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公开(公告)号：US20240359808A1
公开(公告)日：2024-10-31
申请号：US18646087
申请日：2024-04-25
发明人： Peter LINDE , Matthias HEGENBART
CPC分类号： B64D37/06 , B64D37/04 , F17C13/06 , F17C2201/0109 , F17C2221/012 , F17C2260/016 , F17C2265/066 , F17C2270/0189
摘要： A tank comprising one or several anti-sloshing wall arrangements, with a frame portion and a door portion wherein the frame portion is fixed to a tank wall of the tank, and it edges an opening, and wherein the door portion is configured to selectively close or unclose the opening. Also an aircraft comprising such tank and at least one engine, the engine being configured to be fed with fuel, in particular with liquid hydrogen, contained in the tank.
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公开(公告)号：US20240282998A1
公开(公告)日：2024-08-22
申请号：US18441117
申请日：2024-02-14
发明人： Matthias HEGENBART , Peter LINDE
IPC分类号： H01M8/2484 , B64D27/355
CPC分类号： H01M8/2484 , B64D27/355 , H01M2250/20
摘要： A manifold plate for a fuel cell including a plurality of openings for leading reactants towards and/or away from the fuel cell and at least one magnet providing a magnetic field which is oriented in a direction of the stack of the fuel cell. The manifold plate defines a main direction which may be seen as in a direction of a stack including electrodes forming the fuel cell. The openings of the manifold plate may be arranged along the main direction of the manifold plate and the magnet of the manifold plate may be arranged between two of the openings and may be oriented so that the direction between north pole and south pole of the magnet corresponds to the main direction.
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3.发明申请公开(公告)号：US20190135453A1
公开(公告)日：2019-05-09
申请号：US16172564
申请日：2018-10-26
摘要： Disclosed here is a transfer system for transferring luggage into a vehicle having a freight hold opening and a passenger compartment opening arranged at the same level outside the vehicle. The system has a luggage transfer element and a passenger bridge, wherein the passenger bridge has a transition zone that can be simultaneously connected to the freight hold opening and the passenger compartment opening. The luggage transfer element has a housing module for receiving luggage, and a movement module for transferring the luggage transfer element. The luggage transfer element can be transferred through the transition zone and the freight hold opening by way of the movement module. The system avoids delays as the passengers are boarding and simplifies the transfer of luggage into a freight hold.
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4.发明申请公开(公告)号：US20170133135A1
公开(公告)日：2017-05-11
申请号：US15348337
申请日：2016-11-10
CPC分类号： H01F7/0294 , G01N21/88 , G01N21/954 , G01N27/9006 , G01N27/902 , H01F6/00 , H01F6/04 , H01F7/0257 , H01F7/06 , H01F7/20 , H01F7/206 , H02N15/04
摘要： This relates to an inspection apparatus for inspecting a structural component to which access is restricted, comprising a movable unit including a superconductor and an inspection device, a drive unit including a magnetic field generator adapted to generate a magnetic field, wherein said movable unit and said drive unit are arranged with a predetermined gap therebetween for receiving said structural component and are coupled in a force-locking manner by means of the frozen magnetic flux, i.e., without a physical connection, between the magnetic field generator and the superconductor. Thus, spaces or areas to which access is restricted can be inspected without the need of physically connecting the drive unit and the movable unit.
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公开(公告)号：US20210237859A1
公开(公告)日：2021-08-05
申请号：US17159829
申请日：2021-01-27
IPC分类号： B64C23/06
摘要： A vortex generator apparatus for an aircraft includes a surface section having a receiving recess, a vortex generator having a first edge, an opposite second edge and a vortex generator surface component extending from the first edge to the second edge, wherein the first edge is fixedly arranged in or adjacent to the receiving recess. The vortex generator surface component includes at least one electroactive polymer assembly, wherein the at least one electroactive polymer is switchable into an extended state by applying an electrical voltage and into a neutral state by removing the electrical voltage. The electroactive polymer assembly and the vortex generator surface component are configured to retract the vortex generator surface component completely into the receiving recess in the neutral state of the electroactive polymer assembly and to extend the vortex generator surface component from the receiving recess in the extended state.
