-
公开(公告)号：US11538346B2
公开(公告)日：2022-12-27
申请号：US16458483
申请日：2019-07-01
发明人： Jean-Claude Mere , Sylvain Raynaud
摘要： A flight management assembly of an aircraft and method of monitoring the flight management assembly. The assembly includes two flight management systems, and a monitoring and backup unit, each of the flight management systems configured for generating data including a trajectory and a prediction of a parameter of the aircraft, one of the flight management systems being active and the other being passive, the monitoring and backup unit configured for carrying out monitoring of at least one of the items of data generated by the active flight management system in order to verify if the item of data is valid, the flight management assembly carrying out, in case of validation of the monitored item of data, a synchronization of the monitoring and backup unit and of the passive flight management system, with data called synchronization data of the active flight management system, namely a flight plan and/or a flight trajectory.
-
公开(公告)号：US11524192B2
公开(公告)日：2022-12-13
申请号：US17362568
申请日：2021-06-29
摘要： A propulsion assembly including a turbomachine attached to a pylon, and a fire-fighting system, the turbomachine including fire zones, the fire-fighting system including two reservoirs of pressurized extinguishing agent in the pylon and a distribution line connecting the reservoirs to nozzles. The distribution line includes connected pipes having a low point between the reservoirs and the nozzles, and, for each low point, a fluid drainage device for evacuating fluid. The drainage device includes a fluid passage for fluid evacuation from the distribution line and a mechanism for shutting off the fluid passage, the mechanism movable under effect of distribution line pressure, between a first position where it opens the fluid passage and a second position where it closes the fluid passage, the second position being reached when the pressure in the distribution line is greater than or equal to a predetermined pressure.
-
公开(公告)号：US11486318B2
公开(公告)日：2022-11-01
申请号：US17317321
申请日：2021-05-11
发明人： Patrick Zaccaria , David Boyer
摘要： To control an engine shutdown in an aircraft, a control system includes a fuel supply shut-off member, a control member with a set of switches, a first switch on an electrical power supply link of the fuel supply shut-off member and second switches connected to avionics of the aircraft, the set of switches switching position on an engine shutdown command. An engine shutdown confirmation unit includes a third switch on the electrical power supply link, the third switch in open position by default. The engine shutdown confirmation unit includes electronic circuitry configured to switch the third switch over to closed position when a predefined quantity Q of switches of the control member switches position within a sliding window of predefined duration and, otherwise, keeps the third switch in open position. Thus, it is ensured that the engine shutdown is intentional.
-
公开(公告)号：US11467607B2
公开(公告)日：2022-10-11
申请号：US16369214
申请日：2019-03-29
发明人： Jean-luc Robin , José Torralba , Julie Lebas
摘要： Method and device for determining trajectory to optimal position of a follower aircraft with respect to vortices generated by a leader aircraft. The method includes controlling trajectory of a follower aircraft to an optimal position where the follower aircraft benefits from effects of at least one of the vortices of a leader aircraft. A first section control step controls flight of the follower aircraft using current measurements of flight parameters, from a safety position to a search position, along an approach section passing through an approach zone. A second section control step controls flight of the follower aircraft using current measurements of flight parameters, from the search position to a precision position, along a search section passing through a search zone, and a third section control step controls flight of the follower aircraft, from the precision position to the optimal position, along an optimization section passing through an optimization zone.
-
公开(公告)号：US11427348B2
公开(公告)日：2022-08-30
申请号：US16708794
申请日：2019-12-10
发明人： Anne-laure Desclaux-Chevalier , Serge Passemar , Christelle Senegas , Jean-Christophe Rey , Emmanuelle Escorihuela , Christophe Bressy
IPC分类号： B64D45/00 , B64F5/60 , G06F16/245
摘要： A method and device for optimizing tests of systems, in particular of an aircraft, including a first display module displaying a list of tests that can be executed by systems, a selection module allowing an operator to select a set of tests to be executed and communicate it to an optimization module which determines a sequence of tests representing an optimized execution of the set of tests to be executed, the sequence of tests being displayed by a second display module for an operator, a decision module generating either a first signal if the operator validates the sequence of tests, or a second signal if the operator cancels the sequence of tests, and a control module which, if the first signal is generated, commands the execution of the sequence of tests by each of the systems, and generates results of the execution thereof.
