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1.发明申请SYSTEM AND METHOD FOR CORRECTING ACCENT INDUCED SPEECH TRANSMISSION PROBLEMS 有权用于校正感兴趣的语音传播问题的系统和方法公开(公告)号：US20140244246A1
公开(公告)日：2014-08-28
申请号：US13777138
申请日：2013-02-26
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Joseph Nutaro , Robert E. De Mers
IPC: G10L19/005 , G10L15/26
CPC classification number: G10L15/26 , G08G5/0013 , G10L13/00 , G10L15/32 , G10L2015/221
Abstract: A system and method is provided for detecting errors in a speech transmission system. A first audio stream is comprised of a plurality of words, upon which a plurality of independent voice-to-text conversions are performed. If it is determined that at least one of the plurality of independent voice-to-text conversions is error free, a text-to-voice conversion of the at least one error-free voice-to-text conversion is performed to create a second audio stream.
Abstract translation: 提供了一种用于检测语音传输系统中的错误的系统和方法。 第一音频流由多个单词组成，在多个单词上执行多个独立的语音到文本转换。 如果确定多个独立的语音到文本转换中的至少一个是无错误的，则执行至少一个无错误语音到文本转换的文本到语音转换以创建第二个 音频流。
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2.发明申请GROUND REMOTE CONTROL SYSTEM AND METHOD FOR AN AIRCRAFT WITH AN ELECTRIC TAXI SYSTEM 有权地面远程控制系统及使用电动系统的飞机的方法公开(公告)号：US20160124428A1
公开(公告)日：2016-05-05
申请号：US14532443
申请日：2014-11-04
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Joseph Nutaro , William D. Cromer , Daniel P. Johnson , Lee Davis , James Fusaro
CPC classification number: G05D1/0011 , B64C25/405 , B64C25/42 , B64C25/50 , B64D13/06 , B64D41/00 , B64D2013/0611 , G05D1/0038 , G05D1/0083
Abstract: A ground remote control system for an aircraft includes a security pairing device configured to establish a first secure communication link and protocol between a remote control device and a ground remote control system controller; and establish a second secure communication link and protocol, using the first communication link and protocol between the remote control device and the ground remote control system controller. The ground remote control system controller is configured to receive drive command signals, brake command signals, steering command signals, and power command signals, from the remote control device and generate the electronic drive commands, the electronic brake commands, the electronic steering commands, and the electronic power commands.
Abstract translation: 一种用于飞行器的地面遥控系统包括：一个安全配对装置，配置成在遥控装置和地面遥控系统控制器之间建立第一安全通信链路和协议; 并建立第二个安全通信链路和协议，使用远程控制设备和地面遥控系统控制器之间的第一通信链路和协议。 地面遥控系统控制器被配置为从遥控装置接收驱动命令信号，制动指令信号，转向指令信号和电力命令信号，并产生电子驱动命令，电子制动指令，电子转向指令和 电子命令。
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公开(公告)号：US09296490B2
公开(公告)日：2016-03-29
申请号：US14467275
申请日：2014-08-25
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Olukayode Olofinboba , Joseph Nutaro , David Pepitone , Patrick Jackson
CPC classification number: B64D45/00 , B64C25/405 , B64D43/02 , G01C23/00 , G08G5/0008 , G08G5/0013 , G08G5/0021 , G08G5/0078 , G08G5/045 , G08G5/065 , Y02T50/823
Abstract: A method of displaying aircraft operating and position information with an electronic display unit comprises determining a position of a first aircraft at an airport; determining an optimum speed range of the first aircraft; determining a first aircraft speed of the first aircraft; displaying on a screen of the display unit a map of at least part of the airport; displaying a first aircraft symbol on the map, the first aircraft symbol displayed in a position on the map indicative of position of the first aircraft; and displaying an optimum speed range symbol having a lower bound end and a higher bound end in a position on the map such that the first aircraft symbol is between the lower bound end and the higher bound end when the first aircraft speed is within the optimum speed range.
Abstract translation: 用电子显示单元显示飞行器操作和位置信息的方法包括：确定机场处的第一飞机的位置; 确定所述第一飞行器的最佳速度范围; 确定第一架飞机的第一架飞机速度; 在显示单元的屏幕上显示至少部分机场的地图; 在地图上显示第一飞机符号，第一飞行器符号显示在地图上指示第一飞机位置的位置上; 以及在所述地图上的位置中显示具有下限结束端和上限端的最佳速度范围符号，使得当所述第一飞行器速度在所述最佳速度内时，所述第一飞行器符号位于所述下限端和所述较高限制端之间 范围。
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公开(公告)号：US08935018B2
公开(公告)日：2015-01-13
申请号：US14083706
申请日：2013-11-19
Applicant: Honeywell International Inc.
