公开(公告)号：US20230377811A1

公开(公告)日：2023-11-23

申请号：US18319257

申请日：2023-05-17

Applicant: Airbus Operations GmbH ,  Airbus S.A.S.

Inventor： Peter Linde ,  Alois Friedberger ,  Andreas Helwig

IPC: H01H1/58 ,  H01H1/00 ,  H01H3/00

CPC classification number: H01H1/5822 ,  H01H1/0094 ,  H01H2003/007 ,  H01H2300/036 ,  B64D2221/00 ,  H01H2207/008

Abstract: A component for an aircraft includes at least one connection interface, wherein the connection interface is configured to simultaneously establish an electrical connection and a mechanical connection. An electrical system for an aircraft and a method for connecting components for an aircraft are disclosed.

公开(公告)号：US09651501B2

公开(公告)日：2017-05-16

申请号：US14448724

申请日：2014-07-31

Applicant: Airbus Operations GmbH

Inventor： Gerhard Müller ,  Sumit Paul ,  Andreas Helwig ,  Volker Baumbach

IPC: G01N21/89 ,  G01N15/02 ,  G01N33/28 ,  G01N21/31 ,  G01N21/35 ,  G01N21/85 ,  G01N21/3577 ,  G01N21/359 ,  G01N21/03 ,  G01N21/09 ,  G01N21/53 ,  G01N21/64 ,  G01N21/94

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).

公开(公告)号：US10732066B2

公开(公告)日：2020-08-04

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

IPC: G01M3/20 ,  B29C65/82 ,  B29C65/00 ,  G01M3/22 ,  B29C65/48 ,  B64F5/60 ,  B29C65/52 ,  B29L31/30

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.

公开(公告)号：US10429265B2

公开(公告)日：2019-10-01

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

IPC: G01M3/26 ,  G01M3/04 ,  G01N19/08 ,  B29C65/48 ,  B29C65/82 ,  B29C65/00 ,  G01M3/32 ,  G01N3/12 ,  G01N19/04 ,  B64C1/12 ,  B64C3/26 ,  B64D45/00 ,  B29C65/52

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.