公开(公告)号：US20190295425A1

公开(公告)日：2019-09-26

申请号：US16357639

申请日：2019-03-19

Applicant: DASSAULT AVIATION

Inventor： Cyrille GRIMALD ,  Benjamin BRIAND

IPC: G08G5/00

Abstract: A system for establishing an operational flight plan includes a basic flight data acquisition unit for acquiring basic flight data from an external flight plan development system, the basic flight data comprising at least one theoretical fuel weight to be loaded into the aircraft. The system also includes an aircraft actual operational specifications acquisition unit for acquiring actual operational specifications of the aircraft, the actual operational specifications including an airplane context; a proposed flight data calculating unit for calculating proposed flight data including at least one proposed weight of fuel corresponding to the theoretical weight, calculated based on actual operational specifications of the aircraft and a specified trajectory of the aircraft; and a viewer, and a display manager capable of displaying a proposed flight data display window including the proposed fuel weight.

公开(公告)号：US20160259673A1

公开(公告)日：2016-09-08

申请号：US15058895

申请日：2016-03-02

Applicant: DASSAULT AVIATION

Inventor： Benjamin BRIAND

IPC: G06F9/54 ,  G06F17/30

CPC classification number: G06F9/546 ,  G06F17/30312 ,  G06F17/30371 ,  G08G5/0034

Abstract: A management method is provided for managing data relative to an aircraft mission comprising at least one flight by an aircraft, the data comprising input data of at least two applications and output data of the applications, each application being able to be executed by a computer to determine, from the input data of the application, the output data. The method includes a step for providing a set of generic data, each of the generic data being an input datum shared by at least two of the applications, a step for assigning a value to at least one of the generic data for at least one flight of the mission, and a step for configuring the applications comprising the automatic assignment, to each input datum corresponding to a generic datum, of the value of the generic datum.

Abstract translation: 提供一种管理方法，用于管理飞机任务的数据，包括飞行器的至少一个飞行，该数据包括至少两个应用的输入数据和应用的输出数据，每个应用能够被计算机执行 从应用的输入数据确定输出数据。 该方法包括提供一组通用数据的步骤，每个通用数据是由至少两个应用程序共享的输入数据，用于将值分配给至少一个飞行中的至少一个通用数据的步骤 的任务的一个步骤，以及将包括自动分配的应用程序配置到通用数据的值的对应于通用数据的每个输入数据的步骤。

公开(公告)号：US20210374101A1

公开(公告)日：2021-12-02

申请号：US17332319

申请日：2021-05-27

Applicant: DASSAULT AVIATION

Inventor： Benjamin BRIAND ,  Michaël OCIEPKA ,  Stéphane ARDOUIN ,  Vincent HUBERT ,  Nicolas LHOPITEAU

IPC: G06F16/178

Abstract: An aircraft computer file distribution system comprises a store (36) of aircraft computer files for loading into at least one aircraft device (12) that is onboard, mobile or replicated on the ground. The system includes a file manager (44), configured for identifying an aircraft configuration of the aircraft with which the aircraft device (12) is associated and a computer configuration of the aircraft device (12); defining, among the computer files in the computer file store (36), at least one computer file loadable into the aircraft device (12) according to the identified aircraft configuration and computer configuration; and activating a synchronization for remote distribution of at least one computer file to be loaded into the aircraft device (12) selected from the one or more computer files loadable into the aircraft device (12) based on the identified aircraft configuration and computer configuration.

公开(公告)号：US20190164440A1

公开(公告)日：2019-05-30

申请号：US16199045

申请日：2018-11-23

Applicant: DASSAULT AVIATION

Inventor： Benjamin BRIAND ,  Cédric CARLE ,  Stéphane DRINAL ,  Cyrille GRIMALD ,  Jean-François SAEZ ,  Cyril SAINT REQUIER ,  Jean-Baptiste VALLART

IPC: G08G5/00 ,  G01C23/00

Abstract: An aircraft mission computing system includes an aircraft mission path computing engine, and a mission deck comprising a display and a display management assembly configured for displaying, on the display, at least one button for defining an operational specification of the mission. The computing engine is configured to be activated after defining the choice of operational specification using the definition button to determine at least one possible path of the aircraft based on the or each choice of defined operational specification using the or each definition button. The display management assembly is configured to display, on the display, after the activation of the computing engine, at least one outcome indicator providing mission feasibility information while respecting the or each operational specification choice.