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    AIRCRAFT AVIONICS SYSTEM
    2.
    发明公开
    AIRCRAFT AVIONICS SYSTEM 有权
    飞机航空系统

    公开(公告)号：EP2459963A1

    公开(公告)日：2012-06-06

    申请号：EP09781181.4

    申请日：2009-07-28

    申请人： PILATUS FLUGZEUGWERKE AG

    发明人： O'CONNOR, Daniel ,  CERVIA, Bruno ,  MILNS, Robert ,  GIBSON, Paul

    IPC分类号： G01C21/00 ,  G01C23/00 ,  G09B9/08 ,  G08G5/00

    CPC分类号： G01C23/00 ,  G01C21/00 ,  G08G5/0021 ,  G09B9/16

    摘要： An aircraft avionics system (10) for an aircraft, comprising a mission system (2), controlled by an open systems mission computer (OSMC) with a tactical communications system (320) and a tactical navigation system (220); a civil system (1), controlled by a flight management system (FMS) with a civil communications system (310) and a civil navigation system (210), wherein said mission system (2) is logically separated from the civil system (1) through separation of a navigation system (20) of the aircraft into civil navigation system (210) and tactical navigation system (220) and through separation of a communications system (30) of the aircraft (100) into said tactical communications system (320) and said civil communications system (310) and through the independence of the open systems mission computer (OSMC) from the flight management system (FMS), said separation allowing the civil system (1) to operate and be updated independently from the mission system (2).

    Propeller-driven aircraft with improved stability about its yaw axis
    4.
    发明公开
    Propeller-driven aircraft with improved stability about its yaw axis 有权
    Propellerflugzeug mit verbesserterStabilitätum seine Hochachse

    公开(公告)号：EP1293427A1

    公开(公告)日：2003-03-19

    申请号：EP01122167.8

    申请日：2001-09-15

    申请人： PILATUS FLUGZEUGWERKE AG

    发明人： Bretscher, Dietmar ,  Tyndall, William

    IPC分类号： B64D31/06 ,  F02D29/02 ,  G05D1/08

    CPC分类号： B64D31/06 ,  F02D29/02 ,  G05D1/0833

    摘要： Propeller-driven aircraft (30) comprising an engine (31) providing mechanical engine power for rotating a propeller (32), an engine limiting unit (35), an engine control unit (37) for controlling the mechanical engine power of the engine (31), a system (36) for measuring the airspeed and providing information concerning the airspeed to the engine limiting unit (35), wherein the engine limiting unit (35) automatically reduces the mechanical engine power at airspeeds below a certain first airspeed value (V1).

    摘要翻译： 螺旋桨驱动的飞机（30）包括提供用于旋转螺旋桨（32）的机械发动机功率的发动机（31），发动机限制单元（35），用于控制发动机的机械发动机功率的发动机控制单元（37） 31，一种用于测量空速并提供与发动机限制单元（35）的空速有关的信息的系统（36），其中发动机限制单元（35）自动地将空速下的机械发动机功率降低到低于某一第一空速值 V1）。

    DIGITAL RECORDING AND REPLAY SYSTEM FOR AN AIRCRAFT AND METHOD FOR REPRODUCTION OF ONBOARD INSTRUMENTATION OF AN AIRCRAFT
    6.
    发明公开
    DIGITAL RECORDING AND REPLAY SYSTEM FOR AN AIRCRAFT AND METHOD FOR REPRODUCTION OF ONBOARD INSTRUMENTATION OF AN AIRCRAFT 审中-公开
    用于飞机的数字记录和重放系统以及用于生成飞行器的在机仪器的方法

