公开(公告)号：US20170038223A1

公开(公告)日：2017-02-09

申请号：US14819956

申请日：2015-08-06

Applicant: Airbus (S.A.S.)

Inventor： Jean-Jacques Toumazet ,  Mélanie Vadillo

IPC: G01C23/00

CPC classification number: G01C23/005 ,  B64D45/00

Abstract: A display management system is provided for displaying a graphical representation of flight envelope information of an aircraft. Included in the display management system is a control module being coupled to the display management system and programmed to control the graphical representation including at least one flight envelope protection attribute. A signal detection module receives signals from a plurality of sensors of the aircraft, and the received signals include associated parameter values for the at least one flight envelope protection attribute. A protection selection module selects the at least one flight envelope protection attribute based on the received signals and parameter values. A display module displays the at least one flight envelope protection attribute on a display screen in relation to a flight control law state stored in a database using a display model of the aircraft from an elevational view based on the received signals and parameter values.

Abstract translation: 提供了显示管理系统，用于显示飞行器的飞行信封信息的图形表示。 包括在显示管理系统中的是控制模块，其耦合到显示管理系统并被编程以控制包括至少一个飞行包线保护属性的图形表示。 信号检测模块从飞行器的多个传感器接收信号，并且所接收的信号包括用于至少一个飞行包线保护属性的相关参数值。 保护选择模块基于接收到的信号和参数值来选择至少一个飞行包线保护属性。 基于接收到的信号和参数值，显示模块使用飞机的显示模型从正视图显示与显示屏上相对于存储在数据库中的飞行控制律状态的显示屏上的至少一个飞行包线保护属性。

公开(公告)号：US20160340057A1

公开(公告)日：2016-11-24

申请号：US14715269

申请日：2015-05-18

Applicant: AIRBUS (S.A.S.)

Inventor： Dang NGUYEN MANH ,  David MARTY ,  Gerald BIDAULT ,  Massimiliano DI SANTO ,  Fabien FLEUREY

IPC: B64F5/00

CPC classification number: G06Q10/20

Abstract: Methods, systems, and computer readable media for managing periodic aircraft maintenance planning are provided. In some aspects, a method occurs at a maintenance platform server including a processor. The method includes providing one or more maintenance related object (MO), wherein each of the one or more MO represents one or more maintenance related task that includes criteria graphically depicted at an interface. In another aspect, the method further includes manipulating the criteria of the one or more maintenance related task represented by the one or more MO at the interface.

Abstract translation: 提供了用于管理定期飞行器维护计划的方法，系统和计算机可读介质。 在某些方面，在包括处理器的维护平台服务器处发生一种方法。 该方法包括提供一个或多个维护相关对象（MO），其中一个或多个MO中的每一个表示一个或多个维护相关任务，其包括在界面处以图形方式描绘的标准。 在另一方面，该方法还包括操纵由界面处的一个或多个MO表示的一个或多个维护相关任务的标准。

公开(公告)号：US09452901B2

公开(公告)日：2016-09-27

申请号：US14303979

申请日：2014-06-13

Applicant: Airbus Operations GmbH ,  Airbus S.A.S.

Inventor： Uwe Panzram ,  Joerg Klockgether ,  Philippe Le Bigot ,  Peter Esteie ,  Netra Gowda

IPC: B65G67/00 ,  B64D9/00 ,  B64C1/20

CPC classification number: B65G67/00 ,  B64C1/20 ,  B64D9/00 ,  B64D2009/006

Abstract: A system for loading and unloading a cargo compartment of a vehicle, such as an aircraft, with a cargo receiving device is provided. The system includes a cargo receiving device including a base structure arrangement having a horizontal lower contact surface, and a locking mechanism configured to engage one or more corresponding holding members provided in a cargo compartment of a vehicle. The system also includes a transport device including a horizontal upper contact surface configured to be disposed in abutting contact to said lower contact surface, a drive unit configured to initiate horizontal movement of the transport device, a lift unit configured to initiate vertical movement of the upper contact surface, and an actuating unit configured to actuate the locking mechanism of the cargo receiving device.

