Real Time Touch



new TOP 200 Companies filing patents this week

new Companies with the Most Patent Filings (2010+)




Real Time Touch

Airbus Ds Gmbh patents


Recent patent applications related to Airbus Ds Gmbh. Airbus Ds Gmbh is listed as an Agent/Assignee. Note: Airbus Ds Gmbh may have other listings under different names/spellings. We're not affiliated with Airbus Ds Gmbh, we're just tracking patents.

ARCHIVE: New 2018 2017 2016 2015 2014 2013 2012 2011 2010 2009 | Company Directory "A" | Airbus Ds Gmbh-related inventors


Receiving spread spectrum signals

A receiver for spread spectrum signals comprising a first part for preprocessing and digitizing a received signal, and a second part for tracking the digitized signal comprising a carrier loop and a code loop. The code loop comprises a generator for a reference receiver signal for correlation with the received signal and the code loop is configured to modify the reference signal to shape a correlation function between the received signal and the reference receiver signal. ... Airbus Ds Gmbh

Emergency services routing proxy cluster management

Systems and methods for clustering emergency services routing proxies are provided. The described features allow a group of esrps running as individual servers or a group of virtual servers, to be referenced using a single uri. ... Airbus Ds Gmbh

Rocket engine

A rocket engine having a thrust chamber bounded by a casing construction with a chamber longitudinal axis. The casing construction includes at least one cooling channel in fluidic connection with a source of a cooling medium. ... Airbus Ds Gmbh

Combustion chamber and method for the production of a combustion chamber

A combustion chamber suitable in particular for use in a rocket engine comprises a combustion space, a first wall enclosing the combustion space and cooling duct fins, which extend from a surface of the first wall and separate adjacent cooling ducts from one another. At least one of the cooling duct fins has at its end facing away from the surface of the first wall a bent section, which at least partially covers a cooling duct adjacent to the cooling duct fin.. ... Airbus Ds Gmbh

Simulation of gravity and device for generating a force acting on an object

A method is used for simulating a gravity acting on an object in space. The method comprises inducing a magnetic moment in the object via generation of an external magnetic field in an environment of the object. ... Airbus Ds Gmbh

Technique for position calculation of a receiver via use of encrypted signals of a public regulated service

A method for determining a position of a receiver via use of encrypted signals of a public regulated service. The method comprises transmitting prn code chips to the receiver by an assistance server. ... Airbus Ds Gmbh

Delay circuit for time offsetting a radiofrequency signal and interference reducing device using said circuit

A delay circuit for time offsetting an input radiofrequency signal, includes an all-pass filter having a given central frequency to linearize a phase-shift of an output signal relative to the input signal as a function of the frequency on a first frequency range; and first and second antiresonant circuits having respectively first and second central frequencies, the all-pass filter and the antiresonant circuits configured to linearize the phase-shift of the output signal relative to the input signal as a function of the frequency on a second frequency range including the first range. The difference between first and second central frequencies is less than 30% of the value of one of both frequencies, the difference between the first central frequency and the given central frequency of the all-pass filter is less than 30% of the value of a highest frequency between the first central frequency and the given central frequency.. ... Airbus Ds Gmbh

Device and method for processing a signal received by a receiver disrupted by a transmitter

A device for processing a received signal by a receiver disrupted by a transmitter, wherein the transmitters and receiver are co-located, includes: a first coupler configured to take a first reference signal; an analogue circuit for processing the first reference signal; a second coupler configured to combine the modified reference signal with the signal received by an antenna of the receiver; a first analogue-to-digital conversion module digitising the first reference signal; the second analogue conversion module digitising the combined signal in order to deliver a digital combined signal to the digital signal-processing device, wherein signal-processing device delivers a resulting digital signal to a data-processing module of the receiver device.. . ... Airbus Ds Gmbh

Injection apparatus for a rocket engine

An injection apparatus for a rocket engine comprises an injection plate which delimits a combustion chamber upstream. The injection apparatus further comprises a plurality of coaxial injection elements distributed in the injection plate, each of which injection elements forms an inner outlet opening, delimited by a central sleeve body, for a first propellant component and an outer outlet opening for a second propellant component. ... Airbus Ds Gmbh