-
公开(公告)号：US11426968B2
公开(公告)日：2022-08-30
申请号：US16828302
申请日：2020-03-24
发明人： Florian Ravise , Florent Mercat
IPC分类号： B32B3/12 , G10K11/168 , B32B3/26
摘要： An assembly constituting an acoustically absorbent material and including a first panel, a second panel pierced with holes, an intermediate panel pierced with through-holes and arranged between the first panel and the second panel, a first structure between the first panel and the intermediate panel and including first cages, a second structure between the second panel and the intermediate panel and including second cages, and for each through-hole of the intermediate panel, a tube opening out at the two ends thereof, where one of the ends of the tube is fixed to the intermediate panel at the through-hole, and where the other end of the tube is accommodated inside a first cage. Such an assembly makes it possible to obtain broad-band attenuation and is easy to manufacture.
-
公开(公告)号：US11408337B2
公开(公告)日：2022-08-09
申请号：US16253548
申请日：2019-01-22
发明人： Jean Geliot , Adeline Soulie
IPC分类号： F02C6/04 , B64D27/26 , B64D29/02 , B64D33/08 , F01D25/24 , F01D25/12 , F02C7/18 , F02C6/08 , B64D33/10 , F28D7/10 , B64D27/18 , B64D13/08 , B64D33/02 , F28F1/06 , F02C7/047 , F28D7/14 , F28D21/00
摘要： An aircraft pylon including a heat exchange device having a heat exchanger which includes a first circuit portion ducting a flow of hot air tapped off an engine of the aircraft and a second circuit portion ducting a flow of cold air, the first and second circuit portions of the heat exchanger being coaxial, separated by at least one partition forming an exchange surface, and positioned, at least partially, in the primary structure of the pylon.
-
8.发明授权公开(公告)号：US11388509B2
公开(公告)日：2022-07-12
申请号：US17029793
申请日：2020-09-23
摘要： An acoustic reflector for a microphone to measure flyover noise generated by an aircraft. The microphone is configured to measure flyover noise generated by an aircraft flying on a preset path. The acoustic reflector includes at least a central portion having the shape of an ellipse having a major axis and a plurality of peripheral portions distributed around the central portion. The acoustic reflector allows edge effects to be attenuated at the low frequencies of the noise to be measured.
-
公开(公告)号：US10949991B2
公开(公告)日：2021-03-16
申请号：US16349799
申请日：2018-12-07
发明人： Fengmei Nie , Wei Liu , Dongchun Ren , Jian Wang , Meng Yang , Xiaohu Gong
摘要： Disclosed is a method and apparatus for determining a position of a pupil. The method includes: acquiring an image to be detected including a pupil; acquiring a binary image of a preset area based on a preset model of semi-supervised learning, where the preset area is an area where the pupil is located in the image to be detected; acquiring a centroid of the binary image; and determining a central position of the pupil according to the centroid of the binary image.
-
公开(公告)号：US11535402B2
公开(公告)日：2022-12-27
申请号：US16842304
申请日：2020-04-07
发明人： Gonzalo Martin Gomez , Hector Sanchez Paredero , Francisco José Lagares Carrasco , Samuel De La Fuente Lopez
摘要： A system for monitoring the degradation status of refueling hoses on air includes a device with at least one sensor adapted to produce data about the external surface of the refueling hose. The method for monitoring the degradation status of refueling hoses on air includes moving a device with at least one sensor along a refueling hose or moving a refueling hose with respect to the device, producing data about the external surface of the refueling hose from the at least one sensor, and analyzing the data for monitoring the degradation status of the refueling hose. It allows providing a system and method for monitoring the degradation status of refueling hoses on air that reduces the risk of personal injury associated to hose damage inspection and is cost saving.
-
-
-
-
-
-
-
-
-
搜索结果
36 条记录 (耗时 0.026 秒)