Abstract translation: 提供了一种用于装载和卸载诸如飞机的车辆的货舱与货物接收装置的系统。 该系统包括货物接收装置，该货物接收装置包括具有水平下接触表面的基部结构装置，以及锁定机构，其构造成接合设置在车辆的货舱中的一个或多个对应的保持构件。 该系统还包括一个输送装置，该输送装置包括构造成与所述下接触表面邻接接触的水平上接触表面;驱动单元，构造成启动输送装置的水平运动;升降单元，其构造成启动上部 接触表面以及构造成致动货物接收装置的锁定机构的致动单元。

公开(公告)号：US09233760B2

公开(公告)日：2016-01-12

申请号：US14184081

申请日：2014-02-19

Applicant: AIRBUS OPERATIONS (S.A.S.) ,  AIRBUS (S.A.S.)

Inventor： Catalin Perju ,  Laurent Delessard ,  Jerome Robillard

IPC: B64D43/02 ,  G01P13/02 ,  G01D5/347 ,  G01D5/34

CPC classification number: B64D43/02 ,  G01D5/342 ,  G01D5/3473 ,  G01P13/025

Abstract: The invention relates to an angle measurement probe on board an aircraft, which comprises a fin, which can move in rotation about an axis, at least one first optical encoder and one second optical encoder, each comprising at least one disk, each disk being fixed at right angles to the central axis and being provided with at least two circular tracks, each track being provided with alternate opaque and transparent zones, means for processing the output signal from each encoder.

Abstract translation: 本发明涉及一种飞机上的角度测量探针，其包括可围绕轴线旋转的翅片，至少一个第一光学编码器和一个第二光学编码器，每个包括至少一个盘，每个盘固定 与中心轴成直角并且设置有至少两个圆形轨道，每个轨道设置有替代的不透明区域和透明区域，用于处理来自每个编码器的输出信号的装置。

公开(公告)号：US09221551B2

公开(公告)日：2015-12-29

申请号：US13891629

申请日：2013-05-10

Applicant: Airbus (S.A.S.)

Inventor： Amaury Leroy ,  Séverine Vermande

IPC: B64D45/00 ,  G08G5/00 ,  G07C5/00

CPC classification number: B64D45/00 ,  G07C5/008 ,  G08G5/0008 ,  H04B7/18506 ,  H04W4/42

Abstract: The invention relates to a method for transmitting data, characterized in that it includes a step of transmitting in-flight data between a first aircraft and at least a second aircraft, the data transmitted being data stored in at least one black box on board the first aircraft.

Abstract translation: 本发明涉及一种用于发送数据的方法，其特征在于，它包括在第一飞行器和至少第二飞行器之间发送飞行中数据的步骤，所发送的数据是存储在第一飞行器上的至少一个黑匣子中的数据 飞机。

公开(公告)号：US20150348422A1

公开(公告)日：2015-12-03

申请号：US14723503

申请日：2015-05-28

Applicant: AIRBUS GROUP INDIA PRIVATE LIMITED ,  AIRBUS S.A.S

Inventor： ASHUTOSH AGRAWAL ,  NETRA GOWDA

IPC: G08G5/00 ,  G08G5/06

CPC classification number: G08G5/0095 ,  G06Q10/06 ,  G08G5/0013 ,  G08G5/06

Abstract: A system and method for providing an aircraft turnaround schedule are disclosed. In one embodiment, a time taken for each aircraft turnaround activity is obtained from touchdown to takeoff of an aircraft from an aircraft on-board system by a ground station system. Further, the aircraft turnaround schedule is computed based on the obtained time taken for each aircraft turnaround activity using a dynamic buffer management approach by the ground station system.

Abstract translation: 公开了一种用于提供飞行器周转时间表的系统和方法。 在一个实施例中，每个飞行器周转活动所花费的时间从地面站系统从飞机起飞到飞机机载系统获得。 此外，基于由地面站系统使用动态缓冲器管理方法的每个飞机周转活动所获得的时间来计算飞行器周转时间表。

公开(公告)号：US20150295157A1

公开(公告)日：2015-10-15

申请号：US14694638

申请日：2015-04-23

Applicant: Airbus Operations (S.A.S.) ,  Airbus (S.A.S.)

