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1. 发明公开

EP4242100A1 PALONNIER D'AÉRONEF AVEC STRUCTURE ARTICULÉE DE SUPPORT DE PÉDALE 审中-实审
公开(公告)号：EP4242100A1
公开(公告)日：2023-09-13
申请号：EP23160203.8
申请日：2023-03-06
申请人： Dassault Aviation
发明人： PISTIAUX, Laurent , MATEUS, Vincent
IPC分类号： B64C13/04 , B64C25/44 , B64C13/06 , B64C13/12
摘要： L'invention concerne un palonnier (22) d'aéronef comprenant un bâti (28) et au moins un système latéral pédalier (30), le ou chaque système latéral pédalier (30) comprenant une pédale (32) et une structure articulée de support (34) de la pédale connectant la pédale (32) au bâti (28).
La structure articulée de support (34) de ladite pédale (32) comprend une manivelle (48), un levier (52) et une bielle de support (54), la manivelle (48) présentant une première liaison pivot d'articulation (50) avec le bâti (28) et une deuxième liaison pivot d'articulation (56) avec la bielle de support (54), le levier (52) présentant une première liaison pivot d'articulation (58) avec le bâti (28) et une deuxième liaison pivot d'articulation (60) avec la bielle de support (54).

2. 发明授权

EP3335914B1 VEHICLE INCLUDING CONTROL PEDAL ARRANGEMENT 有权
公开(公告)号：EP3335914B1
公开(公告)日：2019-11-13
申请号：EP16203802.0
申请日：2016-12-13
申请人： AeroMobil R&D, s. r. o.
发明人： MACANDREW, Doug , ROOMS, Simon , ROACH, Alan , FAZEKAS, Slavomir , GREÑ, Martin
IPC分类号： B60F5/02 , B64C13/04 , B64C13/06 , B64C37/00

3. 发明授权

EP3124378B1 PALONNIER REGLABLE ET ROTATIF POUR UN AERONEF A VOILURE TOURNANTE 有权
公开(公告)号：EP3124378B1
公开(公告)日：2019-04-17
申请号：EP16178532.4
申请日：2016-07-08
申请人： Airbus Helicopters
发明人： GEMMATI, Bernard , FEUGAS, Florian , PUJOL, Christophe
IPC分类号： B64C13/06

4. 发明授权

EP3102488B1 GESCHLEPPTER AKTIVER FLUGKÖRPER ZUR ERMITTLUNG VON MESSDATEN 有权
标题翻译： GESCHLEPPTER AKTIVERFLUGKÖRPERZUR ERMITTLUNG VON MESSDATEN
公开(公告)号：EP3102488B1
公开(公告)日：2017-04-26
申请号：EP15708707.3
申请日：2015-01-24
申请人： Alfred-Wegener-Institut Helmholtz-Zentrum für Polar- und Meeresforschung
发明人： HERBER, Andreas , KALMBACH, Dirk , GERDES, Rüdiger , WATSON, James Bradley
IPC分类号： B64C13/06 , B64D3/00
CPC分类号： B64D3/00 , B64C9/326 , B64C13/16 , B64C2009/005 , B64D27/24 , B64D45/00 , B64D47/08

5. 发明授权

EP2917102B1 MODULAR, ABOVE-THE-FLOOR RUDDER AND BRAKE CONTROL SYSTEM 有权
标题翻译：模块化舵和制动控制系统安装地板
公开(公告)号：EP2917102B1
公开(公告)日：2016-09-28
申请号：EP13799708.6
申请日：2013-11-11
申请人： Mason Electric Co.
发明人： CARNER, Fred , SALAMAT, Bijan
IPC分类号： B64C13/04 , B64C13/06 , B64C13/50
CPC分类号： B64C13/06 , B64C13/04 , B64C13/503