Rocket propulsion system and method for operating a rocket propulsion system

A rocket propulsion system comprises a combustion chamber, a hydrogen-oxygen supply system connected to the combustion chamber, which hydrogen-oxygen supply system is configured to conduct hydrogen and oxygen into the combustion chamber, and a coolant supply system connected to the combustion chamber, which coolant supply system is configured to conduct a combustible coolant into the combustion chamber. An ignition system of the rocket propulsion system is configured to initiate combustion of the hydrogen-oxygen-coolant mixture in the combustion chamber.. ... Airbus Ds Gmbh

Rocket propulsion system and method for operating a rocket propulsion system

A rocket propulsion system comprises a combustion chamber, an oxygen supply system, comprising an oxygen supply duct and being configured to supply oxygen to the combustion chamber, and a hydrogen supply system, comprising a hydrogen supply duct and being configured to supply hydrogen to the combustion chamber. An ignition unit of the propulsion system, to which at least portions of the oxygen and the hydrogen supplied to the combustion chamber can be supplied, is configured to initiate combustion of the oxygen-hydrogen mixture in the combustion chamber. ... Airbus Ds Gmbh

Method for operating a rocket propulsion system and rocket propulsion system

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.. ... Airbus Ds Gmbh

Discharge chamber of an ion drive, ion drive having a discharge chamber, and a diaphragm for being affixed in a discharge chamber of an ion drive

A discharge chamber of an ion drive, an ion drive having a discharge chamber, and a diaphragm for being affixed in a discharge chamber of an ion drive. The discharge chamber comprises a diaphragm, wherein the diaphragm of the discharge chamber comprises a magnet and is disposed and/or affixed in the discharge chamber.. ... Airbus Ds Gmbh

Thermally fragmentable fastening device

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.. ... Airbus Ds Gmbh

09/28/17 / #20170278683

Ion sensor

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. ... Airbus Ds Gmbh

09/14/17 / #20170260491

Transfer device

A transfer device includes at least one pump unit provided for a defined gas transfer between a first, closed-off space of an installation, in particular a photobioreactor installation, and a second space which is separate from the first space. The at least one pump unit is embodied as a selective oxygen pump.. ... Airbus Ds Gmbh

08/17/17 / #20170238226

Progressive toggling of radio frequency band in a relay node

A method of progressive toggling from a first frequency band to a new frequency band, first mobile nodes being previously attached to the relay node, the method including, upon detection by the relay node of interference on the first frequency band, the relay node triggers the progressive toggling which includes: a selection by the relay node of a new frequency band not suffering interference, an occupation of the new frequency band by the relay node, a blocking of access to the connection to the relay node via the first frequency band for at least one second mobile node, a toggling of the first radio communications of the first active mobile nodes from the first frequency band to the new frequency band, and a freeing of the first frequency band by the relay node.. . ... Airbus Ds Gmbh

08/17/17 / #20170237396

Technique for detecting a defect in a multi-junction solar cell

A method for detecting a defect in a multi-junction solar cell is presented. The multi-junction solar cell comprises at least two vertically stacked p-n junctions. ... Airbus Ds Gmbh

06/22/17 / #20170177467

Method for verifying the functionalities of a software intended to be integrated into a cryptographic component, system

The method for validating the status of a memory of a simulator of a cryptographic component able to save data generated by a cryptographic function, includes a step carried out in the simulator including a first execution of a first cryptographic function generating: a first status of the first memory, and a first result of the first command; a step carried out in a test bench including a second execution of a second simplified cryptographic function, with the first and the second functions carrying out the same operations generating: a second status of the memory, and a second result of the second command; a step of validating including comparisons: of the first status and of the second status and of the first result and of the second result.. . ... Airbus Ds Gmbh

06/22/17 / #20170175806

Hinge assembly for a space structure

A hinge assembly comprises first and second tape spring elements, wherein each of the spring elements is configured to connect a first element of a space structure to a second element of the space structure. Each of the first and the second tape spring elements is movable from a folded state into an unfolded state by releasing stored strain energy, to deploy the first and the second element of the space structure. ... Airbus Ds Gmbh

06/15/17 / #20170170867

Blanking using signal-based thresholding schemes

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. ... Airbus Ds Gmbh

06/15/17 / #20170170854

Noise distribution shaping for signals, particularly cdma signals, with mitigation of artifact signals

