPC: B64D11/00

Abstract: Disclosed are crew rests that may be powered by the outputs of a fuel cell system or other suitable power source. For example, but not limited to, a combination of the water, oxygen-depleted air, thermal energy and/or electrical energy generated by the fuel cell system may be used to supply the crew rest with its various power and water needs, helping to make the crew rest autonomous from the aircraft's main power systems.

公开(公告)号：WO2006093412A2

公开(公告)日：2006-09-08

申请号：PCT/NL2006/050048

申请日：2006-03-06

Applicant: DRIESSEN AEROSPACE GROUP N.V. ,  VAN LOON, Laurentius Petrus Joseph ,  PORTEGIES, Cornelis Petrus Maria ,  BEETS, Peter Hendrik

Inventor： VAN LOON, Laurentius Petrus Joseph ,  PORTEGIES, Cornelis Petrus Maria ,  BEETS, Peter Hendrik

CPC classification number: B64D11/0007 ,  A47B31/00 ,  A47B2031/002 ,  B29D99/006 ,  B62B3/003 ,  B62B5/0006 ,  B62B2202/67 ,  B64D11/04 ,  Y10T29/49826

Abstract: A device for accommodating objects, in particular for use in an airplane, comprises at least one panel. The panel has at least one outer edge which is provided with a rim in order to form a shock-absorbing edge. The rim comprises plastic that is integrally molded onto the outer edge of the panel. The device can be an airplane trolley, folding trolley, container or galley.

Abstract translation: 用于容纳物体，特别是用于飞机中的物体的装置包括至少一个面板。 面板具有至少一个外边缘，该外边缘设有边缘以形成减震边缘。 边缘包括整体模制在面板的外边缘上的塑料。 该设备可以是飞机推车，折叠推车，集装箱或厨房。

公开(公告)号：WO2013136283A2

公开(公告)日：2013-09-19

申请号：PCT/IB2013/051999

申请日：2013-03-13

Applicant: DRIESSEN AEROSPACE GROUP N.V.

Inventor： HUANG, Kevin ,  NASTASE, Lucas ,  SCHREUDER, Tom ,  HOOGEVEEN, Andreas ,  EIJKELENBOOM, Adriaan ,  MOROZEAU, Cyril ,  ZARROUATI, Olivier

IPC: A47B31/00

CPC classification number: A47B31/02 ,  A47B31/00 ,  A47B31/06 ,  A47B2031/002 ,  A47B2031/003 ,  A47B2031/023 ,  B64D11/0007 ,  B64D2041/005 ,  Y02T90/36

Abstract: Autonomous trolleys include an integrated power source, which energy can be utilized for integrated trolley systems such as a wheel assist module, heating module, and cooling module. The power source may include a fuel cell system or a rechargeable electrical energy storage device or a combination thereof. The rechargeable electrical energy storage device can be charged by any other power source, including a fuel cell system. The trolley can also be equipped with a fuel tank for easy and safe refueling of a fuel cell system.

Abstract translation: 自动推车包括集成的电源，其能量可用于集成的车辆系统，例如车轮辅助模块，加热模块和冷却模块。 电源可以包括燃料电池系统或可充电电能存储装置或其组合。 可充电电能存储装置可以由任何其它电源（包括燃料电池系统）充电。 手推车还可以配备燃料箱，以便燃料电池系统轻松安全地加油。

公开(公告)号：WO2006093410A1

公开(公告)日：2006-09-08

申请号：PCT/NL2006/050046

申请日：2006-03-06

Applicant: Driessen Aerospace Group N.V. ,  VAN LOON, Laurentius, Petrus, Joseph ,  PORTEGIES, Cornelis, Petrus, Maria ,  BEETS, Peter, Hendrik

Inventor： VAN LOON, Laurentius, Petrus, Joseph ,  PORTEGIES, Cornelis, Petrus, Maria ,  BEETS, Peter, Hendrik

IPC: A47B31/00

CPC classification number: A47B31/00 ,  A47B2031/002 ,  Y10T16/54085 ,  Y10T16/558

Abstract: A device for accommodating objects, in particular for use in an airplane, comprising a housing, which has an access opening, as well as a door which is connected to the housing by at least one hinge so as to be pivotable between an open position and a closed position. The hinge defines a pivot axis for pivoting the door. The access opening is at least partially clear in the open position of the door and the access opening is at least partially closed off by the door in the closed position of the door. The door is lockable relative to the housing in its closed position. The door, in its closed position, is movable in a direction which extends substantially parallel to the pivot axis between a locked position and an unlocked position. The door, in its locked position, is locked relative to the housing, and the door, in its unlocked position, is pivotable about the pivot axis.

