中科微点-全球专利检索

  1. Login
  2. Sign Up

Search Results

46 records (took 0.022 seconds)

    Method and system for the powered self push back of an aircraft
    11.
    发明专利
    Method and system for the powered self push back of an aircraft 未知

    公开(公告)号：GB2509803A

    公开(公告)日：2014-07-16

    申请号：GB201315874

    申请日：2012-02-08

    Applicant: BOREALIS TECH LTD ,  NEAL GILLERAN

    Inventor： THOMPSON GILBERT ,  COX ISAIAH WATAS ,  GOLDMAN JOSEPH

    IPC: B64C25/40 ,  B64C25/50

    Abstract: A powered self push back method and system for an aircraft are provided to move an aircraft on the ground safely during push back without assistance from an external tug vehicle or the aircraft main engines. The method employs constant cooperative communication and signals between the pilot and the ground crew during the push back process to ensure that push back of the aircraft is safe, efficient, and reduces aircraft turnaround time. The powered self push back system used in conjunction with this method includes at least one powered self-propelled aircraft drive wheel powered by a wheel drive assembly that can be activated by pilot input controls or by remote control exteriorly of or interiorly to the aircraft in response to ground crew signals to activate the driver to rotate the drive wheel in a reverse, push back direction, causing the aircraft to move in the push back direction or in a forward direction for taxi and takeoff in accordance with activation of the controls.

    Integrated aircraft ground navigation control system
    13.
    发明专利
    Integrated aircraft ground navigation control system 未知

    公开(公告)号：GB2499750A

    公开(公告)日：2013-08-28

    申请号：GB201309587

    申请日：2011-11-02

    Applicant: BOREALIS TECH LTD

    Inventor： EDELSON JONATHAN ,  GILLERAN NEAL ,  COX ISAIAH WATAS ,  PERKINS SCOTT ,  SWEET ROBERT M

    IPC: B64C25/40 ,  B64C25/50 ,  B64F1/22 ,  G08G5/06

    Abstract: An aircraft ground control system that moves an aircraft on the ground between landing and take off without external mechanical assistance from airport tugs or tow vehicles or reliance on thrust produced by the aircraft's engines is provided. The aircraft ground control system interfaces only with an aircraft auxiliary power unit or other aircraft power supply, but otherwise operates independently of aircraft systems. A system integrator and controller links cockpit controls designed to actuate the transmission of power to system components and to activate system components only under predetermined conditions with selectively activatable drivers in driving connection with one or more aircraft wheels to move the aircraft on the ground at selected torgues and speeds.

    Aircraft passenger boarding system
    16.
    发明专利
    Aircraft passenger boarding system 未知

    公开(公告)号：GB2524158A

    公开(公告)日：2015-09-16

    申请号：GB201501816

    申请日：2015-02-04

    Applicant: BOREALIS TECH LTD

    Inventor： COX JOSEPH J ,  COX ISAIAH WATAS

    IPC: G06Q90/00 ,  G06Q50/30

    Abstract: An aircraft passenger boarding method comprises providing an aircraft 10 which is equipped for pilot-controllable engines-off taxi that enables a pilot to drive the aircraft without engines in a forward direction into and out of an optimum gate parking orientation, which may be parallel or angled, that permits terminal connections to both forward and aft doors 18, 20 on a terminal-facing side of the aircraft 10. Selected defined classes of passengers board the aircraft separately, through a designated loading bridge 14 connected to a forward door 18 or through a designated loading bridge 16 connected to an aft door 20, to be seated in a designated front or rear aircraft section (11, 13, Fig 3A). An airline may flexibly allocate variably sized sections of the aircraft interior for each defined class, depending on the relative numbers of passengers in each class. Airport terminal interior gate space may be used to separate passenger classes as required for separate boarding through a forward door 18 or an aft door 20.

    Remote control of an aircraft parking brakes and/or APU
    18.
    发明专利
    Remote control of an aircraft parking brakes and/or APU 未知

    公开(公告)号：GB2450796A

    公开(公告)日：2009-01-07

    申请号：GB0811937

    申请日：2008-07-01

    Applicant: BOREALIS TECH LTD

    Inventor： EDELSON JONATHAN SIDNEY ,  COX ISAIAH WATAS

    IPC: B64C25/44

    Abstract: An apparatus 102 for remotely controlling an aircraft 108 having a self-propelled nosewheel 106, on the ground, comprises parking brakes; an APU on said aircraft; control means for applying and releasing said parking brakes 118; control means for turning on and off said APU 116; transmitting means for transmitting information to said parking brakes and said APU; receiving means for receiving information at said parking brakes; and receiving means for receiving information at said APU. The remote control may further comprise means for control the speed of the aircraft, the direction of motion of the aircraft, an emergency stop button and a fire suppression feature.

    Low work-function electrode
    20.
    发明专利
    Low work-function electrode 未知

    公开(公告)号：AU1274099A

    公开(公告)日：1999-05-10

    申请号：AU1274099

    申请日：1998-10-22

    Applicant: BOREALIS TECH LTD

    Inventor： EDELSON JONATHAN SIDNEY ,  COX ISAIAH WATAS

    IPC: C23C14/12 ,  F25B21/00 ,  H01J1/02 ,  H01J1/13 ,  H01J1/14 ,  H01J1/30 ,  H01J21/04 ,  H01J21/10 ,  H01J45/00 ,  C23C16/00

    Abstract: Methods for making low work function electrodes either made from or coated with an electride material in which the electride material has lattice defect sites are described. Lattice defect sites are regions of the crystal structure where irregularities and deformations occur. Also provided are methods for making electrodes which consist of a substrate coated with a layer of a compound comprised of a cation complexed by an electride former, in which said complex has lattice defect sites. In addition, methods for making electrodes which consist of a bulk metal coated with a layer of an electride former having lattice defect sites are described. The electride former stabilizes the loss of electrons by surface sites on the metal, lowering the work-function of the coated surface.

Patent Agency Ranking