6. 发明公开

EP1305210A1 ENVIRONMENTAL CONTROL SYSTEM UTILIZING TWO AIR CYCLE MACHINES 有权
标题翻译：冷却系统，两个空气循环发动机
公开(公告)号：EP1305210A1
公开(公告)日：2003-05-02
申请号：EP01959279.9
申请日：2001-07-27
申请人： Hamilton Sundstrand Corporation
发明人： HIPSKY, Harold
IPC分类号： B64C13/06 , F25B9/00
CPC分类号： B64D13/06 , B64D2013/0662 , F05B2220/50 , F25B9/004 , Y02T50/56
摘要： An environmental control system and method are provided for conditioning water-vapor compressed air for supply as conditioned air. The environmental control system (8) includes two air cycle machines (9, 10) that rotate independent of each other. The air cycle machine (9) includes a turbine (11) that drives a fan (12), and the air cycle machine (10) includes a turbine (15) that drives a compressor 816). The environmental control system (8) further includes a primary heat exchanger (19= upstream of the compressor (16), a secondary heat exchanger (20) downstream of the compressor (16), a reheater (21) downstream of the secondary heat exchanger (20), a condenser (22) downstream of the reheater (21), a water collector (24) downstream of the condenser (22), and three bypass control valves (28, 30, 32). In combination, the turbine (11), reheater (21), condenser (22), and water collector (24) form a dehumidification loop (34) for the environmental control system (8). In one mode of operation, the environmental control system (8) further compresses the compressed air in the compressor (16) and then dehumidifies the further compressed air in the turbine (15) to cool the dehumidified further compressed air and to power the compressor (16) in the absence of rotating engagement between the turbine (15) and the turbine (11).

7. 发明授权

EP4025495B1 RUDDER AND BRAKE PEDAL ASSEMBLY 有权
公开(公告)号：EP4025495B1
公开(公告)日：2024-04-17
申请号：EP20811857.0
申请日：2020-10-29
IPC分类号： B64C13/04 , B64C13/06 , B64C13/08 , B64C13/50 , G05G1/30
CPC分类号： B64C13/044 , B64C13/06 , B64C13/08 , B64C13/50 , B64C13/503 , G05G1/44 , G05G9/02 , G05G13/00

8. 发明公开

EP3798120A1 RETENTION OF FLIGHT DECK PREFERENCES 审中-公开
公开(公告)号：EP3798120A1
公开(公告)日：2021-03-31
申请号：EP20198774.0
申请日：2020-09-28
申请人： Rockwell Collins, Inc.
发明人： KLEIN, Clifford R. , VALESTIN, Jason J.
IPC分类号： B64C13/04 , B64C13/06 , B64D11/00 , B64D11/06 , B64D43/00 , B64D45/00 , G01C23/00 , G01C25/00
摘要： A system and method for retention of flight deck preferences operates to control a comprehensive combination of aircraft systems and system configurations enabling a pilot to seamlessly retain and recall the desired preferences based on a plurality of mission related factors. With system control of flight deck physical settings including seat position and shape, display illumination and color and internal and external lighting configurations, the system allows a pilot to save time, effort, and minimize errors of system set up and configuration. With a short entry, or short-range sensing, of the pilot ID, the pilot commands the system and method for retention of flight deck preferences to configure each of the plurality of aircraft systems according to the recalled pilot preference.

9. 发明授权

EP3323027B1 CONTROL NORMALIZATION FOR UNMANNED AUTONOMOUS SYSTEMS 有权
公开(公告)号：EP3323027B1
公开(公告)日：2019-06-26
申请号：EP16729673.0
申请日：2016-05-23
申请人： Qualcomm Incorporated
发明人： CHAU, Kiet Tuan , CANOY, Michael-David Nakayoshi , DEVICO, Michael Orlando , SPRIGG, Stephen Alton
IPC分类号： B64C13/06 , B64C39/02 , G05B13/04 , G05D1/00

10. 发明公开

EP3659910A1 JAM MITIGATION IN AIRCRAFT FLY-BY-WIRE SYSTEMS AND RELATED METHODS 有权
公开(公告)号：EP3659910A1
公开(公告)日：2020-06-03
申请号：EP19205557.2
申请日：2019-10-28
申请人： The Boeing Company
发明人： HUYNH, Neal V. , ELLIOTT, Joseph E.
IPC分类号： B64C13/04 , B64C13/50 , G05D1/08 , B64C13/06 , B64C13/08 , B64C13/10 , B64C13/12 , B64C13/14
摘要： Systems and methods for jam mitigation in aircraft fly-by-wire systems are described herein. An example method of controlling an aircraft with a fly-by-wire system includes determining a current position of a pilot cockpit controller of the fly-by-wire system, determining an amount of pilot input force applied to the pilot cockpit controller, determining an expected pilot input force value that corresponds to the current position of the pilot cockpit controller, and, if the amount of pilot input force applied exceeds the expected pilot input force value by a threshold, generating a pilot command based on the amount of pilot input force applied and not the current position of the pilot cockpit controller.

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