Inventor： Keith Hughes , Joseph Nutaro , Christine Marie Haissig
CPC classification number: G05D1/0202 , G05D1/0083
Abstract: An auto-guidance and control method and system are provided for use in conjunction with an aircraft electric taxi system, wherein electric taxi guidance may be performed in a manual mode by a crew or in an auto-mode by an auto-guidance and control system. First, aircraft status data and airport feature data are accessed. A processor, in response to at least the aircraft status data and the airport feature data, generates taxi guidance information and renders the taxi guidance information on a display. A guidance route is manually navigated utilizing guidance information on the display in the manual mode. In the auto mode, taxi-path commands, generated by the processor, are applied to taxi path guidance controllers in the auto-mode.
Abstract translation: 提供了一种与飞机电动出租车系统一起使用的自动引导和控制方法和系统，其中电动出租车引导可以由船员以手动方式执行，或者通过自动引导和控制系统以自动模式执行 。 首先，访问飞机状态数据和机场特征数据。 响应于至少飞机状态数据和机场特征数据的处理器产生出租车指导信息，并将出租车引导信息呈现在显示器上。 使用手动模式下的显示器上的指导信息手动导航指导路线。 在自动模式下，由处理器生成的滑行路径命令以自动模式应用于出租车路径引导控制器。
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公开(公告)号：US09602509B2
公开(公告)日：2017-03-21
申请号：US14475258
申请日：2014-09-02
Applicant: Honeywell International Inc.
Inventor： Daniel P. Johnson , Joseph Nutaro
CPC classification number: H04L63/0876 , G06F9/445 , G06F21/64 , H04L9/3242 , H04L63/123 , H04L67/12 , H04L2209/84
Abstract: Embodiments described herein provide for a system for verifying integrity of files uplinked to a remote vehicle. The system is configured to receive a first message authentication code (MAC) for the uplinked file, a first acknowledgement MAC for the MAC, and a first cyclic redundancy check (CRC) for the first MAC and the acknowledgement MAC. The system is also configured to compute a second MAC from the uplinked file, a second acknowledgement MAC from the second MAC and a second CRC from the second MAC and second acknowledgement MAC. Integrity of the uplinked file is verified by comparing the first CRC with the second CRC. If integrity of the uplinked file is confirmed, the uplinked file is accepted. If integrity of the uplinked file is not confirmed, the uplinked file is rejected.
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Patent Agency Ranking
6.发明授权Ground remote control system and method for an aircraft with an electric taxi system 有权具有电动出租车系统的飞机的地面遥控系统和方法公开(公告)号：US09417629B2
公开(公告)日：2016-08-16
申请号：US14532443
申请日：2014-11-04
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Joseph Nutaro , William D. Cromer , Daniel P. Johnson , Lee Davis , James Fusaro
CPC classification number: G05D1/0011 , B64C25/405 , B64C25/42 , B64C25/50 , B64D13/06 , B64D41/00 , B64D2013/0611 , G05D1/0038 , G05D1/0083
Abstract: A ground remote control system for an aircraft includes a security pairing device configured to establish a first secure communication link and protocol between a remote control device and a ground remote control system controller; and establish a second secure communication link and protocol, using the first communication link and protocol between the remote control device and the ground remote control system controller. The ground remote control system controller is configured to receive drive command signals, brake command signals, steering command signals, and power command signals, from the remote control device and generate the electronic drive commands, the electronic brake commands, the electronic steering commands, and the electronic power commands.
Abstract translation: 一种用于飞行器的地面遥控系统包括：一个安全配对装置，配置成在遥控装置和地面遥控系统控制器之间建立第一安全通信链路和协议; 并建立第二个安全通信链路和协议，使用远程控制设备和地面遥控系统控制器之间的第一通信链路和协议。 地面遥控系统控制器被配置为从遥控装置接收驱动命令信号，制动指令信号，转向指令信号和电力命令信号，并产生电子驱动命令，电子制动指令，电子转向指令和 电子命令。
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7.发明申请AIRCRAFT ELECTRIC TAXI SYSTEM DIAGNOSTIC AND PROGNOSTIC EVALUATION SYSTEM AND METHOD 有权飞机电力系统诊断与预警评估系统及方法公开(公告)号：US20160086396A1
公开(公告)日：2016-03-24
申请号：US14490495
申请日：2014-09-18
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Joseph Nutaro , Stephen Abel , Grant Gordon
CPC classification number: G07C5/0808 , B64C25/405 , Y02T50/823
Abstract: An aircraft electric taxi system diagnostics and prognostics evaluation method, including receiving, with a computer, an electronically recorded first performance parameter of a first electric taxi system of a first aircraft during a taxi operational event at an airport; and comparing the first performance parameter with a first performance factor statistical model generated in response to the first performance parameter and first comparative performance parameters; and calculating a first performance parameter difference based on the comparison.