Abstract translation: 一种用于容纳特别用于飞机的物体的装置，包括具有进入开口的壳体以及通过至少一个铰链连接到壳体的门，以便能够在打开位置和 关闭位置 铰链限定了用于枢转门的枢轴。 进入口在门的打开位置至少部分地清晰，并且进入口至少部分地被门关闭在门的关闭位置。 门相对于外壳处于关闭位置可锁定。 门处于其关闭位置，可在锁定位置和解锁位置之间沿基本上平行于枢转轴线延伸的方向移动。 门在其锁定位置相对于壳体被锁定，并且在其解锁位置的门能够围绕枢转轴线枢转。

公开(公告)号：WO2004071239A1

公开(公告)日：2004-08-26

申请号：PCT/NL2004/000104

申请日：2004-02-12

Applicant: DRIESSEN AEROSPACE GROUP N.V. ,  VAN LOON, Laurentius, Petrus, Joseph ,  GELUK, Joost, Cornelis

Inventor： VAN LOON, Laurentius, Petrus, Joseph ,  GELUK, Joost, Cornelis

IPC: A47B31/02

CPC classification number: B64D11/0007 ,  A47B31/02 ,  B62B2202/67 ,  B62B2204/02 ,  B62B2204/04 ,  B62B2204/06 ,  F25B21/02 ,  F25B2321/0251 ,  F25D19/003 ,  F25D2317/0655 ,  F25D2317/0665

Abstract: The invention relates to a cooling unit (1) for a service trolley for use in an aircraft or train. The cooling unit (1) comprises a drawer. The drawer contains a layer of heat-insulating material (29) and one or more Peltier elements (42) located in said layer (29) with a warm side (43) facing the one side of the heat-insulating layer (29) and a cold side (44) facing the other side of the heat-insulating layer (29). First fans (32) are provided on the cold side (44) of the heat-insulating layer (29) and second fans (33) are provided on the warm side (43) of the heat-insulating layer (29). The invention furthermore relates to a service trolley provided with a cooling unit (1) according to the invention as well as to a rack (60) for a multiplicity of cooling units (1) according to the invention. Finally, the invention relates to an aircraft or train containing a cooling unit or service trolley according to the invention.

Abstract translation: 本发明涉及一种用于飞机或火车中的服务手推车的冷却单元（1）。 冷却单元（1）包括抽屉。 抽屉包含位于所述层（29）中的隔热材料层（29）和一个或多个珀耳帖元件（42），其中温热面（43）面向绝热层（29）的一侧，并且 面对隔热层（29）的另一侧的冷侧（44）。 第一风扇（32）设置在绝热层（29）的冷侧（44）上，第二风扇（33）设置在绝热层（29）的暖侧（43）上。 本发明还涉及一种具有根据本发明的冷却单元（1）的服务手推车以及根据本发明的用于多个冷却单元（1）的搁架（60）。 最后，本发明涉及一种包含根据本发明的冷却单元或服务台车的飞机或列车。

公开(公告)号：WO2017037580A1

公开(公告)日：2017-03-09

申请号：PCT/IB2016/055051

申请日：2016-08-24

Applicant: DRIESSEN AEROSPACE GROUP N.V.

Inventor： KLEIS, Reinier ,  PORTEGIES, Kees

IPC: B65D88/14 ,  B65D90/02

CPC classification number: B65D90/008 ,  B65D88/14 ,  B65D90/021

Abstract: Embodiments of the invention described herein thus provide systems and methods for improved securement of a cargo cover/flexible door to a cargo container. The systems generally provide securement using cooperating frame securement features positioned on the cargo container and securement plates positioned on door straps of the cargo cover.

Abstract translation: 因此，本文所述的本发明的实施例提供了用于将货物盖/柔性门固定到货物集装箱的系统和方法。 这些系统通常使用位于货物集装箱上的协作框架固定特征和位于货物盖的门带上的固定板来提供固定。

公开(公告)号：WO2014035244A1

公开(公告)日：2014-03-06

申请号：PCT/NL2013/050625

申请日：2013-08-29

Applicant: DRIESSEN AEROSPACE GROUP N.V.

Inventor： Korenromp, Maarten Michiel ,  Schiphorst, Remko

IPC: B64D11/04

CPC classification number: B64D11/00 ,  F16B2/06 ,  Y10T403/32091

Abstract: The invention relates to a locking assembly for locking an aircraft interior structure(13)to an internal mounting frame (2) comprising :a sliding element (1) which is suitable for insertion in the internal mounting frame (2),a height adjustment assembly, comprising a lower and an upper height adjustment part (4, 5). The assembly further comprises a fitting (6) attachable to the aircraft interior structure, having a recess wherein a projection (19) of the upper height adjustment part (5) is received, wherein the fitting (6) can be moved with respect to the projection(19) in a plane defined by X 1 - and Y 1 - directions. Further provided is a locking bolt (11) received in the upper height adjustment part (5) for locking the fixation element(9), the fitting(6), and the height adjustment parts(4, 5) to the sliding element (1).

