中科微点-全球专利检索

  1. Login
  2. Sign Up

Search Results

39 records (took 0.019 seconds)

    System and methods enabling aircraft energy dissipation for rapid decision making
    1.
    发明授权
    System and methods enabling aircraft energy dissipation for rapid decision making 有权

    公开(公告)号：US11790795B2

    公开(公告)日：2023-10-17

    申请号：US16890614

    申请日：2020-06-02

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Rajesh Chaubey ,  Rajeev Mohan ,  Daniel E. Lewis

    IPC: B64D43/02 ,  G08G5/02 ,  G06F3/0482

    CPC classification number: G08G5/025 ,  B64D43/02 ,  G06F3/0482

    Abstract: A method in an aircraft for energy reduction is disclosed. The method includes: determining a starting point location, altitude and airspeed for a stable approach for landing at a diversion airport; and determining a vertical strategy for achieving the starting point altitude and airspeed by identifying a region of opportunity for adjusting the speed and altitude and identifying a plurality of energy reduction strategies for achieving the starting point altitude and airspeed while in the region of opportunity based on a speed mode during the stable approach. The method further comprises causing a graphic display to be displayed that lists for selection each of the plurality of identified strategies, detailed maneuver information for strategy implementation, and costs for implementing each identified strategy; and causing to be displayed, responsive to flight crew selection, a lateral view and vertical view of a proposed trajectory based on a selected identified strategy.

    Radar vectoring energy management guidance methods and systems
    2.
    发明授权
    Radar vectoring energy management guidance methods and systems 有权

    公开(公告)号：US11525699B2

    公开(公告)日：2022-12-13

    申请号：US16866257

    申请日：2020-05-04

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Rajesh Chaubey ,  Akshay Sankeshwari ,  Sharanabasappa Advani ,  Bhalakrishnan Janardhanan ,  Roopa Niveditha Sundara Kulal ,  Ravish Udupa ,  Daniel E. Lewis

    IPC: G01C23/00 ,  B64D43/02 ,  G01S13/91

    Abstract: Methods and systems are provided for guiding or otherwise assisting energy management of an aircraft radar vectoring en route to a runway. A method involves determining a predicted lateral trajectory for the radar vectoring in accordance with interception criteria, wherein the lateral trajectory comprises a sequence of segments for satisfying the interception criteria from a current location of the aircraft and each navigational segment of the sequence is associated with an anticipated aircraft heading assignment. The method determines a reference vertical trajectory corresponding to the lateral trajectory, determines a target value for an energy state parameter of the aircraft at the current location on the lateral trajectory using the reference vertical trajectory, and provides indication of a recommended action to reduce a difference between a current value for the energy state parameter and the target value.

    METHOD AND SYSTEM FOR ENGAGING A VERTICAL NAVIGATION DESCENT MODE FOR AN AIRCRAFT
    3.
    发明申请
    METHOD AND SYSTEM FOR ENGAGING A VERTICAL NAVIGATION DESCENT MODE FOR AN AIRCRAFT 审中-公开

    公开(公告)号：US20200160731A1

    公开(公告)日：2020-05-21

    申请号：US16193522

    申请日：2018-11-16

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Dorothee De Villele ,  Rajesh Chaubey ,  John Hillier ,  Daniel E. Lewis

    IPC: G08G5/00

    Abstract: Methods and systems are provided for engaging a vertical navigational descent (VNAV/DES) mode of a flight management system (FMS) for an aircraft. The method comprises retrieving a preset vertical navigation (VNAV) profile for a descent path of the aircraft that is stored in the FMS. The current flight path angle (FPA) and vertical speed (VS) of the aircraft is determined and intercept parameters are calculated to intercept the preset VNAV profile with the VNAV/DES mode of the FMS. The intercept parameters are calculated based on the current FPA and VS and displayed to an aircrew member of the aircraft on a visual display device. The aircrew member is allowed to accept the intercept parameters with the VNAV/DES mode of the FMS.

    Variable energy management methods and systems
    6.
    发明授权
    Variable energy management methods and systems 有权

    公开(公告)号：US11645924B2

    公开(公告)日：2023-05-09

    申请号：US17127504

    申请日：2020-12-18

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Rajesh Chaubey ,  Daniel E. Lewis

    IPC: G08G5/00

    CPC classification number: G08G5/0039 ,  G08G5/0017 ,  G08G5/0047

    Abstract: Methods and systems are provided for assisting operation of a vehicle deviating from a desired manner of operation, such as an aircraft deviating from a planned trajectory. One method involves identifying a current aircraft altitude, identifying a current aircraft configuration, determining a recommended flight path from the current aircraft altitude for satisfying an upcoming constraint associated with a reference descent strategy based at least in part on the current aircraft configuration in response to a deviation between the current aircraft altitude a target altitude according to the reference descent strategy, and providing an output influenced by the recommended flight path. The recommended flight path includes a recommended vertical profile and a recommended speed profile, and the recommended flight path is configured to vary at least one of a kinetic energy or a potential energy of the aircraft along the recommended flight path en route to the upcoming constraint.

    SYSTEMS AND METHODS FOR ALERTING DESCENT BELOW ALTITUDE
    7.
    发明申请
    SYSTEMS AND METHODS FOR ALERTING DESCENT BELOW ALTITUDE 有权

    公开(公告)号：US20230089086A1

    公开(公告)日：2023-03-23

    申请号：US17647179

    申请日：2022-01-06

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Rajesh Chaubey ,  Ratan Khatwa

    IPC: G08G5/04 ,  G08G5/02 ,  G08G5/00

    Abstract: Methods and system for alerting descent with respect to at least one of minimum sector altitude, minimum safe altitude and terrain clearance floor in an aircraft. The methods and systems receive at least one of a minimum sector altitude value, a minimum safe altitude value and a terrain clearance floor value based on a flight plan of the aircraft or a location of the aircraft. A movement trajectory of the aircraft is predicted. The aircraft predicted movement trajectory is evaluated with respect to the at least one of the minimum sector altitude value, the minimum safe altitude value and the terrain clearance floor value. An alert is output when the evaluation predicts convergence of the aircraft predicted movement trajectory and the at least one of the minimum sector altitude value, the minimum safe altitude value and the terrain clearance floor value.

    Systems and methods for alerting descent below altitude
    10.
    发明授权
    Systems and methods for alerting descent below altitude 有权

    公开(公告)号：US11830373B2

    公开(公告)日：2023-11-28

    申请号：US17647179

    申请日：2022-01-06

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Rajesh Chaubey ,  Ratan Khatwa

    IPC: G08G5/04 ,  G08G5/00 ,  G08G5/02

    CPC classification number: G08G5/045 ,  G08G5/003 ,  G08G5/0021 ,  G08G5/0086 ,  G08G5/025

    Abstract: Methods and system for alerting descent with respect to at least one of minimum sector altitude, minimum safe altitude and terrain clearance floor in an aircraft. The methods and systems receive at least one of a minimum sector altitude value, a minimum safe altitude value and a terrain clearance floor value based on a flight plan of the aircraft or a location of the aircraft. A movement trajectory of the aircraft is predicted. The aircraft predicted movement trajectory is evaluated with respect to the at least one of the minimum sector altitude value, the minimum safe altitude value and the terrain clearance floor value. An alert is output when the evaluation predicts convergence of the aircraft predicted movement trajectory and the at least one of the minimum sector altitude value, the minimum safe altitude value and the terrain clearance floor value.

Patent Agency Ranking