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1.发明申请公开(公告)号：US20200002005A1
公开(公告)日：2020-01-02
申请号：US16455086
申请日：2019-06-27
发明人： Gerd Brüchmann
摘要： An aircraft seat with a voltage supply port associated only with the aircraft seat and/or a data port associated only with the aircraft seat, a voltage supply unit, associated with the aircraft seat and including a voltage input and a voltage output, each of which is connected to another of the voltage supply ports, a switching circuit associated only with the aircraft seat and hooked up between the voltage output and the voltage supply port and/or between the data port and a data network, with which each of the voltage supply port or each of the data port can be activated or deactivated. A control unit is associated only with the aircraft seat and connected to the switching circuit, and a near-field communication reading device connected to the control unit and associated only with the aircraft seat for wireless reception of signals from an external near-field communication sending device, wherein the reading device can receive signals from a predetermined group of predetermined near-field communication signals, and the reading device and control unit adapted for the control unit to activate at least one of the voltage supply ports and/or at least one of the data ports only upon reception of one of the signals by the switching circuit in dependence on the received signal.
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公开(公告)号：US20240359789A1
公开(公告)日：2024-10-31
申请号：US18646050
申请日：2024-04-25
发明人： Alexei VICHNIAKOV
IPC分类号： B64C1/06
CPC分类号： B64C1/068
摘要： A fastener bracket configured to be installed on a holding structure. The fastener bracket is formed as a single piece comprising a plate portion and at least two pins protruding in parallel from a first surface of the plate portion. The at least two pins are at least partially made of a remoldable material. Also a fastener kit comprising such fastener bracket and at least one counter component. Moreover, an aircraft structure comprising at least one fastener bracket or fastener kit. Also an installation method of installing a fastener bracket.
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公开(公告)号：US12131669B2
公开(公告)日：2024-10-29
申请号：US17871571
申请日：2022-07-22
发明人： Robert Jarczyk , Michael Telkamp
CPC分类号： G09F3/10 , G09F3/02 , G09F2003/0202 , G09F2003/0257
摘要： A method for producing a label for affixing in a vehicle. The method includes printing of a substrate layer to yield a basic label form; production of an adhesive film with a first adhesive layer; and sticking the adhesive film to the basic label form using a second adhesive layer to produce the label. Also described is a label kit including a basic label form with a printed substrate layer and an adhesive film, wherein the adhesive film is configured to be stuck to a printed side of the substrate layer of the basic label form.
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公开(公告)号：US12128617B2
公开(公告)日：2024-10-29
申请号：US16903494
申请日：2020-06-17
IPC分类号： B29C64/236 , B29C64/118 , B29C64/241 , B33Y30/00
CPC分类号： B29C64/236 , B29C64/118 , B29C64/241 , B33Y30/00
摘要： A conveying installation by way of which the 3D printing rate can be increased and the reliability of transporting a semi-finished product to be processed in an additive manufacturing machine can be improved. The conveying installation comprises a longitudinal conveying mechanism which conveys the semi-finished product along a conveying direction in that a preferably continuously revolving conveying arrangement, for example a conveyor belt or a conveying belt, engages the semi-finished product in a force-fitting and/or form-fitting manner
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公开(公告)号：US12128605B2
公开(公告)日：2024-10-29
申请号：US18330842
申请日：2023-06-07
CPC分类号： B29C63/42 , B29C63/0021 , B64C1/06 , F16B7/0426 , F16L3/12 , B64C2001/0072
摘要： A reinforcing element for a structural profile, in particular for a round, oval or elliptical structural tube, includes a composite structure, which has a hollow-cylindrical, helically wound mesh of fiber strands which form an inner shell surface configured to receive the structural profile, wherein the fiber strands are respectively embedded in a matrix material, which has an electroactive polymer which can be stretched along a longitudinal extent of the fiber strands by application of an electrical voltage, such that the composite structure can be expanded by application of the electrical voltage to introduce the structural profile into the composite structure and can be shrunk by switching off the electrical voltage to fix the structural profile on the shell surface in the composite structure.
