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1. 发明授权

US09846432B2 Aircraft wing structure and control system 有权
公开(公告)号：US09846432B2
公开(公告)日：2017-12-19
申请号：US14907067
申请日：2014-07-25
申请人： LAM AVIATION, INC.
发明人： Michael Lam , Greg Cole
IPC分类号： G05D1/00 , G05D1/08 , G06F7/00 , G06F17/00 , B64C9/04 , B64C13/38 , B64C9/20 , B64C9/00
CPC分类号： G05D1/0083 , B64C9/04 , B64C9/20 , B64C13/38 , B64C2009/005 , G05D1/0816 , Y02T50/32
摘要： An aircraft includes a wing. The wing includes an aileron pivotally connected to a trailing edge of the wing, and a Lam aileron pivotally connected to the trailing edge of the wing. The aircraft includes a motor connected to the Lam aileron and configured to rotate the Lam aileron. The aircraft includes a controller configured to detect a deflection of the aileron from a neutral position, calculate a target deflection for the Lam aileron using the deflection of the aileron, and cause the motor to rotate the Lam aileron to the target deflection.

2. 发明授权

US09830829B1 Management system and methods for implementing aircraft intentions harmonization 有权
公开(公告)号：US09830829B1
公开(公告)日：2017-11-28
申请号：US14827377
申请日：2015-08-17
申请人： ROCKWELL COLLINS, INC.
发明人： William George Doyen , Geoffrey A. Shapiro
IPC分类号： G08G5/00 , G01C23/00 , B64D45/08 , G08G5/02 , G05D1/06 , B64D45/04 , G06F19/00 , G01C5/00 , G08G5/06 , G05D1/00 , G05D1/10
CPC分类号： G08G5/0082 , B64D45/04 , B64D45/08 , G01C5/00 , G01C23/00 , G05D1/0083 , G05D1/06 , G05D1/0676 , G05D1/101 , G06F19/00 , G07C5/008 , G08G5/0013 , G08G5/0026 , G08G5/0043 , G08G5/0056 , G08G5/025 , G08G5/065
摘要： A system and method are provided for integrating voice communication systems with voice recognition devices or units and myriad other data sources to provide a harmonization between intended aircraft operations and actual aircraft operations, including logical components to provide a mechanism to flag certain alert communications that signal the initiation of particular response scenarios based on detected terms and track initiation of pre-planned processes to address specific events that are signaled through the use of the detected terms. Information from myriad data sources is collected and integrated to provide an indication of intended operations for an aircraft. A data comparison device compares the indicated real-time intended operations of the aircraft with actual monitored operations of the aircraft to discern unacceptable deviations. Data sources include operator-generated data transmissions, voice transcriptions, automated voice recognized information, measurable operations of the aircraft, and prescribed operating guidance, directives and parameters for the aircraft.

3. 发明申请

US20170185083A1 METHOD FOR GUIDING AN AIRCRAFT 审中-公开
公开(公告)号：US20170185083A1
公开(公告)日：2017-06-29
申请号：US15304833
申请日：2015-04-22
申请人： Safran Electronics & Defense
发明人： Julien FARJON
IPC分类号： G05D1/00 , G08G5/02 , G08G5/06
CPC分类号： G05D1/0083 , G01C23/00 , G06K9/00637 , G08G5/025 , G08G5/065
摘要： The invention relates to a method for guiding an aircraft along a reference path, said method comprising: a) when the altitude of the aircraft is greater than a threshold, estimating (E1) a relative location of the aircraft in relation to a taxiing starting point using a map of the platform and reference points on the ground, b) when the altitude of the aircraft is less than said threshold and before the aircraft is located at the taxiing starting point, estimating (E2) a relative location of the aircraft in relation to the taxiing starting point using data relating to the absolute location of the aircraft and the last relative location estimated at step a), c) when the aircraft is located at the taxiing starting point, guiding (E3) the aircraft on the basis of a location of the aircraft relative to the reference path as estimated using data relating to a set of indicators on the ground.

