公开(公告)号：US20150325047A1

公开(公告)日：2015-11-12

申请号：US14270903

申请日：2014-05-06

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Kevin J. Conner ,  Santosh Mathan

IPC: G06T19/00 ,  G01C21/36 ,  G06F3/0484

CPC classification number: G06T19/006 ,  G01C21/36 ,  G01C21/3623 ,  G05B2219/23148 ,  G05B2219/32226 ,  G06F3/04842 ,  G06F3/04847 ,  G06F16/9537 ,  G06F16/9554 ,  G06T11/60 ,  G06T2215/16 ,  Y02P90/14

Abstract: A method for providing maintenance instructions to a user is provided. The method obtains a set of data, comprising maintenance instructions, macrolocation data, and object recognition characteristics associated with a target apparatus; guides the user to a macrolocation and a microlocation of the target apparatus, based on the obtained set of data; and provides the maintenance instructions associated with the target apparatus, when the user has reached the macrolocation and the microlocation.

Abstract translation: 提供了一种向用户提供维护指令的方法。 该方法获得一组数据，包括与目标设备相关联的维护指令，宏位置数据和对象识别特征; 基于获得的数据集，引导用户进行目标设备的宏位置和微位置; 并且当用户已经到达宏位置和微位置时，提供与目标设备相关联的维护指令。

公开(公告)号：US20170110018A1

公开(公告)日：2017-04-20

申请号：US14886982

申请日：2015-10-19

Applicant: Honeywell International Inc.

Inventor： Guoqing Wang ,  Rong Zhang ,  Kevin J. Conner ,  Ruy C. Brandao ,  Zhong Chen

IPC: G08G5/00

CPC classification number: G08G5/0078 ,  G08G5/0008 ,  G08G5/0021 ,  G08G5/0065

Abstract: This disclosure is directed to systems and methods for generating outputs based on collected aircraft maneuver data. In one example, a system is configured to collect surveillance data from one or more aircraft. The system is further configured to identify, from the collected surveillance data, aircraft maneuver data indicative of maneuvers of the one or more aircraft. The system is further configured to store the aircraft maneuver data in a data store. The system is further configured to perform one or more analyses of the stored aircraft maneuver data in the data store. The system is further configured to generate an output based on the one or more analyses of the stored aircraft maneuver data.

公开(公告)号：US20140368359A1

公开(公告)日：2014-12-18

申请号：US13919431

申请日：2013-06-17

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Steve Johnson ,  Yasuo Ishihara ,  Kevin J. Conner

IPC: G01P1/10 ,  G01P5/00

CPC classification number: G01P1/10 ,  G01C23/00 ,  G01P5/00

Abstract: Embodiments of a flight deck display system deployed onboard an aircraft are provided, as are embodiments of a method carried-out by a flight deck display system. In one embodiment, the flight deck display system includes a cockpit display device and a controller. The controller is configured to: (i) establish the speed trend of the aircraft over a predetermined time period; (ii) generate a primary flight display on the cockpit display device including a speed trend vector graphic representative of the established speed trend; and (iii) alter the appearance of the speed trend vector graphic in a first predetermined manner if a low speed change condition is detected during at least one of aircraft takeoff and landing.

Abstract translation: 提供了部署在飞行器上的飞行甲板显示系统的实施例，由飞行甲板显示系统执行的方法的实施例也是如此。 在一个实施例中，驾驶舱显示系统包括驾驶舱显示装置和控制器。 控制器被配置为：（i）在预定时间段内建立飞机的速度趋势; （ii）在驾驶舱显示装置上产生代表所建立的速度趋势的速度趋势矢量图形的主飞行显示; 以及（iii）如果在飞机起飞和着陆期间的至少一个中检测到低速变化条件，则以第一预定方式改变速度趋势矢量图形的外观。

公开(公告)号：US20190228668A1

公开(公告)日：2019-07-25

申请号：US15878521

申请日：2018-01-24

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Rui Wang ,  Sean J. Caufield ,  Gang He ,  Kevin J. Conner ,  Sabrina Yan ,  Thea L. Feyereisen ,  Yong Zhang ,  Fangzhou Shi

IPC: G08G5/06 ,  B64D43/00

Abstract: Methods and systems are provided for automatically predicting a surface movement path of an aircraft. The method comprises collecting historical aircraft trajectory data from an empirical aircraft path database. Next, aircraft trajectory paths for a designated airport are mapped based on the historical aircraft trajectory data and map data for the designated airport. Different aircraft trajectory paths are each assigned a weight for the designated airport. A graphical display is then generated for each of the aircraft trajectory paths for the designated airport along with a table that identifies a most probable terminal area and entry node for use by the aircraft at the designated airport.

公开(公告)号：US20170103662A1

公开(公告)日：2017-04-13

申请号：US14878598

申请日：2015-10-08

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Yuriy Kurgan ,  Kevin J. Conner

IPC: G08G5/04

CPC classification number: G08G5/025 ,  G08G5/0013 ,  G08G5/0026 ,  G08G5/065

Abstract: A stationary object identification system includes memory and a transmitter. The memory has obstacle data stored therein that includes a plurality of parameters associated with each of a plurality of stationary obstacles located at a location, such as an aerodrome. The transmitter is in operable communication with the memory and is configured to generate a plurality of signals. Each of the signals is associated with a different one of the stationary obstacles and has a power level representative of the plurality of parameters associated with the stationary obstacle.