Abstract translation: 一种飞机电动出租车系统诊断和预测评估方法，包括在机场的出租车操作事件期间用计算机接收第一飞机的第一电动出租车系统的电子记录的第一性能参数; 以及将所述第一性能参数与响应于所述第一性能参数和所述第一性能参数产生的第一性能因子统计模型进行比较; 以及基于所述比较来计算第一性能参数差异。
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公开(公告)号：US20160052641A1
公开(公告)日：2016-02-25
申请号：US14467275
申请日：2014-08-25
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Olukayode Olofinboba , Joseph Nutaro , David Pepitone , Patrick Jackson
IPC: B64D45/00
CPC classification number: B64D45/00 , B64C25/405 , B64D43/02 , G01C23/00 , G08G5/0008 , G08G5/0013 , G08G5/0021 , G08G5/0078 , G08G5/045 , G08G5/065 , Y02T50/823
Abstract: A method of displaying aircraft operating and position information with an electronic display unit comprises determining a position of a first aircraft at an airport; determining an optimum speed range of the first aircraft; determining a first aircraft speed of the first aircraft; displaying on a screen of the display unit a map of at least part of the airport; displaying a first aircraft symbol on the map, the first aircraft symbol displayed in a position on the map indicative of position of the first aircraft; and displaying an optimum speed range symbol having a lower bound end and a higher bound end in a position on the map such that the first aircraft symbol is between the lower bound end and the higher bound end when the first aircraft speed is within the optimum speed range.
Abstract translation: 用电子显示单元显示飞行器操作和位置信息的方法包括：确定机场处的第一飞机的位置; 确定所述第一飞行器的最佳速度范围; 确定第一架飞机的第一架飞机速度; 在显示单元的屏幕上显示至少部分机场的地图; 在地图上显示第一飞机符号，第一飞行器符号显示在地图上指示第一飞机位置的位置上; 以及在所述地图上的位置中显示具有下限结束端和上限端的最佳速度范围符号，使得当所述第一飞行器速度在所述最佳速度内时，所述第一飞行器符号位于所述下限端和所述较高限制端之间 范围。
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公开(公告)号：US20160012736A1
公开(公告)日：2016-01-14
申请号：US14325565
申请日：2014-07-08
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Joseph Nutaro , Patrick Jackson , Jay Sims
CPC classification number: G08G5/065 , B64C25/34 , B64C25/405 , B64C25/42 , G05D1/0083 , G05D13/62 , G08G5/0021
Abstract: An aircraft taxi control system may include a motor connected to drive a landing gear wheel of the aircraft. A motor controller may be connected to control speed of the motor. The system may also include an aircraft taxi route database, an aircraft position determination unit; an aircraft performance database and a processor configured to a) integrate signals from the aircraft taxi route database, the aircraft position determination unit and aircraft performance database, and b) produce a motor deceleration signal to the motor controller when the aircraft arrives at a predetermined distance from a predetermined location so that the aircraft arrives at the location traveling at a desired speed
Abstract translation: 飞机出租车控制系统可以包括连接以驱动飞行器的起落架的马达。 可以连接电机控制器来控制电机的速度。 该系统还可以包括飞机出租车路线数据库，飞机位置确定单元; 飞机性能数据库和处理器，其被配置为a）整合来自飞机出租车路线数据库，飞行器位置确定单元和飞行器性能数据库的信号，以及b）当飞机到达预定距离时，向马达控制器产生马达减速信号 从预定位置起飞机到达以期望速度行驶的位置
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公开(公告)号：US20150375854A1
公开(公告)日：2015-12-31
申请号：US14317112
申请日：2014-06-27
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Stephen Abel , David Lazarovich , Joseph Nutaro
CPC classification number: B64C25/405 , Y02T50/823
Abstract: An aircraft taxi control system may include a left main gear (MG) drive motor, a right MG motor, a first motor drive controller configured to produce a left motor torque signal responsively to nose gear angle (NGA) and nose wheel speed (NGS), and a second motor drive controller configured to produce a right motor toque signal responsively to the NGA and the NGS. The left motor torque signal and the right motor torque signal may be coordinated to reduce lateral loading of the nose wheel during a turning maneuver.
Abstract translation: 飞机出租车控制系统可以包括左主齿轮（MG）驱动马达，右MG马达，第一马达驱动控制器，其构造成响应于前档角（NGA）和前轮速度（NGS）产生左电机转矩信号， 以及第二电动机驱动控制器，被配置为响应于NGA和NGS产生正确的电动机转矩信号。 可以协调左电动机转矩信号和右电动机转矩信号以减少转向操纵期间前轮的横向负载。
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