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：WO2012071456A3

公开(公告)日：2013-07-25

申请号：PCT/US2011061928

申请日：2011-11-22

Applicant: BOREALIS TECH LTD ,  GILLERAN NEAL ,  SWEET ROBERT M ,  EDELSON JONATHAN ,  COX ISAIAH WATAS

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

IPC: B64C25/50

CPC classification number: B64C25/405 ,  Y02T50/823

Abstract: A failsafe system and method for ensuring the safe operation of an aircraft with a ground movement system to drive the aircraft independently on the ground is provided. The system includes at least one aircraft nose or main drive wheel powered by an onboard wheel driver responsive to sensed aircraft and ground movement system operating parameters to continue operation in response to parameters within normal limits or to prevent continued operation if sensed parameters are outside normal limits and indicate continued operation to be unsafe. The onboard wheel driver includes a locking assembly responsive automatically or manually to signals indicating sensed parameters to lock the onboard wheel driver in an activated or an inactivated condition, depending on whether operation of the ground movement system can be continued safely.

Abstract translation: 提供一种用于确保具有地面运动系统的飞机的安全操作以在地面独立地驱动飞机的故障安全系统和方法。 该系统包括至少一个飞行器鼻部或主驱动轮，其由响应于感测到的飞行器和地面移动系统操作参数的车载驱动器驱动，以响应于正常限度内的参数继续操作，或者如果感测参数在正常限度之外，则防止继续操作 并指示持续运作不安全。 车载轮驱动器包括一个自动或手动响应的信号，该锁定组件响应于指示感测参数的信号，以根据地面移动系统的操作是否可以安全地继续操作将车载车轮驱动器锁定在激活状态或非激活状态。

公开(公告)号：GB2499756A

公开(公告)日：2013-08-28

申请号：GB201310160

申请日：2011-11-22

Applicant: BOREALIS TECH LTD ,  EDELSON JONATHAN SIDNEY

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

IPC: B64C25/40 ,  B64C19/02 ,  B64C25/36 ,  B64C25/50 ,  B64F1/22 ,  G08G5/06

Abstract: A failsafe system and method for ensuring the safe operation of an aircraft with a ground movement system to drive the aircraft independently on the ground is provided. The system includes at least one aircraft nose or main drive wheel powered by an onboard wheel driver responsive to sensed aircraft and ground movement system operating parameters to continue operation in response to parameters within normal limits or to prevent continued operation if sensed parameters are outside normal limits and indicate continued operation to be unsafe. The onboard wheel driver includes a locking assembly responsive automatically or manually to signals indicating sensed parameters to lock the onboard wheel driver in an activated or an inactivated condition, depending on whether operation of the ground movement system can be continued safely.

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.

公开(公告)号：AU2011332896B2

公开(公告)日：2015-06-11

申请号：AU2011332896

申请日：2011-11-22

Applicant: BOREALIS TECH LTD ,  EDELSON JONATHAN

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

IPC: B64C25/50

Abstract: A failsafe system and method for ensuring the safe operation of an aircraft with a ground movement system to drive the aircraft independently on the ground is provided. The system includes at least one aircraft nose or main drive wheel powered by an onboard wheel driver responsive to sensed aircraft and ground movement system operating parameters to continue operation in response to parameters within normal limits or to prevent continued operation if sensed parameters are outside normal limits and indicate continued operation to be unsafe. The onboard wheel driver includes a locking assembly responsive automatically or manually to signals indicating sensed parameters to lock the onboard wheel driver in an activated or an inactivated condition, depending on whether operation of the ground movement system can be continued safely.

公开(公告)号：AU2011332896A1

公开(公告)日：2013-07-04

申请号：AU2011332896

申请日：2011-11-22

Applicant: BOREALIS TECH LTD ,  EDELSON JONATHAN

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

IPC: B64C19/02

Abstract: A failsafe system and method for ensuring the safe operation of an aircraft with a ground movement system to drive the aircraft independently on the ground is provided. The system includes at least one aircraft nose or main drive wheel powered by an onboard wheel driver responsive to sensed aircraft and ground movement system operating parameters to continue operation in response to parameters within normal limits or to prevent continued operation if sensed parameters are outside normal limits and indicate continued operation to be unsafe. The onboard wheel driver includes a locking assembly responsive automatically or manually to signals indicating sensed parameters to lock the onboard wheel driver in an activated or an inactivated condition, depending on whether operation of the ground movement system can be continued safely.