4. 发明授权

US09547993B2 Automated aircraft ground threat avoidance system 有权
标题翻译：自动飞机地面威胁避免系统
公开(公告)号：US09547993B2
公开(公告)日：2017-01-17
申请号：US14629017
申请日：2015-02-23
申请人： Honeywell International Inc.
发明人： Ratan Khatwa , Jayasenthilnathan B
IPC分类号： G08G5/06 , G08G5/04 , G08G5/00 , G01S19/51 , G01S13/93 , B64D45/04 , G05D1/00
CPC分类号： G08G5/04 , B64D45/04 , G01S13/93 , G01S19/51 , G05D1/0061 , G05D1/0083 , G05D1/0676 , G08G5/0021 , G08G5/045 , G08G5/06 , G08G5/065
摘要： This disclosure is directed to methods, systems, and computer program products for automated avoidance of ground threats by an aircraft. In one example, a method includes determining, by one or more processing devices, whether a sufficient evasive maneuver for an aircraft to avoid a detected ground surface threat is performed via pilot controls of the aircraft within a selected threshold after an alert of the ground surface threat is outputted via one or more cockpit systems of the aircraft. The method further includes, in response to determining that a sufficient evasive maneuver via the pilot controls is not performed within the selected threshold, controlling, by the one or more processing devices, one or more flight systems of the aircraft to perform an automated evasive maneuver to avoid the ground surface threat.
摘要翻译：本公开涉及用于自动避免飞机的地面威胁的方法，系统和计算机程序产品。在一个示例中，一种方法包括通过一个或多个处理装置来确定在飞机的地面的警报之后是否通过飞行员在所选择的阈值内的飞行员控制来执行用于飞机避免检测到的地面威胁的足够的回避机动通过飞机的一个或多个驾驶舱系统输出威胁。该方法还包括响应于确定在所选择的阈值内不执行经由导频控制的足够的回避机动，由一个或多个处理装置控制飞行器的一个或多个飞行系统执行自动回避机动以避免地面的威胁。

5. 发明申请

US20160161949A1 AIRCRAFT WING STRUCTURE AND CONTROL SYSTEM 有权
标题翻译：飞机结构与控制系统
公开(公告)号：US20160161949A1
公开(公告)日：2016-06-09
申请号：US14907067
申请日：2014-07-25
申请人： Michael LAM , Greg COLE , Lam Aviation, Inc.
发明人： Michael LAM , Greg COLE
IPC分类号： G05D1/00 , B64C9/20 , G05D1/08 , B64C13/38 , B64C9/04
CPC分类号： G05D1/0083 , B64C9/04 , B64C9/20 , B64C13/38 , B64C2009/005 , G05D1/0816 , Y02T50/32
摘要： An aircraft includes a wing. The wing includes an aileron pivotally connected to a trailing edge of the wing, and a Lam aileron pivotally connected to the trailing edge of the wing. The aircraft includes a motor connected to the Lam aileron and configured to rotate the Lam aileron. The aircraft includes a controller configured to detect a deflection of the aileron from a neutral position, calculate a target deflection for the Lam aileron using the deflection of the aileron, and cause the motor to rotate the Lam aileron to the target deflection.
摘要翻译：飞机包括一个机翼。机翼包括枢转地连接到翼的后缘的副翼和枢转地连接到翼的后缘的Lam副翼。该飞机包括连接到Lam副翼并配置为旋转Lam副翼的马达。飞机包括控制器，该控制器被配置为检测来自中立位置的副翼的偏转，使用副翼的偏转来计算Lam副翼的目标偏转，并使马达将Lam副翼旋转到目标偏转。

6. 发明申请

US20160122007A1 Method for Defining and Controlling Aircraft Taxi Profile 有权
标题翻译：定义和控制飞机出租车配置文件的方法
公开(公告)号：US20160122007A1
公开(公告)日：2016-05-05
申请号：US14531339
申请日：2014-11-03
申请人： Borealis Technical Limited
发明人： Isaiah W. Cox , Rodney T. Cox , Aaron Z. Sichel
IPC分类号： B64C25/40 , G05D17/02 , B64D41/00
CPC分类号： B64C25/405 , B60L11/00 , B60L2200/10 , G05D1/0083 , G05D1/0223 , G05D17/02 , G08G5/065 , Y02T50/823
摘要： A system and method are provided for defining, optimizing, and controlling taxi profiles for aircraft equipped with onboard non-engine drive means controllable to drive one or more nose or main landing gear wheels to drive an aircraft autonomously during taxi. An onboard taxi profile control system may employ smart software to determine selected taxi operational data at an airport and use this data to control and maintain torque of the drive means at desired selected levels that move the aircraft during taxi in response to determined taxi data or predetermined programmed taxi parameters. The system is designed to set default taxi profiles for each taxi cycle to achieve efficient aircraft taxi and to extend operational life of drive means components. Taxi profiles are modified and updated at periodic intervals or in real time in response to actual taxi conditions to optimize aircraft taxi at a specific airport.
摘要翻译：提供了一种用于定义，优化和控制配备有车载非发动机驱动装置的飞机的出租车轮廓的系统和方法，该装置可控制地驱动一个或多个鼻子或主起落架轮，以便在出租车期间自主地驾驶飞行器。车上出租车轮廓控制系统可以使用智能软件来确定在机场处的选定的出租车操作数据，并使用该数据来控制和维持驱动装置的扭矩，以期望的选定水平，以响应于确定的出租车数据或预定的编程出租车参数。该系统旨在为每个出租车周期设置默认的出租车轮廓，以实现高效的飞机出租车，并延长驱动装置部件的使用寿命。出租车配置文件将按照实际的出租车条件定期或实时地进行修改和更新，以优化特定机场的飞机出租车。