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公开(公告)号：US20240351676A1
公开(公告)日：2024-10-24
申请号：US18421130
申请日：2024-01-24
发明人： Carsten PAUL , Cord HAACK , Sergej KAUFMANN
摘要： An aircraft section for aircraft. The aircraft section comprises at least one flight component, such as a wing assembly and a tail assembly, and a first fuselage component. The flight component is mounted on the first fuselage component. The first fuselage component has a first coupling point designed for releasable connection to a second coupling point on a second fuselage component, in order to form an integrated fuselage of an aircraft when in a coupled state. The first coupling point provides a mechanical coupling with a second coupling point, forms a system infrastructure interface, and provides a data transmission device for integrity checking when the aircraft section is coupled to another aircraft section. The first coupling point likewise provides positioning sensors for guided docking of the aircraft section with another aircraft section in a target position.
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公开(公告)号：US20240343382A1
公开(公告)日：2024-10-17
申请号：US18630256
申请日：2024-04-09
发明人： Dort DAANDELS , Florian LORENZ , Sönke WUNDERLICH
摘要： An aerodynamic system for an aircraft. The aerodynamic system includes a first aerodynamic component configured to be movably coupled to a primary structure of the aircraft, a second aerodynamic component which is movably coupled to the first aerodynamic component and a first panel element coupled to the first aerodynamic component. The first panel element at least partially covers a gap between the first aerodynamic component and the second aerodynamic component. The aerodynamic system further includes a sealing element arranged between the first aerodynamic component and the second aerodynamic component. The sealing element is configured to at least partially block an airflow between the first aerodynamic component and the second aerodynamic component.
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公开(公告)号：US20240343380A1
公开(公告)日：2024-10-17
申请号：US18631807
申请日：2024-04-10
发明人： Luc ANDREANI , Florian LORENZ
摘要： A fairing arrangement for a high-lift mechanism for an aircraft is disclosed including a flap to be arranged at a trailing edge of an aircraft wing, and a mounting and guiding mechanism for the flap. The fairing arrangement includes a flap side fairing unit and a wing side fairing unit. The flap side fairing unit includes a flap side fairing for covering an aft part of the mounting and guiding mechanism and a flap side fairing mount for mounting the flap side fairing to the flap. The wing side fairing unit includes a wing side fairing for covering a forward part of the mounting and guiding mechanism, and a wing side fairing mount for mounting the wing side fairing to the wing. The wing side fairing mount is configured for movably connecting the wing side fairing to the wing such that the wing side fairing is rotatable around an axis directed at least partially in a vertical direction.
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公开(公告)号：US20240332574A1
公开(公告)日：2024-10-03
申请号：US18411209
申请日：2024-01-12
申请人： Airbus Operations GmbH , Airbus SAS
IPC分类号： H01M8/04746 , H01M8/04029 , H01M8/0432 , H01M8/04537
CPC分类号： H01M8/04768 , H01M8/04029 , H01M8/04358 , H01M8/04559 , H01M8/04619 , H01M8/04753 , H01M2250/20
摘要： A method for controlling a fuel cell during operation of the fuel cell by determining a power requirement of a load electrically connected with the fuel cell, sensing an electromotive force of the fuel cell, determining an available electrical power from the fuel cell based on the sensed electromotive force of the fuel cell, calculating a deviation between the determined power requirement of the load and the available electrical power from the fuel cell, and controlling thermal operating parameters of the fuel cell to compensate for the calculated deviation. Also, a fuel cell system configured to perform such a method.
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公开(公告)号：US20240326981A1
公开(公告)日：2024-10-03
申请号：US18602477
申请日：2024-03-12
发明人： Bernhard SCHLIPF , Martin FEES
摘要： A sealing strip for sealing a gap between convexly curved aerodynamic surface elements of an aircraft. The sealing strip has a convexly curved outer side, welting sections at both longitudinal edges of the sealing strip for fixing the sealing strip at the aerodynamic surface elements, and a mid-seal section between the welting sections. The welting sections protrude on an inner side from the mid-seal section. The sealing strip has a first, second, and third length regions, the second length region being located longitudinally between the first and third length region. The welting sections are omitted in the second length region or the welting sections in the second length region are less rigid than the welting sections in the first and third length regions. Further, a control surface arrangement, a wing and an aircraft with such a sealing strip.
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