公开(公告)号：US20190237726A1

公开(公告)日：2019-08-01

申请号：US16331102

申请日：2017-09-08

Applicant: THALES

Inventor： Eric Ravindranath DUBOIS ,  Hocine KHERBOUCHI ,  Joël BOSSON

IPC: H01M2/10 ,  H01M2/06 ,  H01M2/02 ,  H01M2/30 ,  H01M10/42 ,  H01G9/08 ,  H01G9/008 ,  H01G9/28 ,  H01G9/26

CPC classification number: H01M2/1094 ,  H01G9/008 ,  H01G9/08 ,  H01G9/26 ,  H01G9/28 ,  H01M2/0285 ,  H01M2/06 ,  H01M2/1077 ,  H01M2/30 ,  H01M2/305 ,  H01M2/34 ,  H01M10/4257 ,  H01M10/4264 ,  H01M2010/4278 ,  H01M2200/00 ,  H01M2250/20 ,  H02H7/00 ,  H02J7/00 ,  H02J7/0029 ,  H02J7/0045 ,  H02J7/007 ,  H03H7/06 ,  Y02T90/32

Abstract: The protection of an electrical energy accumulation device from electromagnetic attacks is provided. The electrical energy accumulation device comprises a housing made of an electrically conductive material, at least one electrical energy storage cell that is arranged in the housing and two terminals that are arranged through the housing, the terminals being electrically insulated from the housing, the terminals allowing electrical energy to be transferred between the at least one storage cell and the exterior of the device. The device further comprises, inside the housing, a specific component exhibiting an impedance having at least one resistive component that is higher than 1 ohm, which component is configured to dissipate the energy of electromagnetic interference attempting to penetrate the housing through at least one of the terminals.

公开(公告)号：US20190196927A1

公开(公告)日：2019-06-27

申请号：US16226188

申请日：2018-12-19

Applicant: Thales

Inventor： Joël BOSSON ,  Frederick Clement ,  Patrick Cadotte ,  Marc Fumey ,  Jean-Christophe Reculeau

IPC: G06F11/30 ,  G06F11/07 ,  G05B23/02 ,  G05B9/02

CPC classification number: G06F11/3013 ,  G05B9/02 ,  G05B23/0208 ,  G06F11/0739 ,  G06F11/0796 ,  G06F11/1608 ,  G06F11/1633 ,  G06F11/1637

Abstract: A programmable electronic computer embedded in an avionics environment on board an aircraft for implementing at least one critical function and associated electronic device, method and computer program are disclosed. In one aspect, the electronic computer includes at least one control module configured to implement a respective critical function and configured to deliver at least one output data item associated with the critical function, and at least one monitoring module of a control module of another electronic computer. Each monitoring module configured to implement the same respective critical function as the one implemented by the monitored control module.

公开(公告)号：US20170323571A1

公开(公告)日：2017-11-09

申请号：US15319489

申请日：2015-06-05

Applicant: THALES

Inventor： Sylvain LISSAJOUX ,  Eric GUILLOUET ,  Christophe GARNAVAULT ,  Joël BOSSON

IPC: G08G5/00 ,  G01C23/00 ,  G05D1/02

CPC classification number: G08G5/0039 ,  G01C23/005 ,  G05D1/0061 ,  G05D1/0202 ,  G08G5/0052 ,  G08G5/045

Abstract: This method makes it possible to generate a resulting setpoint trajectory of an aircraft, a guiding system controlling the trajectory of the aircraft relative to the resulting setpoint trajectory.The generating method is implemented by an electronic device and comprises selecting at least one mode from among several operating modes, acquiring a setpoint trajectory prepared by a flight management system, obtaining an alternative setpoint trajectory from an element from among a module for computing a trajectory and an external generating system, and generating the resulting setpoint trajectory, which includes one or several segments of the alternative setpoint trajectory for the period of time corresponding to the selection of another mode.

公开(公告)号：US20130158750A1

公开(公告)日：2013-06-20

申请号：US13721636

申请日：2012-12-20

Applicant: THALES ,  LIEBHERR AEROSPACE TOULOUSE SAS

Inventor： Joël BOSSON ,  Vincent GOMEZ

IPC: B64C19/00

CPC classification number: B64C19/00 ,  H02J3/14 ,  H02J4/00

Abstract: Energy management on board an aircraft includes: a plurality of thermal and electrical energy sources, a plurality of loads which are capable of being supplied with power by the various energy sources, among which at least one load is capable of being supplied with power by an electrical energy source and by a thermal energy source, and real-time management means for energy transfers from the various energy sources to the various loads as a function of the present and future energy requirement of the various loads and the present and future availability of the various sources, with the management means providing a permanent and standardized correlation between thermal and electrical energies.

Abstract translation: 飞机上的能量管理包括：多个热能和电能源，能够被各种能量源供电的多个负载，其中至少一个负载能够通过 电能源和热能源，以及用于从各种能源到各种负载的能量转移的实时管理手段，作为各种负载的当前和未来能量需求的函数以及当前和将来可用性 各种来源，管理手段提供热能和电能之间永久和标准化的相关性。