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公开(公告)号：US10227144B2
公开(公告)日：2019-03-12
申请号：US15218792
申请日：2016-07-25
Applicant: Airbus SAS
Inventor： Didier Gendre , Kevin Goburdhun , Alexandre Fouillot
Abstract: A mobile vehicle for supplying pressurized air to an aircraft, the vehicle being configured to tow the aircraft during its movements on the ground and including a pneumatic supply system configured to supply pressurized air to the aircraft, the pneumatic supply system being manually connectable to a high-pressure connector of the aircraft and remotely disconnectable from the connector.
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公开(公告)号：US20190033379A1
公开(公告)日：2019-01-31
申请号：US16037392
申请日：2018-07-17
Applicant: Airbus SAS
Inventor： Benoit Ferran , Clément Dinel
Abstract: A method for estimating a state of energy of a battery, comprising the steps of estimating a state of charge of the battery, determining a discrepancy between the state of charge and the state of energy as a function of the state of charge, computing the state of energy as a function of the estimated state of charge and of the determined discrepancy. Also a battery including apparatus configured to implement the method is provided.
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公开(公告)号：US20190001588A1
公开(公告)日：2019-01-03
申请号：US16017180
申请日：2018-06-25
Applicant: Airbus SAS
Inventor： Patrice LEFEBURE , Jonas BURTH
Abstract: A method for creating a structural part made of composite material by injecting-infusing a liquid, thermosetting resin into a fibrous reinforcement, the structural part comprising a first element and at least one second element. Both the first element and the at least one second element are created in an intermediate state during a distinct injection-infusion step associated with partial curing that is arrested at a degree of cross-linking of the resin below a gelling point of the resin. The first element and the at least one second element are held in a tooling, in a relative position and in a shape that the elements are to have in the structural part to be created, during an out-of-autoclave simultaneous complete curing phase so as to obtain a desired degree of polymerization of the resin of the first element and of the resin of the at least one second element.
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公开(公告)号：US20180363564A1
公开(公告)日：2018-12-20
申请号：US16060305
申请日：2016-12-07
Applicant: Airbus SAS
Inventor： Jean-Francois GENESTE
Abstract: A hybrid power or thrust generator including at least one thermodynamic turbine engine and at least one electric power generator. An electric power generator is electrically connected to at least one electric motor, mechanically and rotatably coupled to one or more rotating portions of the thermodynamic turbine engine, and the electric power generator operates simultaneously with the thermodynamic engine so as to supply the electric motor(s) to reduce the power drawn from the turbines of the thermodynamic turbine engine in operation. The electric power generator may comprise a thermoacoustic engine driving a linear electric alternator. The generator is advantageously implemented in a vehicle, such as an aircraft.
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85.发明授权公开(公告)号：US10150570B2
公开(公告)日：2018-12-11
申请号：US14965926
申请日：2015-12-11
Applicant: AIRBUS SAS
Inventor： Emmanuel Joubert , Benoit Ferran , Antonin Sanitas
IPC: B64D33/08 , H01M10/625 , H01M10/6563 , B64D27/24 , B64D33/10
Abstract: A device for cooling at least one autonomous electric power source of an aircraft, includes: an inlet for air cooling a cooling fluid; the cooling fluid being fed towards at least one autonomous electric power source of the aircraft; a convergent hot air outlet, including moving elements for controlling the air flowrate; and supervision elements of the aircraft, which control the moving elements for controlling the air flowrate depending on the need for cooling of the autonomous electric power source. A method for cooling at least one autonomous electric power source of an aircraft and an aircraft including such a device are also described.
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Patent Agency Ranking
公开(公告)号：US20180346139A1
公开(公告)日：2018-12-06
申请号：US15984638
申请日：2018-05-21
Applicant: Airbus SAS
Inventor： Benoit FERRAN , Emmanuel JOUBERT , Nicolas Fouquet , Jonathan LANDOLT
CPC classification number: B64D27/24 , B64D2027/026
Abstract: A method and an architecture for implementing the method for the management of a hybrid thermal/electrical propulsion aircraft in the course of its various flight phases. The hybrid propulsion receives at each instant i a total power command Ptot,com,i distributed between thermal Pth,com,i and electrical Pe,com,i power commands. The method includes steps of calculating a maximum admissible thermal power command Pth,com,max,i for compliance with acoustic objectives on the ground, selecting the thermal power command Pth,com,i in a bounded range of values, determining the electrical power command Pe,com,i. The thermal Pth,com,i and electrical Pe,com,i power commands supplied by the hybrid propulsion are thus adjusted in the course of the different flight phases depending on a height hi of the aircraft in order to make it possible to comply with acoustic requirements on the ground.
