中科微点-全球专利检索

  1. Login
  2. Sign Up

Search Results

55 records (took 0.03 seconds)

    Connected instrument procedure placekeeping system
    21.
    发明授权
    Connected instrument procedure placekeeping system 有权

    公开(公告)号：US10580308B2

    公开(公告)日：2020-03-03

    申请号：US15968050

    申请日：2018-05-01

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Aaron James Gannon ,  Ivan Sandy Wyatt

    IPC: G08G5/00 ,  G06F3/147 ,  G06T11/60 ,  B64D43/00 ,  G01C21/00 ,  G06F16/29 ,  G06F3/0482 ,  G06F3/0488

    Abstract: A connected instrument procedure placekeeping system includes a navigation database, a flight deck display, a flight deck processor, and an electronic device. The flight deck processor is in operable communication with the navigation database and the flight deck display and selectively retrieves flight plan data from the navigation database. The flight deck processor causes the flight deck display to render images of an instrument procedure. The electronic device is in operable communication with the flight deck processor and simultaneously renders an image of a published representation of the instrument procedure. One of either the flight deck processor or the electronic device is responsive to user input signals to highlight a waypoint and its associated constraint and the other of the electronic device or the flight deck processor simultaneously highlights the waypoint and its associated constraint for ease of comparison.

    Aircraft systems and methods for unusual attitude recovery
    23.
    发明授权
    Aircraft systems and methods for unusual attitude recovery 有权

    公开(公告)号：US10216471B1

    公开(公告)日：2019-02-26

    申请号：US15679405

    申请日：2017-08-17

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Gang He ,  Jason F. Harvey ,  Ivan Sandy Wyatt ,  Thea L. Feyereisen

    IPC: G01C5/00 ,  G06F3/147 ,  B64D43/00

    Abstract: A vehicle system and method are provided. The system includes a processor configured to compare received data representative of a current attitude with predetermined bank, nose up, and nose down values to determine that an occurrence of unusual attitude is currently underway. Upon determining that an occurrence of unusual attitude conditions is currently underway, the system and method generate display signals that command and control a display system to render roll angle alert symbology. The roll angle alert symbology includes a tracing arrowhead that more clearly shows the direction to recover from unusual attitude conditions. Based in part on the tracing nature of the arrowhead, provided technological improvements are observable on display systems that are monochrome, as well as those with color. In various embodiments, color attributes and confining the dynamic tracing performed by the arrowhead more clearly inform a pilot of the roll recovery direction to recover from unusual attitude conditions.

    AIRCRAFT SYSTEMS AND METHODS FOR UNUSUAL ATTITUDE RECOVERY
    24.
    发明申请
    AIRCRAFT SYSTEMS AND METHODS FOR UNUSUAL ATTITUDE RECOVERY 审中-公开

    公开(公告)号：US20190056901A1

    公开(公告)日：2019-02-21

    申请号：US15679405

    申请日：2017-08-17

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Gang He ,  Jason F. Harvey ,  Ivan Sandy Wyatt ,  Thea L. Feyereisen

    IPC: G06F3/147 ,  B64D43/00

    Abstract: A vehicle system and method are provided. The system includes a processor configured to compare received data representative of a current attitude with predetermined bank, nose up, and nose down values to determine that an occurrence of unusual attitude is currently underway. Upon determining that an occurrence of unusual attitude conditions is currently underway, the system and method generate display signals that command and control a display system to render roll angle alert symbology. The roll angle alert symbology includes a tracing arrowhead that more clearly shows the direction to recover from unusual attitude conditions. Based in part on the tracing nature of the arrowhead, provided technological improvements are observable on display systems that are monochrome, as well as those with color. In various embodiments, color attributes and confining the dynamic tracing performed by the arrowhead more clearly inform a pilot of the roll recovery direction to recover from unusual attitude conditions.

    Systems and method of automatically generated radio calls
    25.
    发明授权
    Systems and method of automatically generated radio calls 有权

    公开(公告)号：US10116378B1

    公开(公告)日：2018-10-30

    申请号：US15709916

    申请日：2017-09-20

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Katarina Alexis Morowsky ,  Aaron Gannon ,  Ivan Sandy Wyatt

    IPC: G08B21/00 ,  H04B7/185 ,  G08G5/02 ,  G08G5/00 ,  G08G5/04 ,  G05D1/00

    Abstract: A method in an aircraft computing system for facilitating communication between a flight crew and external communication facility (ECF) such as air traffic control (ATC) or airline operational control (AOC) is provided. The method comprises monitoring aircraft data by an aircraft computing system for a plurality of pre-defined, non-emergency conditions, detecting, by the aircraft computing system, a pre-defined, non-emergency condition requiring communication from the flight crew to the ECF, automatically generating and displaying a computer-generated message on an aircraft cockpit display responsive to detecting the condition requiring communication from the flight crew to the ECF, providing a selection option for transmitting the message to the ECF, and transmitting the message to the ECF in accordance with the option selected.