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6.发明申请公开(公告)号：US20200339267A1
公开(公告)日：2020-10-29
申请号：US16859148
申请日：2020-04-27
IPC分类号： B64D11/06
摘要： An aircraft seat fastening assembly, due to the use of electroactive polymers, facilitates the compensation of tolerances and the fastening of aircraft seats in the passenger cabin of the aircraft. A fixing actuator contains the electroactive polymer and can be switched electrically between a fixed state, in which a movement of a fastening region is not possible, and a non-fixed state, in which a movement of the fastening region is possible in a vertical direction. The aircraft seats can thereby be displaced in a continuously variable manner along the aircraft seat fastening rail. The aircraft seats can also be locked in a fully automated manner, and possibly from a central location. It is also conceivable to individually control the aircraft seats and/or the group(s) of seats.
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公开(公告)号：US20200172222A1
公开(公告)日：2020-06-04
申请号：US16695544
申请日：2019-11-26
发明人： Peter LINDE , Matthias HEGENBART
摘要： A door arrangement for an aircraft comprising a door designed to close an aperture in an outer skin of the aircraft, and a articulated arm which is fixed by a first end to the door and which is designed to move the door in at least two translational directions and at least two rotational directions. An aircraft area with this door arrangement and an aircraft having such an aircraft area are furthermore provided. The aircraft area comprises a door aperture arranged in an outer skin of an aircraft, and a door arrangement. Here the door of the door arrangement may be designed to close the door aperture from an inside of the outer skin, and the articulated arm of the door arrangement may be fixed to the aircraft area.
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公开(公告)号：US20170297270A1
公开(公告)日：2017-10-19
申请号：US15486949
申请日：2017-04-13
CPC分类号： B29C65/548 , A44B18/00 , A44B18/0003 , A44B18/0007 , A44B18/0011 , A44B18/0015 , A44B18/0019 , A44B18/0038 , A44B18/0042 , A44B18/0046 , A44B18/0049 , A44B18/0053 , A44B18/0057 , A44B18/0061 , A44B18/0065 , A44B18/008 , B29C65/48 , B29C65/56 , B29C66/1122 , B29C66/1142 , B29C66/30321 , B29C66/30325 , B29C66/3034 , B29C66/43 , B29C66/474 , B29C66/5221 , B29C66/5261 , B29C66/5268 , B29C66/54 , B29C66/69 , B29C66/7212 , B29L2031/3076 , B64F5/10 , F16B11/006 , Y10T428/24017 , B29K2307/04
摘要： A connection system has a first adhesion segment, on which a first connection region is formed, a second adhesion segment, on which a second connection region is formed, and a solidifiable liquid connection substance for connecting the two adhesion segments in a material fit, wherein at least one of the two connection regions is formed flexibly, such that, when the liquid connection substance is introduced between the two connection regions which are opposite one another in an assembly arrangement of the two adhesion segments, a material connection is formed between the two connection regions automatically as a result of the elastocapillary effect via the liquid connection substance.
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公开(公告)号：US20240308642A1
公开(公告)日：2024-09-19
申请号：US18594422
申请日：2024-03-04
摘要： A vehicle with a cabin comprising an adaptive rail system. The cabin includes a connection area adapted to hold the adaptive rail system. The adaptive rail system includes a rail interface, configured to be attachable to the connection area, at least one installation rail, configured to be attachable to the rail interface, and a jig. The jig is connected to the at least one installation rail in a moveable manner, such that a module attached to the jig is movable inside the cabin.
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公开(公告)号：US20230378485A1
公开(公告)日：2023-11-23
申请号：US18319663
申请日：2023-05-18
发明人： Matthias HEGENBART , Peter LINDE
IPC分类号： H01M8/0258
CPC分类号： H01M8/0258 , H01M2250/20 , H01M8/24
摘要： A bipolar plate for a fuel cell stack comprises a first main boundary surface and a second main boundary surface, arranged parallel and at a distance to each other and define an interior space. A plurality of lateral delimiting surfaces extend between outer edges of the first and second main boundary surfaces to enclose the interior space. At least one of the lateral delimiting surfaces comprises a plurality of lateral openings and at least one of the main boundary surfaces comprises a plurality of axial openings. Internal distribution channels are arranged inside the interior space in a distance to the first main boundary surface and the second main boundary surface, and lateral openings are in fluid connection with the axial openings through at least a part of the internal distribution channels.
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