公开(公告)号：US20160221686A1

公开(公告)日：2016-08-04

申请号：US14611544

申请日：2015-02-02

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Yasuo Ishihara ,  Kevin J. Conner ,  Steve Johnson

IPC: B64D45/08 ,  G07C5/02 ,  B64D45/04

CPC classification number: B64D45/08 ,  B64D45/04 ,  G07C5/02 ,  G08G5/0021 ,  G08G5/0065 ,  G08G5/025

Abstract: A system and method for alerting a helicopter pilot to an undesirable operating condition during landing operations are provided. Avionics data are supplied from an avionics data source. A controller coupled to receive at least a portion of the avionics data from the avionics data source is configured, upon receipt of the avionics data, to determine when the undesirable operating condition exists and, upon determining that the undesirable operating condition exists, to generate an alert signal that provides notification to the helicopter pilot to increase helicopter airspeed.

Abstract translation: 提供了一种用于在着陆操作期间将直升机飞行员警报到不期望的操作状态的系统和方法。 航空电子数据来自航空电子数据源。 被配置为从航空电子数据源接收航空电子数据的至少一部分的控制器被配置为在接收到航空电子数据时确定何时存在不期望的操作条件，并且在确定存在不需要的操作条件时，生成 警报信号，通知直升机飞行员增加直升机空速。

公开(公告)号：US20150146008A1

公开(公告)日：2015-05-28

申请号：US14090106

申请日：2013-11-26

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Kevin J. Conner ,  Santosh Mathan

IPC: G06K9/00

CPC classification number: G06K9/00671 ,  G05B2219/32014 ,  G06F3/0304 ,  G06K9/3216 ,  G06Q10/20 ,  G09B9/006

Abstract: A maintenance assistance system and method of operating are provided. The maintenance assistance system may include, but is not limited to, a camera, a speaker, a technician marker, a memory configured to store a location of a plurality of tags and a location of at least one component relative to at least one of the plurality of tags, and a processor communicatively coupled to the camera, the speaker and the memory, the processor configured to receive an indication of one of the components, determine a location of the technician marker relative to the location of the indicated component based upon data from the camera and the location of the indicated component relative to the at least one of the plurality of tags, and output position information to the speaker based upon the determined location of the technician marker relative to the location of the indicated component.

Abstract translation: 提供维护辅助系统和操作方法。 维护辅助系统可以包括但不限于相机，扬声器，技术人员标记，被配置为存储多个标签的位置的存储器以及相对于至少一个标签的至少一个部件的位置 多个标签和通信地耦合到相机，扬声器和存储器的处理器，处理器被配置为接收组件之一的指示，基于数据确定技术人员标记相对于所指示部件的位置的位置 根据相对于指示的组件相对于所指示的组件的位置确定的位置，从照相机和所指示的组件相对于多个标签中的至少一个标签的位置输出位置信息到扬声器。

公开(公告)号：US09685092B2

公开(公告)日：2017-06-20

申请号：US14878598

申请日：2015-10-08

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Yuriy Kurgan ,  Kevin J. Conner

IPC: G08G5/00 ,  G08G5/02 ,  G08G5/06

CPC classification number: G08G5/025 ,  G08G5/0013 ,  G08G5/0026 ,  G08G5/065

Abstract: A stationary object identification system includes memory and a transmitter. The memory has obstacle data stored therein that includes a plurality of parameters associated with each of a plurality of stationary obstacles located at a location, such as an aerodrome. The transmitter is in operable communication with the memory and is configured to generate a plurality of signals. Each of the signals is associated with a different one of the stationary obstacles and has a power level representative of the plurality of parameters associated with the stationary obstacle.

公开(公告)号：US20170083231A1

公开(公告)日：2017-03-23

申请号：US14862798

申请日：2015-09-23

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Rui Wang ,  Fenfei Guo ,  Gang He ,  Thea L. Feyereisen ,  Yong Zhang ,  Kevin J. Conner

IPC: G06F3/0488 ,  G06F17/30

CPC classification number: G06F3/04886 ,  G01C21/20 ,  G01C21/3611 ,  G06F3/0219 ,  G06F3/0237 ,  G06F3/03547 ,  G06F16/252 ,  G08G5/0021 ,  G08G5/065

Abstract: A database driven input system and a method for operating the same are provided. The database driven input system, for example, may include, but is not limited to, a memory configured to store a database comprising airport information, a touchscreen display, and a processor communicatively coupled to the touchscreen display and the database system, the processor configured to generate a database driven taxiway input interface comprising a database driven keyboard input interface, the database driven keyboard input interface comprising a smart keyboard configured to prevent invalid input based upon the airport information in the database, display the database driven taxiway input interface on the touchscreen display, receive an input from the touchscreen display, and dynamically update the database driven keyboard input interface based upon the input to the touchscreen display.

公开(公告)号：US20150321748A1

公开(公告)日：2015-11-12

申请号：US14272738

申请日：2014-05-08

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Steve Johnson ,  Yasuo Ishihara ,  Kevin J. Conner

IPC: B64C9/32 ,  B64D45/00

CPC classification number: B64C9/323 ,  B64D45/00 ,  B64D45/0005 ,  Y02T50/32

Abstract: A system and method is provided for controlling the speed of an aircraft with a speed brake during landing. The system includes a speed brake control system and a speed brake controller coupled to the speed brake control system for arming the speed brake. An alert generator is coupled to the speed brake controller for generating an alert when the speed brake is not armed.

Abstract translation: 提供了一种用于在着陆期间用速度制动器控制飞行器的速度的系统和方法。 该系统包括速度制动控制系统和与制动控制系统相连的速度制动控制器，用于制动速度制动器。 警报发生器耦合到速度制动控制器，用于当速度制动器未布防时产生警报。