Inventor： Philippe Tatry ,  Sébastien Berhouet

IPC: H01L35/30

CPC classification number: H01L35/30 ,  H01L35/32

Abstract: An energy conversion system comprising: a conversion unit for converting thermal energy into electrical energy, said unit comprising at least one thermal exchange surface for exchanging thermal energy with at least one external heat source, and a thermal inertia unit configured to cooperate with the conversion unit to slow down the return of the conversion unit to thermal equilibrium during the exchange of thermal energy.

Abstract translation: 一种能量转换系统，包括：用于将热能转换成电能的转换单元，所述单元包括用于与至少一个外部热源交换热能的至少一个热交换表面，以及配置成与转换单元配合的热惯性单元 以减少转换单元在热能交换期间的热平衡。

公开(公告)号：US20150123820A1

公开(公告)日：2015-05-07

申请号：US14070895

申请日：2013-11-04

Applicant: Airbus S.A.S. ,  Airbus Operations S.A.S.

Inventor： Jean Michel Merle ,  Frédéric Dehais ,  Philippe Pellerin ,  Laure Christophe ,  Justine Beaucamp ,  Mickaël Causse

IPC: B64D45/00

CPC classification number: B64D45/00 ,  A61B5/18 ,  B60K28/066 ,  G06K9/00845

Abstract: Methods and systems are provided for determining over focalization of a pilot of an aircraft. The method includes receiving human parameter data from one or more systems that observe conditions associated with the pilot and receiving controls data that indicates an interaction of the pilot with one or more control systems of the aircraft. The method includes, based on the human parameter data and the controls data, generating at least one alert. The method also includes communicating the at least one alert to the pilot to change a focus of the pilot.

Abstract translation: 提供了用于确定飞机飞行员的聚焦的方法和系统。 该方法包括从观察与飞行员相关联的条件的一个或多个系统接收人参数数据，以及接收指示飞行员与飞行器的一个或多个控制系统的相互作用的控制数据。 该方法包括基于人类参数数据和控制数据，生成至少一个警报。 该方法还包括将该至少一个警报传达给飞行员以改变飞行员的焦点。

公开(公告)号：US20250029505A1

公开(公告)日：2025-01-23

申请号：US18775593

申请日：2024-07-17

Applicant: AIRBUS (S.A.S.)

Inventor： Jinming HUANG

IPC: G08G5/04 ,  G06T15/10 ,  G06V20/58 ,  G08G5/00

Abstract: An aircraft ground anti-collision system and method is disclosed including multiple sensors including an on-board sensor and an off-board sensor, and an obstacle detection processing unit, which is configured to: process data received from the multiple sensors to detect an object around the aircraft and/or a trailer for towing the aircraft, and fuse sensing ranges of the multiple sensors and unify information about the object detected by the multiple sensors in a same coordinate system, to generate a view-angle fused view indicating the detected object. Hence, vision blind areas of a pilot and a ground operator during ground movement of the aircraft can be advantageously eliminated, and the cooperation and scene awareness of the pilot and the ground operator can be improved, thereby reducing the accident rate and improving the safety of the ground movement.

公开(公告)号：US20240402330A1

公开(公告)日：2024-12-05

申请号：US18675242

申请日：2024-05-28

Applicant: Airbus (S.A.S.)

Inventor： Markus Klügel ,  Nunzio Sciammetta

IPC: G01S13/87 ,  G01S7/00 ,  G01S13/933 ,  G08G5/00

Abstract: An urban air mobility system includes aerial vehicles, a detection platform, and a fusion platform. The aerial vehicles include one cooperative aerial vehicle and one data consuming aerial vehicle. The detection platform detects a position of flight objects and transmits first data indicative of the position of the detected flight objects to the fusion platform. The cooperative aerial vehicle detects a relative position of flight objects in its surroundings and transmits second data indicative of the relative position of detected flight objects to the fusion platform. The fusion platform fuses the first data and the second data and generates an air traffic scenario. The data consuming aerial vehicle and the cooperative aerial vehicle receive the air traffic scenario from the fusion platform.