7. 发明申请

US20150301531A1 LANDING GEAR FORCE AND MOMENT DISTRIBUTOR 有权
标题翻译：起重齿轮和动力分配器
公开(公告)号：US20150301531A1
公开(公告)日：2015-10-22
申请号：US14443252
申请日：2013-11-15
申请人： AIRBUS OPERATIONS LIMITED , AIRBUS OPERATIONS SAS
发明人： Miguel Angel GAMA-VALDEZ , Louis-Emmanuel ROMANA , Andrea DAMIANI , Michael Richard WHINCUP
IPC分类号： G05D1/00 , G05D1/02 , B64C25/48 , B64C25/34 , B64C25/40
CPC分类号： G05D1/0083 , B60T8/1703 , B60T8/1766 , B64C25/00 , B64C25/10 , B64C25/18 , B64C25/26 , B64C25/34 , B64C25/405 , B64C25/48 , B64C2025/008 , G05D1/0202 , Y02T50/823
摘要： A landing gear force and moment distributor system for an aircraft having a longitudinal axis aligned in a forward-aft direction, a vertical axis perpendicular to the longitudinal axis, and a landing gear including a pair of bogies arranged symmetrically about the longitudinal axis, each bogie having an actuator arranged to brake and/or drive one or more wheels. The force distribution system includes a distribution module arranged to: receive an input demand including a longitudinal force input demand corresponding to a desired braking or driving force along the longitudinal axis for the landing gear and a moment input demand corresponding to a desired moment about the vertical axis for the landing gear; and to use the received input demand to calculate an output command including, for each bogie, a longitudinal force output command corresponding to a braking or driving force along the longitudinal axis to be applied to the bogie
摘要翻译：用于飞行器的起落架力矩和力矩分配器系统，其具有沿着前后方向对准的纵向轴线，垂直于纵向轴线的垂直轴线，以及起落架，其包括围绕纵向轴线对称布置的一对转向架，每个转向架具有用于制动和/或驱动一个或多个车轮的致动器。力分配系统包括分配模块，该分配模块被布置成：接收包括沿着用于起落架的纵向轴线的期望制动或驱动力的纵向力输入需求的输入需求，以及对应于围绕垂直方向的期望力矩的力矩输入需求轴起落架; 并且使用所接收的输入需求来计算包括对于每个转向架的输出命令，该纵向力输出命令对应于沿纵轴的制动或驱动力，以被施加到转向架

8. 发明授权

US09134730B2 Method of managing a turning movement of an aircraft taxiing on the ground 有权
标题翻译：管理在地面上滑行的飞机转弯运动的方法
公开(公告)号：US09134730B2
公开(公告)日：2015-09-15
申请号：US13099450
申请日：2011-05-03
申请人： David Lemay , David Frank , Michel Basset , Yann Chamaillard
发明人： David Lemay , David Frank , Michel Basset , Yann Chamaillard
IPC分类号： A01B69/00 , B62D6/00 , B62D11/00 , B62D12/00 , B63G8/20 , B63H25/04 , G05D1/00 , G06F7/00 , G06F17/00 , G06F19/00 , B64C25/40
CPC分类号： G05D1/0083 , B64C25/405 , Y02T50/823
摘要： The invention relates to a management method for managing a turning movement of an aircraft taxiing on the ground, the aircraft having wheels each fitted with an independent drive device, in which method commands are generated for the independent drive devices so that at least some of those devices contribute to the turning movement. According to the invention, the method comprises the steps of: estimating at each instant during the turning movement: an instantaneous total power developed by all of the independent drive devices in response to the commands; and an instantaneous mean angular acceleration for all of the wheels; and adapting the commands to the independent drive devices such that the total instantaneous power developed by all of the independent drive devices is minimized, while conserving the mean angular acceleration.
摘要翻译：本发明涉及一种用于管理在地面上滑行的飞行器的转动运动的管理方法，所述飞机具有各自装配有独立驱动装置的轮子，其中为独立驱动装置生成指令，使得至少一些装置有助于转弯运动。根据本发明，该方法包括以下步骤：在转动运动期间的每个瞬间估计：由所有独立驱动装置响应命令产生的瞬时总功率; 和所有车轮的瞬时平均角加速度; 并且使命令适应独立的驱动装置，使得由所有独立驱动装置产生的总瞬时功率最小化，同时节省平均角加速度。