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公开(公告)号：US20180334253A1
公开(公告)日：2018-11-22
申请号：US15773474
申请日：2016-11-09
Applicant: Airbus SAS
Inventor： Jean-Francois GENESTE
Abstract: An aircraft including a fuselage and at least one wing comprising, on the aerodynamic plane, a plurality of distributed airfoils separated from one another, numbering more than 10, and arranged inside an enclosing space bearing on the airfoils. The shape and dimensions of the enclosing space correspond to the shape and dimensions of a simple wing of conventional structure, which is adapted to the aircraft taking account of the weight and flight speed of the aircraft. Advantageously, the airfoils are arranged such that the cross-section of the enclosing space in a vertical plane XZ of the aircraft matches the shape of the aerodynamic profile of the simple wing of conventional structure. The airfoils are arranged, for example, to produce a V formation in plan view, with the tip pointing forwards.
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公开(公告)号：US10124416B2
公开(公告)日：2018-11-13
申请号：US15348135
申请日：2016-11-10
Applicant: Airbus SAS
Inventor： Daniel Aliaga , Dominique Schuster , Fernand Vinhas , Guillaume Abrivard
Abstract: A drill bit having an interior canal for liquid nitrogen to pass longitudinally through the body of the drill bit. The canal has, on the side of a cutting edge of the drill bit, at least one liquid nitrogen ejection duct that opens near the cutting edge which is formed by an insert made with polycrystalline diamond fixed to the body of the drill bit. A device for drilling a metal-composite stack includes the drill bit, a liquid nitrogen production unit and a distribution network to distribute the liquid nitrogen. The device drills through a metal-composite stack in a single pass of the drill bit. The liquid nitrogen at cryogenic temperature is conveyed close to the cutting edge, at least while the cutting edge is in contact with the metallic material.
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公开(公告)号：US10111283B2
公开(公告)日：2018-10-23
申请号：US14470157
申请日：2014-08-27
Applicant: Airbus SAS , Airbus Operations GmbH
Inventor： Christian Karch , Juergen Steinwandel , Heiko Fietzek , Paulin Fideu , Bernard Duprieu
Abstract: An induction heating system and a method for controlling a process temperature for induction heating of a workpiece. The induction heating system comprises an inductor configured to generate an alternating magnetic field in response to an alternating current supplied thereto, a magnetic load comprising a magnetic material, the magnetic material having a Curie temperature and being configured to generate heat in response to the alternating magnetic field being applied thereto, the magnetic load being connectable to the workpiece in a heat-conducting manner so as to transfer the generated heat to the workpiece, and a control unit configured to control the process temperature for manufacturing the workpiece by adjusting the alternating magnetic field when the temperature of the magnetic material is in a temperature control range around or below the Curie temperature of the magnetic material, the temperature control range being dependent on the magnetic material of the magnetic load.
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公开(公告)号：US20180281961A1
公开(公告)日：2018-10-04
申请号：US15937466
申请日：2018-03-27
Applicant: AIRBUS INTERIORS SERVICES (AIS) , AIRBUS (SAS)
Inventor： Sylvain Mariat , Béranger Chantal , Nicolas Ferrere , Nicolas Rios
Abstract: An passenger cabin of an aircraft including a floor (108) on which are mounted a front seat (104a), a rear seat (104b) and a partition wall separating the front and rear seats, wherein the front seat (104a) pivots about an axis perpendicular to the floor (108) through an angle of at least 180 degrees, and the partition wall (106) has a fixed lower portion (106a) and a removable upper portion, and wherein a securing means has a securing position which secures the upper portion to the lower portion (106a), and a release position which allows the upper portion to detach from the lower portion (106a). The pivoting front seat and partition wall with detachable upper portion provide a first configuration seating configures that provides confidentiality between two passengers seated one behind the other, and a second configuration that permits communication between the seated passengers.
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