公开(公告)号：US11053892B2

公开(公告)日：2021-07-06

申请号：US15598473

申请日：2017-05-18

申请人： Airbus DS GmbH

发明人： Ulrich Gotzig ,  Malte Wurdak ,  Joel Deck ,  Manuel Frey

IPC分类号： F02K9/56 ,  F02K9/64 ,  F02K9/95 ,  F02K9/58 ,  F02K9/42

摘要： A method for operating a rocket propulsion system comprises the steps of supplying oxygen to a combustion chamber, supplying hydrogen to the combustion chamber and combusting the oxygen-hydrogen mixture in the combustion chamber. The rocket propulsion system is operated alternately in a first operating mode, in which oxygen and hydrogen are supplied to the combustion chamber in a first mass mixing ratio of oxygen to hydrogen, and in a second operating mode, in which oxygen and hydrogen are supplied to the combustion chamber in a second mass mixing ratio of oxygen to hydrogen that is greater than the first mass mixing ratio.

公开(公告)号：US10396889B2

公开(公告)日：2019-08-27

申请号：US15253332

申请日：2016-08-31

申请人： Airbus DS GmbH

发明人： Jean-Jacques Floch ,  Francis Soualle ,  Jan Wendel

IPC分类号： H04W4/00 ,  H04B7/185 ,  G01S19/07 ,  H04L7/00

摘要： A wireless communication unit for compensating for Ionospheric group delay in a satellite communication system. The wireless communication unit comprises: a receiver configured to receive a multi-carrier signal from a satellite; and a processor coupled to the receiver. The processor is configured to: process the multi-carrier signal to produce a plurality of digital representations of individual carriers of the multi-carrier signal; estimate, from the plurality of digital representations of individual carriers of the multi-carrier signal, a Total Electron Content, TEC, value associated with a communication path between the satellite and the wireless communication unit through Earth's Ionosphere; and apply compensation for Ionospheric group delay subjected to the multi-carrier signal based on the determined TEC value.

公开(公告)号：US10378575B2

公开(公告)日：2019-08-13

申请号：US15473289

申请日：2017-03-29

申请人： Airbus DS GmbH

发明人： Mathias Von Alberti

IPC分类号： F16B31/00 ,  B64G1/62 ,  B64G1/64

摘要： A fastening device for use in a spacecraft comprises a shaft and a head, which is connected by a first solder to the shaft. The first solder comprises a material of which the melting point is lower than the temperature acting on the fastening device on re-entry of a spacecraft equipped with fastening device into the earth's atmosphere.

公开(公告)号：US10141167B2

公开(公告)日：2018-11-27

申请号：US15464800

申请日：2017-03-21

申请人： Airbus DS GmbH

发明人： Franz Georg Hey ,  Christopher Groll

IPC分类号： H01J37/32 ,  B64F5/60

摘要： An ion sensor comprises an electron repelling electrode to be placed at a negative electric potential, and an ion repelling electrode to be placed at a variable positive electric potential. The electron repelling electrode is formed by a diaphragm element having a diaphragm opening for the passage of an ion beam. The ion repelling electrode forms a blind hole which faces the diaphragm opening with its open hole end and the hole surface of which forms a collector face for detecting impinging ions. With such an ion sensor it is possible, for example, to test the energy spectrum of the ions contained in an exhaust plasma plume of an ion thruster.

公开(公告)号：US09878803B2

公开(公告)日：2018-01-30

申请号：US15270104

申请日：2016-09-20

申请人： Airbus DS GmbH

发明人： Harald Frankenberger

IPC分类号： B64D45/00 ,  B64C1/14 ,  G06K9/00 ,  G08C17/02

CPC分类号： B64D45/0015 ,  B64C1/1469 ,  B64D2045/0035 ,  G06K9/00832 ,  G08C17/02

摘要： An interactive system for unlocking a locked airplane cockpit door having at least one ground station and at least one system for transmitting data between the ground station and airplane, including a ground station signal for actuating a door unlock mechanism. The airplane has: a passenger cabin located door unlock request unit to generate a door unlock request signal; a unit to transmit the request signal; at least one image capture unit in the passenger cabin or a cockpit and a unit to transmit images; a unit for receiving a door unlock signal; and an on-board computer, configured to receive the door unlock signal from the receiving unit and activate the door unlock mechanism. The ground station is connected to at least one receiving station for door unlock request and image signals transmitted from airplanes and is provided with or connected to a transmitting unit for door unlock signals.

公开(公告)号：US09691512B2

公开(公告)日：2017-06-27

申请号：US14676052

申请日：2015-04-01

申请人： Airbus DS GmbH

发明人： Berno Spiegelhalder ,  Uwe Keller ,  Ernst Kaeppeler

IPC分类号： G21K1/04 ,  G21K1/10 ,  B29C70/42 ,  B29C70/54 ,  B29C70/46 ,  B29C67/00 ,  B29C53/56 ,  B29C53/82 ,  B29L31/00

CPC分类号： G21K1/10 ,  B29C53/564 ,  B29C53/821 ,  B29C64/112 ,  B29C70/42 ,  B29C70/46 ,  B29C70/545 ,  B29L2031/7728 ,  G21K1/04 ,  G21K1/043

摘要： A chopper disc for a device for the processing of neutron beams is made of carbon fibers and has a concentric, hollow cylindrical recess for receiving a hub for connection to a pivot bearing. The chopper disc also includes a concentric absorber area for absorbing neutrons striking the chopper disc and at least one window in the absorber area through which neutrons of the neutron beam can pass. The carbon fibers extend from the outer periphery of the chopper disc radially in the direction of the recess and contact the recess tangentially.