9. 发明授权

US09105186B2 Method for aiding the taxiing of an aircraft 有权
标题翻译：协助飞机滑行的方法
公开(公告)号：US09105186B2
公开(公告)日：2015-08-11
申请号：US12640106
申请日：2009-12-17
申请人： Pascal Gayraud , Nicolas Marty , Julia Percier
发明人： Pascal Gayraud , Nicolas Marty , Julia Percier
IPC分类号： G06F19/00 , G05D1/00 , G08G5/06 , G08G5/00
CPC分类号： G08G5/065 , G05D1/0083 , G08G5/0013 , G08G5/0043
摘要： The invention relates to a method for aiding the taxiing of an aircraft comprising a plurality of onboard propulsion means and which is able to move over an airport zone according to at least one specific taxiing procedure making it possible to reduce fuel consumption, the method being characterized in that it implements the following steps during the phase of taxiing of the aircraft on an airport:Checking of the taxiing conditions for the implementation of the said taxiing procedure and calculation of the implementation parameters of the procedure, Calculation of the taxiing performance data resulting from the implementation of the taxiing procedure, Display of the taxiing directives and performance related to the taxiing procedure, Monitoring of the parameters of the avionics systems during the implementation of the taxiing procedure.The invention applies to taxiing plan formulation systems and/or aircraft monitoring systems.
摘要翻译：本发明涉及一种用于帮助飞机的滑行的方法，其包括多个机载推进装置，并且能够根据至少一个特定的滑行程序在机场区域上移动，使得可以减少燃料消耗，该方法被表征因为它在飞机在机场的滑行阶段中执行以下步骤：检查执行所述滑行程序的滑行条件和计算程序的执行参数，计算由执行滑行程序，显示滑行指示和与滑行程序有关的表现，在执行滑行程序期间监测航空电子系统的参数。本发明适用于滑行计划制定系统和/或飞机监控系统。

10. 发明授权

US09082299B2 Methods and systems for taxiway traffic alerting 有权
标题翻译：滑行道交通警报的方法和系统
公开(公告)号：US09082299B2
公开(公告)日：2015-07-14
申请号：US13533394
申请日：2012-06-26
申请人： Tomas Kabrt , Tomas Marczi , J. Howard Glover , Matej Dusik
发明人： Tomas Kabrt , Tomas Marczi , J. Howard Glover , Matej Dusik
IPC分类号： G08G5/00 , G08G5/04 , G08G5/06 , G05D1/00 , G08G1/16 , B60Q9/00 , B64F1/00
CPC分类号： G08G5/0008 , B60Q9/008 , B64F1/002 , G05D1/0083 , G08G1/16 , G08G5/0021 , G08G5/0078 , G08G5/045 , G08G5/065
摘要： Systems and methods for providing the crew of a vehicle with a potential collision alert. The alert is based on presumed flight-crew action and reaction times, ownship speed, and required distance to safely stop the ownship before intersection with traffic. An exemplary system located aboard an ownship includes a communication device that receives information from a ground traffic; a memory device that stores ownship information and predefined constants; and a processing device that determines a distance to the traffic when the traffic passes the ownship after the ownship stops at a estimated full-stop location, based on the received ownship information and the predefined constants, determines distance to the ground traffic vehicle, based on the determined point in time, and generates a potential collision alert if the determined distance is less than a predefined safe distance value. An exterior lighting device outputs a visual illumination after the potential collision alert is generated.
摘要翻译：为车辆的船员提供潜在的碰撞警报的系统和方法。该警报基于假定的机组人员行动和反应时间，拥有速度以及在与交通相交之前安全停止自己的所需距离。位于本身的示例性系统包括从地面业务接收信息的通信设备; 存储自身信息和预定义常数的存储器件; 以及处理装置，其基于所接收的本体信息和预定义的常数，基于所接收到的本地信息和预定义常数来确定在自身在估计的全停止位置停止之后交通通过本身的交通的距离，基于确定的时间点，并且如果所确定的距离小于预定义的安全距离值，则产生潜在的碰撞警报。在产生潜在的碰撞警报之后，外部照明装置输出视觉照明。

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