中科微点-全球专利检索

  1. Login
  2. Sign Up

Search Results

262 records (took 0.014 seconds)

    AIRCRAFT BRAKING
    32.
    发明申请
    AIRCRAFT BRAKING 审中-公开

    公开(公告)号：US20190263510A1

    公开(公告)日：2019-08-29

    申请号：US16285950

    申请日：2019-02-26

    Applicant: AIRBUS OPERATIONS LIMITED ,  AIRBUS OPÉRATIONS (S.A.S.) ,  AIRBUS (S.A.S.)

    Inventor： Andrew BILL ,  Utsav OZA ,  Esther RAMIREZ-PAYA ,  David Joel CLARKE

    IPC: B64C25/42 ,  B60T8/58 ,  B60T8/17

    Abstract: A braking system and a method for applying one or more aircraft wheel brakes according to at least one of a plurality of wheel brake control functions are disclosed. The method includes receiving an indication of an aircraft speed from an aircraft speed indicator, controlling a wheel braking operation of the aircraft according to at least a first wheel brake control function if the aircraft speed indicated by the aircraft speed indicator exceeds a speed threshold, and controlling the wheel braking operation of the aircraft according to at least a second wheel brake control function if the aircraft speed does not exceed the speed threshold. Also disclosed is an aircraft including one or more aircraft wheel brakes and the disclosed braking system.

    AERODYNAMIC PROFILE HAVING A ROUNDED OBLONG HOLLOW CORE MADE OF COMPOSITE MATERIAL REINFORCED WITH A TEXTILE HAVING UNIDIRECTIONAL FIBERS
    34.
    发明申请
    AERODYNAMIC PROFILE HAVING A ROUNDED OBLONG HOLLOW CORE MADE OF COMPOSITE MATERIAL REINFORCED WITH A TEXTILE HAVING UNIDIRECTIONAL FIBERS 审中-公开

    公开(公告)号：US20190023372A1

    公开(公告)日：2019-01-24

    申请号：US16037269

    申请日：2018-07-17

    Applicant: Airbus Operations (S.A.S.) ,  Airbus (S.A.S.)

    Inventor： Rodolphe Trouve ,  Jean-Claude Lacombe ,  Julien Rodes ,  Thomas Schutz

    IPC: B64C3/14 ,  B64C3/26

    Abstract: An aerodynamic profile including a skin defining the outer surface of the aerodynamic profile, a leading edge, a trailing edge and a central portion representing at least 50% of the chord of the profile. The profile includes a hollow core of composite material reinforced with a textile having unidirectional fibers. The hollow core has, in cross section, an oblong shape that is rounded, in particular at each of its ends. The skin bears against the hollow core over the length of the central portion of the aerodynamic profile, both on the pressure side and on the suction side of the profile. The reinforcement with a textile having unidirectional fibers permits an ideal orientation of reinforcing fibers in order to optimize mechanical properties in certain directions. The shape of the hollow core, elongate along the chord of the profile and rounded, lends it great resistance to deformation.

    AIRFOIL EXTENSION FOR AN AIRCRAFT WING
    37.
    发明申请
    AIRFOIL EXTENSION FOR AN AIRCRAFT WING 审中-公开

    公开(公告)号：US20180057143A1

    公开(公告)日：2018-03-01

    申请号：US15666049

    申请日：2017-08-01

    Applicant: AIRBUS (S.A.S.)

    Inventor： Pascal JULE

    IPC: B64C3/54 ,  B64C3/26

    CPC classification number: B64C3/54 ,  B64C3/26 ,  B64C3/48

    Abstract: An airfoil extension for a wing of an aircraft, the airfoil extension including an upper surface wall and a lower surface wall, the upper surface wall and the lower surface wall defining between them a profile of the airfoil extension. A structural reinforcement is disposed along the leading edge of the airfoil extension. The profile of the airfoil is configured to be modified in response to flight conditions (e.g., aerodynamic pressures acting on the upper surface wall and the lower surface wall) experienced by, on, and/or at the airfoil extension.

    Device and method for locating impacts on the outer surface of a body
    38.
    发明授权
    Device and method for locating impacts on the outer surface of a body 有权

    公开(公告)号：US09886531B2

    公开(公告)日：2018-02-06

    申请号：US14604877

    申请日：2015-01-26

    Applicant: AIRBUS (S.A.S.)

    Inventor： Jerome Golenzer ,  Cedric Chamfroy ,  Julien Bardelli

    IPC: G05B13/02 ,  G06F17/50 ,  G01M17/00 ,  G01B21/04

    CPC classification number: G06F17/50 ,  G01B21/04 ,  G01M17/00

    Abstract: A method and device to locate an impact on an outer surface of a body including: locating the impact on the outer surface of a virtual model of the body; selecting a first and a second visual reference element on the virtual model; positioning an acquisition module on the outer surface of the actual body at the impact; measuring, using an acquisition module, measuring distances between the impact and the first visual reference element and between the impact and the second visual reference element; calculating a first arc around the first visual reference element and a second contour around the second visual reference element wherein each arc has a radius equal to one of the measured distances; determining a point of intersection of the first and second contours; and calculating coordinates of the point of intersection on the virtual model to locate the impact on the virtual body.

    SUPPORT DEVICE FOR ACTUATOR, AIR INTAKE SYSTEM AND AIRCRAFT
    40.
    发明申请
    SUPPORT DEVICE FOR ACTUATOR, AIR INTAKE SYSTEM AND AIRCRAFT 审中-公开

    公开(公告)号：US20180002029A1

    公开(公告)日：2018-01-04

    申请号：US15629915

    申请日：2017-06-22

    Applicant: AIRBUS (S.A.S.)

    Inventor： Feng ZHANG ,  Na SHI ,  Ying AN

    IPC: B64D33/02

    Abstract: This disclosure relates to a support device for an actuator. The support device includes a support unit adapted to be mounted to a stationary structure, an attachment unit adapted to be attached to an actuator casing and a single pivot shaft, and the attachment unit is pivotably connected to the support unit via the single pivot shaft. The support device according to the present disclosure has a simple structure and is stable in operation. The present disclosure further relates to an air intake system for an auxiliary power unit, which includes the above support device for the actuator. In addition, the present disclosure further relates to an aircraft including the air intake system for the auxiliary power unit.

Patent Agency Ranking