公开(公告)号：WO2013186635A3

公开(公告)日：2014-05-08

申请号：PCT/IB2013001905

申请日：2013-05-01

Applicant: BOREALIS TECH LTD

Inventor： PERKINS SCOTT

IPC: B60B19/06 ,  B60B37/10 ,  B64C25/40

CPC classification number: B60B27/001 ,  B60B19/06 ,  B60B25/04 ,  B60B27/0047 ,  B60B27/0078 ,  B60B37/10 ,  B60B2380/14 ,  B60B2380/64 ,  B60B2900/311 ,  B60B2900/351 ,  B60Y2200/51 ,  B64C25/36 ,  B64C25/405 ,  Y02T50/823

Abstract: A bearing arrangement for an aircraft landing gear wheel is provided that effectively supports the wheel on an axle while maximizing internal wheel volume available for mounting non- engine drive means used to power the wheel and/or brakes or other structures within the maximized wheel volume. The bearing arrangement is preferably employed with a two-part aircraft wheel mounted on a landing gear axle and includes bearing structures located only on wheel sections adjacent to the axle. A specifically configured cantilevered joint portion of inboard and outboard wheel sections supports weight and loads bearing structures, eliminating the need for and space required by a high speed bearing. Stiffness necessary for strength and structural integrity is provided by the materials selected to form the wheel sections.

Abstract translation: 提供了一种用于飞机起落架的轴承装置，其有效地支撑在车轴上的车轮，同时最大化可用于安装非发动机驱动装置的内轮体积，用于为最大轮体积内的车轮和/或制动器或其他结构提供动力。 轴承布置优选地与安装在起落架轴上的两部分飞机轮一起使用，并且包括仅位于与轴相邻的轮部分上的轴承结构。 专门设计的内侧和外侧车轮部分的悬臂接头部分支撑重量和承载结构，消除了高速轴承所需的空间和空间。 强度和结构完整性所需的刚度由选择用于形成车轮部分的材料提供。

公开(公告)号：WO2012174306A3

公开(公告)日：2014-05-01

申请号：PCT/US2012042547

申请日：2012-06-14

Applicant: BOREALIS TECH LTD ,  GILLERAN NEAL ,  SWEET ROBERT M ,  PERKINS SCOTT

Inventor： GILLERAN NEAL ,  SWEET ROBERT M ,  PERKINS SCOTT

IPC: B64C25/36

CPC classification number: B64C25/405 ,  B60B25/002 ,  B60B25/04 ,  Y02T10/82 ,  Y02T50/823

Abstract: A split circumference wheel assembly is provided for an aircraft landing gear wheel configured to maximize the space available within a landing gear wheel well to support a motor driver assembly with drive means that drives the aircraft wheel on the ground. The split circumference wheel assembly includes separable inboard and outboard support walls that are spaced axially apart a maximized distance so that the motor driver assembly is completely contained within the maximized space defined. A preferred wheel assembly employs a demountable flange and a locking ring to integrally and removably support the motor driver assembly within the maximized wheel volume to drive one or more aircraft wheels and move the aircraft independently on the ground. The wheel and motor driver assembly described herein are designed to be retrofitted in an existing aircraft wheel.

Abstract translation: 为飞机着陆齿轮提供分体式圆周轮组件，其被配置为使起落架轮井内的空间最大化，以支撑具有驱动装置的马达驱动器组件，所述驱动装置驱动地面上的飞行器轮。 分体式圆周轮组件包括可分离的内侧和外侧支撑壁，其间隔开最大距离的轴向间隔，使得电动机驱动器组件完全包含在限定的最大空间内。 优选的车轮组件采用可拆卸的凸缘和锁定环，以将电动机驱动器组件整体地和可拆卸地支撑在最大化的车轮体积内以驱动一个或多个飞行器轮子并且独立地在地面上移动飞行器。 这里描述的车轮和马达驱动器组件被设计成在现有飞行器轮中进行改装。

公开(公告)号：GB2516598A

公开(公告)日：2015-01-28

申请号：GB201421331

申请日：2013-05-01

Applicant: BOREALIS TECH LTD

Inventor： PERKINS SCOTT

IPC: B60B19/06 ,  B60B37/10 ,  B64C25/40

Abstract: A bearing arrangement for an aircraft landing gear wheel is provided that effectively supports the wheel on an axle while maximizing internal wheel volume available for mounting non- engine drive means used to power the wheel and/or brakes or other structures within the maximized wheel volume. The bearing arrangement is preferably employed with a two-part aircraft wheel mounted on a landing gear axle and includes bearing structures located only on wheel sections adjacent to the axle. A specifically configured cantilevered joint portion of inboard and outboard wheel sections supports weight and loads bearing structures, eliminating the need for and space required by a high speed bearing. Stiffness necessary for strength and structural integrity is provided by the materials selected to form the wheel sections.

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.

公开(公告)号：GB2515704A

公开(公告)日：2014-12-31

申请号：GB201419139

申请日：2013-03-28

Applicant: BOREALIS TECH LTD

Inventor： EDELSON JONATHAN SIDNEY ,  PERKINS SCOTT ,  SWEET ROBERT M ,  COX ISAIAH W

IPC: G01M17/00 ,  G01L3/00

Abstract: A wheel testing system and method are provided that simulates realistically conditions likely to be encountered during operation of vehicle wheels, especially powered drive wheels and wheel-connected structures. The system may include an integral support frame designed to adjustably mount wheels or wheel-connected structures to be tested, a load motor drivingly connected to an inertial load, and an adjustable mounting sled configured to adjustably mount a test wheel or a wheel-connected structure with an hydraulic system actuatable to adjust the location of the test wheel relative to the inertial load to vary or fix the load on the test wheel desired. Speed of the test wheel can be varied or fixed by controlling the speed of the load motor. System measurement and data collection electronics measure a range of selected wheel parameters and gather data for transmission to a processor or non-transitory storage medium for processing and evaluation.

公开(公告)号：AU2011323421A1

公开(公告)日：2013-06-20

申请号：AU2011323421

申请日：2011-11-02

Applicant: BOREALIS TECH LTD

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

IPC: B64C25/50

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.