Noise distribution shaping for signals, particularly for the application in receivers for cdma signals. A method for noise distribution shaping for signals comprises the acts of receiving a signal of interest from a signal transmitter, detecting whether the received signal of interest is present, and if the received signal of interest is present iteratively performing the following acts of adapting at least one blanking threshold or the received signal of interest according to an offset value depending on the amplitude of the received signal of interest, and generating a blanking control signal by comparing the received signal of interest with the at least one blanking threshold, modifying the noise distribution of the received signal of interest by applying blanking of the received signal of interest under control of the blanking control signal.. ... Airbus Ds Gmbh

05/18/17 / #20170141858

Method for estimating a radioelectric propagation channel

A method estimates a channel for radioelectric propagation between a transmitter and a receiver. The transmitter transmits a signal including frames that each use n1 frequency subcarriers, over each of which n1 symbols are transmitted, wherein, among the set of symbols, certain symbols, referred to as pilot symbols, are known to the receiver. ... Airbus Ds Gmbh

05/11/17 / #20170130899

Tank

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.. . ... Airbus Ds Gmbh

05/04/17 / #20170122260

Thrust nozzle

A thrust nozzle, in particular thrust nozzle for a rocket engine, with a convergent wall section, a throat section and a divergent wall section. The divergent wall section has a first region adjacent to the throat section, the wall contour of which region corresponds to a truncated ideal nozzle, and the divergent wall section has a second region facing away from the throat section, which region has a wall contour deviating from the first region.. ... Airbus Ds Gmbh

03/30/17 / #20170093008

Coaxial diplexer and signal coupling device

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. ... Airbus Ds Gmbh

03/30/17 / #20170093003

Polarisation-preserving filter for a dual-polarised waveguide

A polarisation-preserving filter for a dual-polarised waveguide with a basic body that is circular in cross section. Arranged in the interior of the basic body is a plurality of nubs, wherein the nubs are grouped in several rings, due to which a first, predetermined frequency band can be transmitted unobstructed and the transmission of a second, predetermined frequency band can be blocked.. ... Airbus Ds Gmbh

03/23/17 / #20170081042

Interactive system and method for integral emergency unlocking of a locked cockpit door on an airplane

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. ... Airbus Ds Gmbh

03/16/17 / #20170078083

Tracking of signals with at least one subcarrier

A system for tracking a received signal with a subcarrier, the received signal representing a carrier signal modulated with a code signal and with a subcarrier signal. The system comprises independent and cooperatively operating loops: a phase lock loop tracking the carrier signal, a subcarrier lock loop tracking the subcarrier signal, and a delay lock loop tracking the code signal. ... Airbus Ds Gmbh

03/09/17 / #20170070283

Wireless communication unit, integrated circuit, satellite communication system and method for compensating for ionospheric group delay

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. ... Airbus Ds Gmbh

02/16/17 / #20170043549

Honeycomb core for dimensionally stable sandwich components

A honeycomb core for dimensionally stable components (e.g., a reflector) in sandwich construction with a plurality of cells with a triangular cell cross section made from carbon fiber reinforced plastic. The honeycomb core is assembled from flat laminate strips by plugging, wherein the laminate strips have slots running transversely to the extension direction respectively on their longitudinal side. ... Airbus Ds Gmbh

02/09/17 / #20170041852

Method of communication between a battery powered terminal and a base station and associated communication network

A method of communication between a user terminal powered by a battery and a base station allowing optimization of the management of the battery of the user terminal, includes a step of selecting from among terminals, termed surrounding terminals, powered by battery and situated in a zone within range of the base station, terminals whose distance with the user terminal is less than a predetermined distance and whose battery level is greater than a predetermined threshold, termed neighbour terminals, a step of configuring the neighbour terminals and the user terminal by way of a configuration setpoint, a step of transmitting data between the user terminal and the base station according to the configuration setpoint defining at least one neighbour terminal through which the data pass.. . ... Airbus Ds Gmbh

02/09/17 / #20170037814

Catalyst chamber with a catalyst bed embedded therein for a monopropellant thruster of a rocket engine