Abstract translation: 本发明涉及一种用于将飞行器内部结构（13）锁定到内部安装框架（2）的锁定组件，包括：适于插入内部安装框架（2）中的滑动元件（1），高度调节组件 ，包括下部和上部高度调节部分（4,5）。 组件还包括可附接到飞行器内部结构的配件（6），具有凹部，其中容纳上部高度调节部分（5）的突起（19），其中，所述配件（6）能够相对于 突起（19）在由X1-和Y1-方向限定的平面内。 还提供了一种容纳在上部高度调节部分（5）中的锁定螺栓（11），用于将固定元件（9），配件（6）和高度调节部件（4,5）锁定到滑动元件（1） ）。

公开(公告)号：WO2014035241A1

公开(公告)日：2014-03-06

申请号：PCT/NL2013/050622

申请日：2013-08-29

Applicant: DRIESSEN AEROSPACE GROUP N.V.

Inventor： KORENROMP, Maarten Michiel

IPC: B64D11/04

CPC classification number: B64D11/04 ,  F16B1/0071 ,  F16B5/0233

Abstract: The invention relates to a locking assembly (16) for locking an aircraft interior structure, such as a galley, to an aircraft main support structure, such as a floor hard point, comprising : -a cylindrical adjustment bushing (4) having a hollow cylindrical space (15), the adjustment bushing having an outer thread (12) that engages an inner thread of a through-hole (3) arranged in a fitting (7) attachable to or part of the aircraft interior structure, wherein the adjustment bushing can be rotated around its centre line to adjust the height of the fitting in a Z-direction, -a cylindrical outer eccentric bushing (2) inserted in the hollow cylindrical space (So) of the adjustment bushing, the outer eccentric bushing having an eccentric longitudinal hollow cylindrical space whose centre line is placed at a distance from the centre line of the cylindrical outer eccentric bushing, -a cylindrical inner eccentric bushing (1) inserted in the hollow cylindrical space of the outer eccentric bushing, the inner eccentric bushing having an eccentric longitudinal hollow cylindrical space (Si) whose centre line is placed at a distance from the centre line of the inner eccentric bushing, the inner and outer eccentric bushings (1, 2) allowing adjustment of the fitting in a plane perpendicular to the Z-direction, -a locking bolt (8) inserted in the hollow cylindrical space of the inner eccentric bushing, the locking bolt engaging an elongated projection (18) to lock the assembly (16), wherein the adjustment bushing is provided with a visual indicator (17) for indicating its relative position in Z-direction with respect to the fitting. The invention also relates to an aircraft comprising such a locking assembly, as well as a method for locking an aircraft interior structure to an aircraft main support structure.

Abstract translation: 本发明涉及一种用于将诸如厨房的飞行器内部结构（例如厨房）锁定到飞机主支撑结构（例如地板硬点）的锁定组件（16），包括： - 具有中空圆柱形的圆柱形调节衬套（4） 空间（15），所述调节衬套具有与布置在可附接到所述飞行器内部结构的一部分的配件（7）中的通孔（3）的内螺纹接合的外螺纹（12），其中所述调节衬套 围绕其中心线旋转以调节配件在Z方向上的高度， - 插入调节衬套的中空圆柱形空间（So）中的圆柱形外偏心衬套（2），外偏心衬套具有偏心纵向 中心圆柱形空间的中心线与圆柱形外偏心衬套的中心线相距一定距离， - 一个插入外偏心套筒中空圆柱形空间的圆柱形内偏心衬套（1） g，内偏心衬套具有偏心纵向中空圆柱形空间（Si），其中心线与内偏心衬套的中心线相距一定距离，内外偏心衬套（1,2）允许调整配件 在垂直于Z方向的平面中， - 插入在内部偏心衬套的中空圆柱形空间中的锁定螺栓（8），锁定螺栓与细长突起（18）接合以锁定组件（16），其中调节 衬套设置有用于指示其相对于配件在Z方向上的相对位置的视觉指示器（17）。 本发明还涉及一种包括这种锁定组件的飞行器以及用于将飞行器内部结构锁定到飞行器主支撑结构的方法。

公开(公告)号：WO2016128944A1

公开(公告)日：2016-08-18

申请号：PCT/IB2016/050765

申请日：2016-02-12

Applicant: DRIESSEN AEROSPACE GROUP N.V.

Inventor： PORTEGIES, Cornelis ,  KLEIS, Reinier

IPC: B65D88/14 ,  B65D90/02

CPC classification number: B65D88/14 ,  B65D90/021

Abstract: Embodiments of the invention described herein thus provide systems and methods for improved securement of a cargo cover/flexible door to a cargo container. The systems generally provide securement using an integrated hook shape that is formed into the frame extrusions of the cargo container. This internal shape provides a construction that is less vulnerable to damage, can reduce the repair ratio, and the out of service time for the unit.

Abstract translation: 因此，本文所述的本发明的实施例提供了用于将货物盖/柔性门固定到货物集装箱的系统和方法。 这些系统通常使用形成在货物集装箱的框架挤压件中的集成的钩形状提供固定。 这种内部形状提供了一种不易受到损坏的构造，可以减少维修率和设备的停机时间。