    COCKPIT DISPLAY SYSTEMS AND METHODS FOR GENERATING COCKPIT DISPLAYS INCLUDING ENHANCED FLIGHT VISIBILITY INDICATORS
    26.
    发明申请
    COCKPIT DISPLAY SYSTEMS AND METHODS FOR GENERATING COCKPIT DISPLAYS INCLUDING ENHANCED FLIGHT VISIBILITY INDICATORS 有权

    公开(公告)号：US20170214904A1

    公开(公告)日：2017-07-27

    申请号：US15007673

    申请日：2016-01-27

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Ivan Sandy Wyatt ,  David Allen Tunheim ,  Gang He

    IPC: H04N13/04 ,  G08G5/00 ,  B64D43/00

    CPC classification number: H04N13/302 ,  B64D43/00 ,  G01C23/005 ,  G06F1/163 ,  G06T15/005 ,  G08G5/0047

    Abstract: Cockpit display systems and methods are provided for generating cockpit displays including symbology useful in assessing whether enhanced flight visibility requirements are satisfied during approach and landing. In one embodiment, the cockpit display system includes an Enhanced Flight Vision System (EFVS) sensor configured to monitor a region forward of the aircraft for runway reference features, a cockpit display device on which an EFVS image is generated utilizing EFVS sensor data, and a controller coupled to the EFVS sensor and to the display device. The controller determines an enhanced flight visibility requirement for a runway approached by the aircraft, and then visually indicates on the EFVS image whether enhanced flight visibility requirement is currently satisfied by, for example. generating an enhanced flight visibility indicator (EFVI) graphic on the EFVS image visually identifying a ground location beyond which the appearance of a runway reference feature satisfies the enhanced flight visibility requirement.

    System and method for displaying a runway position indicator
    29.
    发明授权
    System and method for displaying a runway position indicator 有权
    用于显示跑道位置指示器的系统和方法

    公开(公告)号：US09129521B2

    公开(公告)日：2015-09-08

    申请号：US13904241

    申请日：2013-05-29

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Aaron Gannon ,  Ivan Sandy Wyatt ,  Troy Nichols ,  John G. Suddreth

    IPC: G01C21/00 ,  G08G5/00 ,  G08G5/02

    CPC classification number: G08G5/025 ,  G08G5/0021 ,  G08G5/0047

    Abstract: A dynamic runway indicator is displayed overlying a conformal runway for assisting a pilot in completing an approach to landing on a runway. The dynamic runway indicator includes a polygon, that by changing position with respect to the conformal runway, provides advanced instrumentation cues to the pilot for adjusting the aircraft flight path to a normal, or recommended, path to the runway for landing, thereby assisting the pilot to improve the accuracy and safety of the approach and landing.

    Abstract translation: 一个动态跑道指示器显示在一个保形跑道上，以协助飞行员完成在跑道上着陆的方法。 动态跑道指示器包括多边形，其通过相对于保形跑道改变位置，向飞行员提供高级仪表线索，用于调整飞行器飞行路径到达跑道的正常或推荐路径以降落，从而辅助飞行员 提高进场和落地的准确性和安全性。

    Systems and methods for reducing error detection latency in LPV approaches
    30.
    发明授权
    Systems and methods for reducing error detection latency in LPV approaches 有权
    用于降低LPV方法中的错误检测延迟的系统和方法

    公开(公告)号：US08928527B2

    公开(公告)日：2015-01-06

    申请号：US13847151

    申请日：2013-03-19

    Applicant: Honeywell International Inc.

    Inventor： Gang He ,  Ivan Sandy Wyatt

    IPC: G01C21/16 ,  G08G5/02 ,  G01C21/00

    CPC classification number: G08G5/02 ,  G01C21/005 ,  G01S19/15 ,  G01S19/23 ,  G01S19/47 ,  G08G5/025

    Abstract: Systems and methods for reducing error detection latency in LPV approaches are provided. In certain embodiments, a method for navigational guidance includes calibrating inertial measurements acquired from an inertial navigation system with satellite-based augmentation system position measurements acquired from a satellite-based augmentation system to create corrected inertial navigation system positions. The method also includes determining whether the satellite-based augmentation system experienced a fault when the inertial measurements were calibrated with the satellite-based augmentation system position measurements. Further, when the satellite-based augmentation system did not experience a fault, the method includes monitoring the satellite-based augmentation system navigation position measurements based on the corrected inertial navigation system positions.

    Abstract translation: 提供了用于减少LPV方法中的错误检测延迟的系统和方法。 在某些实施例中，用于导航指导的方法包括校准从惯性导航系统获得的惯性测量，其具有从基于卫星的增强系统获取的基于卫星的增强系统位置测量值，以创建校正的惯性导航系统位置。 该方法还包括当使用基于卫星的增强系统位置测量校准惯性测量时，确定基于卫星的增强系统是否经历故障。 此外，当基于卫星的增强系统没有遇到故障时，该方法包括基于校正的惯性导航系统位置监视基于卫星的增强系统导航位置测量。

Patent Agency Ranking