    公开(公告)号：EP3312563A1

    公开(公告)日：2018-04-25

    申请号：EP17186158.6

    申请日：2010-12-06

    申请人： PILATUS FLUGZEUGWERKE AG

    发明人： O'Connor, Daniel ,  Cervia, Bruno ,  Milns, Robert ,  Gibson, Paul

    IPC分类号： G01C23/00 ,  G09B9/08

    CPC分类号： G01C23/00 ,  G07C5/085 ,  G09B9/08

    摘要： Digital recording and replay system (100) for an aircraft, comprising a Mission Computer (MC) with an Operational Flight Program (OFP) for generating instrument data (ID) for onboard instruments of the aircraft; a Mission Data Recorder (MDR) connected to said Mission Computer (MC) for recording said instrument data (ID); and a Mission Debriefing System (MDS);wherein the Mission Debriefing System (MDS) is configured to reproduce the onboard instruments of the aircraft based on instrument data (ID) retrieved from the Mission Data Recorder (MDR). Method for reproduction of onboard instrumentation of an aircraft, comprising the steps of connecting a Mission Data Recorder (MDR) to a Mission Computer (MC) of an aircraft having an Operational Flight Program (OFP) for generating instrument data (ID) for onboard instruments; recording instrument data (ID); providing a Mission Debrief System (MDS) and causing it to reproduce the onboard instruments of the aircraft based on instrument data (ID) retrieved from the Mission Data Recorder (MDR).

    摘要翻译： 一种用于飞机的数字记录和重放系统（100），包括具有操作飞行程序（OFP）的任务计算机（MC），用于生成飞行器的机载仪器的仪器数据（ID） 连接到所述任务计算机（MC）的任务数据记录器（MDR），用于记录所述仪器数据（ID）; 和任务报告系统（MDS）;其中任务报告系统（MDS）被配置为基于从任务数据记录器（MDR）检索的仪器数据（ID）来再现飞机的机载仪器。 一种用于再现飞机的机载仪器的方法，包括以下步骤：将任务数据记录器（MDR）连接到具有操作飞行程序（OFP）的飞机的任务计算机（MC），以生成用于机载仪器的仪器数据 ; 记录仪器数据（ID）; 提供任务汇报系统（MDS），并根据从任务数据记录器（MDR）检索到的仪器数据（ID）复制飞机的机载仪器。

    Aircraft wing
    8.
    发明公开
    Aircraft wing 有权
    Flugzeugflügel

    公开(公告)号：EP1475304A1

    公开(公告)日：2004-11-10

    申请号：EP03010467.3

    申请日：2003-05-09

    申请人： PILATUS FLUGZEUGWERKE AG

    发明人： Verdan, Patrice R.

    IPC分类号： B64C3/28

    CPC分类号： B64C3/28

    摘要： The wing has a structural part (15) and a separable complementary part (10) designed in a way that it can be mounted respectively dismounted in the structural part of the wing reproducing the form of a desired standard wing. Said complementary part constitutes at least partially a leading edge of the wing and comprises a space filled with an energy absorption material which constitutes a core (14) of said leading edge.

    摘要翻译： 机翼具有结构部件（15）和可分离的互补部件（10），其可以被安装成分别被拆卸在机翼的结构部分中，再现所需标准机翼的形式。 所述互补部分至少部分地构成翼的前缘，并且包括填充有能量吸收材料的空间，该能量吸收材料构成所述前缘的芯（14）。

    CONFORMAL ENERGY BAY
    10.
    发明公开
    CONFORMAL ENERGY BAY 审中-实审

    公开(公告)号：EP4420984A2

    公开(公告)日：2024-08-28

    申请号：EP24182964.7

    申请日：2019-04-11

    申请人： PILATUS FLUGZEUGWERKE AG

    发明人： CERVIA, Bruno

    IPC分类号： B64D27/02

    CPC分类号： B64D37/08 ,  B64D9/00 ,  B64C1/22 ,  B64D27/026

    摘要： In an aircraft (A, A.1, A.2) comprising at least one bay (1, 1.1, 1.2) for receiving different types of standardized modules, the bay (1, 1.1, 1.2) is configured to receive at least two different types of energy modules (6, 7, 8, 9, 10, 11) as standardized modules.