A catalyst chamber with a catalyst bed embedded therein for a monopropellant thruster of a rocket engine. The catalyst chamber comprises an inlet having a first cross-sectional area through which a propellant can be introduced into the catalyst chamber and an outlet having a second cross-sectional area through which the propellant and/or resulting reaction products can be introduced into a combustion chamber of the thruster. ... Airbus Ds Gmbh

01/26/17 / #20170025191

Material arrangement for fusion reactor and method for producing the same

A material arrangement for a fusion reactor comprising at least one material which is configured as a foam-like carrier material for condensable binding and fusing of hydrogen. The carrier material is provided with positively charged vacancies for condensing hydrogen atoms, small pores for receiving the condensate and for accelerating the condensation after previous penetration of atoms or molecules into these, and large pores for transporting a catalyst into the small pores. ... Airbus Ds Gmbh

01/26/17 / #20170023473

Method for segmenting the data of a 3d sensor produced in the presence of aerosol clouds for increasing the situational awareness and the location detection of obstacles

A method for segmenting the data of a 3d sensor produced in the presence of aerosol clouds and for increasing the situation awareness and the location detection of obstacles involves transforming the sensor data are transformed into a 3d measurement point cloud, determining related subsets as measurement point clusters from the 3d measurement point cloud of an single measurement cycle of the 3d sensor based on the local measurement point density, determining at least one of the characteristic parameters of the individual measurement point clusters, the characteristic parameters including position, orientation in space, and shape, and determining a time variation of the characteristic parameters using the recorded parameters calculated from subsequent measurement cycles, from which the association of a measurement point cluster with a real obstacle or with the aerosol cloud results.. . ... Airbus Ds Gmbh

01/26/17 / #20170022055

Method and apparatus for generating and for fusing ultra-dense hydrogen

A method for generating and for fusing ultra-dense hydrogen in which molecular hydrogen is fed into at least one cavity and catalyzed, where the splitting and subsequent condensation of the molecular hydrogen is initiated on a catalyst of the cavity to form an ultra-dense hydrogen. The ultra-dense hydrogen is exposed to pressure or electromagnetic radiation to initiate fusion of the ultra-dense hydrogen in the at least one cavity and the reaction heat is led out from the at least one cavity. ... Airbus Ds Gmbh

01/19/17 / #20170015442

Landing device for a low gravity lander

A landing device for a low gravity lander having a main body. The landing device comprises a number of leg-like rods attached to the main body, wherein, in a deployment position of the rods, each of the number of rods is inclined with regard to a plane of a first side surface of the main body such that the rods substantially extend in a direction of movement of the low gravity lander. ... Airbus Ds Gmbh

01/12/17 / #20170012759

Method for allocating resources and system implementing said method

A method for allocating radio resources in a wide band radio communication network for uplink communications, the network including cells, each having a base station and terminals, the method including during connection of a first terminal to a first base station of a first cell: performing reference signal quality measurements, defined respectively for the terminals of the cells by each base station, analyzing the interference detected from the first terminal on the uplink communications from the terminals connected to the base stations, the analysis being carried out as a function of the reference signal quality measurements, by each base station, allocating radio resources by the first base station for an uplink communication from the first terminal, as a function of the analysis results on detection of interference from the first terminal on the uplink communications from the other terminals of the cells, the results coming from each cell.. . ... Airbus Ds Gmbh

01/05/17 / #20170003378

Method for automatic classification of radar objects

Classification of radar objects involves processing a received radar signal in an input channel within a number of successive coherent integration intervals (bursts), detecting an object using doppler filter amplitudes, and producing range reports. A number of range reports are combined using a cluster algorithm to form a plot, and adding doppler filter amplitudes of the two azimuthally adjacent bursts from the same range cell each range report. ... Airbus Ds Gmbh








ARCHIVE: New 2018 2017 2016 2015 2014 2013 2012 2011 2010 2009



###

This listing is an abstract for educational and research purposes is only meant as a recent sample of applications filed, not a comprehensive history. Freshpatents.com is not affiliated or associated with Airbus Ds Gmbh in any way and there may be associated servicemarks. This data is also published to the public by the USPTO and available for free on their website. Note that there may be alternative spellings for Airbus Ds Gmbh with additional patents listed. Browse our Agent directory for other possible listings. Page by FreshPatents.com

###