公开(公告)号：US20170170867A1

公开(公告)日：2017-06-15

申请号：US15377558

申请日：2016-12-13

申请人： Airbus DS GmbH

发明人： Francis Soualle ,  Mathieu Cattenoz

IPC分类号： H04B1/7097 ,  H04B1/7075

CPC分类号： H04B1/7097 ,  H04B1/70755 ,  H04B2001/70706

摘要： An apparatus comprising a blanker configured to provide a plurality of blanked signals, each blanked signal corresponding to a respective correlator channel signal of a plurality of correlator channel signals. The correlator channel signal is obtainable based on the respective blanked signal and a respective signal replica of a plurality of signal replicas, the signal replicas being shifted with respect to each other. The blanker is configured to obtain each blanked signal based on applying a respective thresholding scheme to a respective signal component of a plurality of signal components derived from a received spread-spectrum signal. The respective thresholding scheme is based on the respective signal component and the signal replica based on which the correlator channel signal corresponding to the respective blanked signal is obtainable. A receiver comprising such an apparatus is provided as is a method comprising providing a plurality of blanked signals.

公开(公告)号：US20170130899A1

公开(公告)日：2017-05-11

申请号：US15340455

申请日：2016-11-01

申请人： Airbus DS GmbH

发明人： Kei-Philipp Behruzi ,  Francesco De Rose

IPC分类号： F17C3/04

CPC分类号： F17C3/04 ,  F17C1/12 ,  F17C2201/0157 ,  F17C2201/052 ,  F17C2203/012 ,  F17C2203/014 ,  F17C2203/015 ,  F17C2203/0304 ,  F17C2203/032 ,  F17C2203/0358 ,  F17C2205/013 ,  F17C2221/033 ,  F17C2221/035 ,  F17C2223/0161 ,  F17C2223/033 ,  F17C2223/045 ,  F17C2223/047 ,  F17C2260/033 ,  F17C2270/0105 ,  F17C2270/0168

摘要： A tank or tank system for storing a cryogenic liquid exhibiting at least one collecting container with an upper region and a lower region, so as to hold the cryogenic liquid, at least one arrangement for feeding and discharging liquids and at least one arrangement for feeding and discharging gases, wherein the tank further exhibits at least one frame structure comprising a thermal insulation material.

公开(公告)号：US20170093008A1

公开(公告)日：2017-03-30

申请号：US15279675

申请日：2016-09-29

申请人： Airbus DS GmbH

发明人： Michael Schneider ,  Michael Szymkiewicz

IPC分类号： H01P1/213

CPC分类号： H01P3/123 ,  H01P1/161 ,  H01P1/2133 ,  H01P1/2138 ,  H01P5/16 ,  H04B3/52

摘要： A signal coupling device associating a first frequency band signal and a second, different frequency band, signal in a common waveguide and distributing the signals to two separate waveguides. The device comprises first and second circular waveguides. The second waveguide is coaxially arranged inside a cylindrical interior of the first waveguide. The first waveguide comprises inwardly projecting inner circumference projections in a region occupied only by the first waveguide. The projections activate higher modes from a fundamental mode. The first and second waveguides and the projections cause the superposition of the fundamental and higher modes to produce a wave front having field components in the first frequency band only in a cylindrical ring region between the second waveguide outer circumference and the first waveguide inner circumference, and having field components in the second frequency band only in a cylindrical interior of the second waveguide.

公开(公告)号：US20170070283A1

公开(公告)日：2017-03-09

申请号：US15253332

申请日：2016-08-31

申请人： Airbus DS GmbH

发明人： Jean-Jacques Floch ,  Francis Soualle ,  Jan Wendel

IPC分类号： H04B7/185 ,  H04L7/00

CPC分类号： H04B7/18532 ,  G01S19/07 ,  H04B7/185 ,  H04B7/18508 ,  H04L7/0016 ,  H04L7/0054

摘要： A wireless communication unit for compensating for Ionospheric group delay in a satellite communication system. The wireless communication unit comprises: a receiver configured to receive a multi-carrier signal from a satellite; and a processor coupled to the receiver. The processor is configured to: process the multi-carrier signal to produce a plurality of digital representations of individual carriers of the multi-carrier signal; estimate, from the plurality of digital representations of individual carriers of the multi-carrier signal, a Total Electron Content, TEC, value associated with a communication path between the satellite and the wireless communication unit through Earth's Ionosphere; and apply compensation for Ionospheric group delay subjected to the multi-carrier signal based on the determined TEC value.

摘要翻译： 一种用于补偿卫星通信系统中电离层组延迟的无线通信单元。 无线通信单元包括：被配置为从卫星接收多载波信号的接收机; 以及耦合到接收器的处理器。 所述处理器被配置为：处理所述多载波信号以产生所述多载波信号的各个载波的多个数字表示; 从多载波信号的各个载波的多个数字表示估计与卫星和无线通信单元之间通过地球电离层的通信路径相关联的总电子内容TEC; 并根据确定的TEC值对受多载波信号影响的电离层组延迟进行补偿。