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Patent Agency Ranking
公开(公告)号：US20170176281A1
公开(公告)日：2017-06-22
申请号：US15386277
申请日：2016-12-21
Applicant: Airbus Defence and Space GmbH , Airbus Operations GmbH
Inventor： Thomas KRUSE , Thomas KÖRWIEN , Alois FRIEDBERGER , Andreas HELWIG
Abstract: The disclosure relates to a component device, in particular for a primary supporting component of an aircraft, which comprises a first component element, a second component element, a bonding providing a connection between the first component element and the second component element, a marker substance device configured to dispense a volatile marker gas to the environment when in contact with the surrounding air and being hermetically sealed from the surrounding air by the first component element, the second component element, and/or the bonding if the bonding is not damaged, and a detector device configured to detect the marker gas dispensed by the marker substance device.
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公开(公告)号：US20170176282A1
公开(公告)日：2017-06-22
申请号：US15386269
申请日：2016-12-21
Applicant: Airbus Defence and Space GmbH , Airbus Operations GmbH
Inventor： Thomas KRUSE , Thomas KÖRWIEN , Alois FRIEDBERGER , Andreas HELWIG
CPC classification number: G01M3/26 , B29C65/48 , B29C65/52 , B29C65/522 , B29C65/526 , B29C65/8246 , B29C66/026 , B29C66/1122 , B29C66/131 , B29C66/474 , B29C66/71 , B29C66/721 , B29C66/73753 , B29C66/73754 , B29C66/73755 , B29C66/73756 , B29C66/7394 , B29C66/742 , B64C1/12 , B64C3/26 , B64D45/00 , B64D2045/0085 , G01M3/04 , G01M3/3272 , G01N3/12 , G01N19/04 , G01N19/08 , B29K2049/00
Abstract: The disclosure relates to a component device, in particular for a primary supporting component of an aircraft, the component device having a first component element, a second component element, a bonding providing a connection between the first component element and the second component element, and a detector device having at least one interior space sensor device configured to measure a change in a pressure and/or a concentration of a gas surrounding the interior space sensor device. The first component element, the second component element, and the bonding confine an interior space. The interior space sensor device is arranged in the interior space.
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公开(公告)号：US20240109642A1
公开(公告)日：2024-04-04
申请号：US18470008
申请日：2023-09-19
Applicant: Airbus Operations GmbH , Airbus SAS
Inventor： Elmar BONACCURSO , Christian THOMAS , Alois FRIEDBERGER , Wolfgang MACHUNZE , Andreas HELWIG , Tassilo WITTE
IPC: B64C1/40
CPC classification number: B64C1/40
Abstract: A multifunctional thermal and acoustic insulation system having a multilayer structure and a plurality of functional components formed integrally and non-exchangeably with the multilayer structure. The multilayer structure has a thermal and acoustic damping performance and comprises, in a stacked arrangement, a continuous first outer layer, a core layer and a continuous second outer layer. The core layer is between the outer layers so that the outer layers cover the core layer at least on opposite sides thereof. Functions of the functional components are related to at least one of the thermal and the acoustic damping performance of the multilayer structure and the functional components are provided on a first outer layer side of the core layer and/or on a second outer layer side of the core layer.
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公开(公告)号：US20240109640A1
公开(公告)日：2024-04-04
申请号：US18475597
申请日：2023-09-27
Applicant: Airbus Operations GmbH , Airbus SAS
Inventor： Christian THOMAS , Alois FRIEDBERGER , Wolfgang MACHUNZE , Andreas HELWIG , Tassilo WITTE , Elmar BONACCURSO
Abstract: A thermal and acoustic insulation system for an aircraft, to be received between an inner surface of an aircraft primary structure, such as an aircraft fuselage structure, and a surface of a panel arrangement delimiting an aircraft cabin, the surface facing away from the aircraft cabin, comprises an insulation package and at least one sensor adapted to measure a level of humidity present in the insulation package. The insulation package comprises a core layer having a thermal and acoustic damping performance, and a packing layer enclosing the core layer. The packing layer is provided with a plurality of normally closed and selectively openable drainage openings which are actuatable to change between their normally closed state and an open state.
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公开(公告)号：US20150021482A1
公开(公告)日：2015-01-22
申请号：US14448724
申请日：2014-07-31
Applicant: Airbus Operations GmbH
Inventor： Gerhard MÜLLER , Paul SUMIT , Andreas HELWIG , Volker BAUMBACH
CPC classification number: G01N21/8914 , G01N15/0205 , G01N21/0317 , G01N21/09 , G01N21/314 , G01N21/3577 , G01N21/359 , G01N21/53 , G01N21/643 , G01N21/85 , G01N21/94 , G01N33/2847 , G01N33/2852 , G01N33/2876 , G01N2021/3148 , G01N2201/0214 , G01N2201/06113 , G01N2201/062 , G01N2201/0621 , G01N2201/0627 , G01N2201/0697
Abstract: The invention relates to a contamination recording apparatus (12) for recording contaminations in a flowing hydraulic fluid (10) to be examined in aircraft (11a), which comprises a conveying device (14) for conveying the flowing hydraulic fluid (10), a light source (34) for exposing the hydraulic fluid (10) flowing in the conveying device (14) to light (46), and a detection device (36) for recording a fraction of the light (46) absorbed by the exposed hydraulic fluid (10), the light source (34) being formed in order to emit light (46) having a wavelength in the near-infrared range. The invention furthermore relates to a hydraulic system (11) equipped with such a contamination recording apparatus (12) and to an aircraft (11a), and also to a method for recording contaminations in a hydraulic fluid (10) flowing in a hydraulic system (11) of an aircraft (11a).
Abstract translation: 本发明涉及一种用于记录飞机（11a）中要检查的流动液压流体（10）中的污染物的污染物记录装置（12），其包括用于输送流动的液压流体（10）的输送装置（14） 用于将在输送装置（14）中流动的液压流体（10）暴露于光（46）的光源（34）;以及用于记录暴露的液压流体吸收的光（46）的一部分的检测装置（36） （10）中，形成光源（34）以发射具有近红外范围波长的光（46）。 本发明还涉及一种配备有这种污染记录装置（12）和飞机（11a）的液压系统（11），还涉及一种在液压系统中流动的液压流体（10）中记录污染物的方法 11）。
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