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    HIGH-LIFT FLAP, ARRANGEMENT OF A HIGH-LIFT FLAP TOGETHER WITH A DEVICE FOR INFLUENCING THE FLOW ON THE SAME AND AIRCRAFT COMPRISING SAID ARRANGEMENT
    1.
    发明申请
    HIGH-LIFT FLAP, ARRANGEMENT OF A HIGH-LIFT FLAP TOGETHER WITH A DEVICE FOR INFLUENCING THE FLOW ON THE SAME AND AIRCRAFT COMPRISING SAID ARRANGEMENT 审中-公开
    HIGH电梯门，高升门与设备流量的影响在同一平面，采用这样的布局安排

    公开(公告)号：WO2010084025A3

    公开(公告)日：2011-12-08

    申请号：PCT/EP2010000447

    申请日：2010-01-26

    Applicant: AIRBUS OPERATIONS GMBH ,  GOELLING BURKHARD ,  HANSEN HEINZ ,  RADESPIEL ROLF ,  JENSCH CHRISTOPH ,  PFINGSTEN KAI-CHRISTOPH ,  NEITZKE KLAUS-PETER

    Inventor： GOELLING BURKHARD ,  HANSEN HEINZ ,  RADESPIEL ROLF ,  JENSCH CHRISTOPH ,  PFINGSTEN KAI-CHRISTOPH ,  NEITZKE KLAUS-PETER

    IPC: B64C21/08 ,  B64C21/02

    CPC classification number: B64C21/025 ,  B64C9/18 ,  B64C21/08 ,  B64C2230/04 ,  B64C2230/06 ,  Y02T50/166

    Abstract: The invention relates to an aerodynamic body (K) of an aircraft, which has a first lateral face and a second lateral face, both extending along the flap depth direction (KT) and a flow flowing around them in a direction of flow (S). The first lateral face on the regulating flap has a top surface (11) extending along the intake side and the second side is a lower surface (12) extending along the pressure side (B) of the regulating flap (K), at least one air outlet opening and at least one air inlet opening being arranged on the regulating flap (K), the air inlet opening communicating with the air outlet opening via at least one air conduit (30, 31, 32, 33, 34, 35, 36). A flow delivery drive (40, 41, 42) for influencing the flow within the air conduit (30, 31, 32, 33, 34, 35, 36) is integrated with the air conduit (30, 31, 32, 33, 34, 35, 36) and following openings are provided at the lateral faces of the regulating flap (K) in the flap depth direction (KT): at least one air outlet opening which is arranged in the front area (10a) of the regulating flap (K), when seen in the direction of flow, said area extending across up to 15% of the flap depth (KT), and at least one air inlet opening (23) which is arranged on the top surface of the regulating flap and in the rear area (10b) of the regulating flap (K), when seen in the direction of flow, extending across 30% to 90% of the flap depth (KT), and/or on the top surface of the regulating flap in the rear edge area (10c) extending across 90% to 100% of the flap depth (KT), and/or on the lower surface of the regulating flap in the rear edge area (10c) of the regulating flap (K) extending across 90% to 100% of the flap depth (KT). The invention further relates to arrangements of a main wing and a regulating flap (K) and to an aircraft having said aerodynamic body.

    Abstract translation: 流线型体的飞行器的（K），其包括第一侧表面和第二侧表面，沿着翼片深度（KT）上延伸，并且在流动方向（S）的预期目的流周围，其中，所述第一侧表面与所述调节瓣意一个沿 是延伸的上侧（11）吸入侧，而沿延伸的下部面（12）的调节襟翼（K），压力侧（B）的第二侧，其中，所述可调节襟翼（K）的至少一个空气出口开口并通过至少一个空气管线的至少一种（ 与所述进气口的空气出口开口连通30，31，32，33，34，35，36）被布置，其中（与空气管线30，31，32，33，34，35，36）的流量输送驱动器（ 40，41，42）用于影响空气管线内的流动（30，31，32，33，34，35，36）是集成的，并且其中（在翼片深度R中的蝶形阀K）的侧表面上 看出ichtung（KT），提供了下面的端口： - 至少一个 - 在流动方向看到的正面的至少一个，并且延伸到延伸的调节襟翼的部分（10a）的（K）和空气出口开口襟翼深度的15％（KT）， 空气入口开口（23），看到的蝶形阀的上侧和（10b）的所述调节襟翼的（K）和/或所述蝶形阀的上侧在延伸的30％和90％的翼片深度（KT）区域之间的流动的方向的后方 的延伸的后缘部（10c）的和/或在设置（K）的调节瓣的瓣片深度（KT）后缘区域（10C）的90％至100％的蝶形阀的下侧延伸的翼片深度（KT）的90％至100％; 主翼和蝶形阀（K）以及飞机与这样的流线型体的组合件。

    HIGH-LIFT SYSTEM FOR AN AIRCRAFT
    2.
    发明申请
    HIGH-LIFT SYSTEM FOR AN AIRCRAFT 审中-公开
    飞机高架系统

    公开(公告)号：WO2011076425A3

    公开(公告)日：2011-10-13

    申请号：PCT/EP2010007921

    申请日：2010-12-23

    Applicant: AIRBUS OPERATIONS GMBH ,  GOELLING BURKHARD

    Inventor： GOELLING BURKHARD

    IPC: B64C9/18

    CPC classification number: B64C9/18 ,  B64C9/16 ,  B64C9/38 ,  B64C21/04 ,  Y02T50/166 ,  Y02T50/32 ,  Y02T50/44

    Abstract: A high-lift system (100) with a main wing (112) and adjustable flaps (110) as well as guiding devices (130) for holding the adjustable flaps (110) and adjustment devices (120) for adjusting the adjustable flaps (110), wherein the respective guiding device (130) and/or adjustment device (120) at least in part comprise/comprises a fairing (118), comprising a flow influencing (10) device for influencing the flow around the high- lift system (100), with at least one inlet line (20) with at least one inlet that is situated on or below the bottom of the high- lift system (100), wherein, furthermore, at least one outlet line (30) for air is provided that comprises a fluid-communicating connection to the inlet line (10) and comprises at least one outlet situated at the top in the region of at least one adjustable flap (110) of the high-lift system (100).

    Abstract translation: 具有主翼（112）和可调节翼片（110）的高升力系统（100）以及用于保持可调节翼片（110）和用于调节可调节翼片（110）的调节装置（120）的引导装置（130） ），其中相应的引导装置（130）和/或调节装置（120）至少部分地包括/包括整流罩（118），包括用于影响高升力系统周围的流动的流动影响装置（10） 至少一个入口管线（20）具有至少一个入口，所述至少一个入口位于所述高升程系统（100）的底部上或下方，其中，至少一个用于空气的出口管线（30） 条件是包括与入口管线（10）的流体连通的连接，并且包括位于高升程系统（100）的至少一个可调整的挡板（110）的区域中的顶部的至少一个出口。

    AIRCRAFT WITH A CONTROL DEVICE
    3.
    发明申请
    AIRCRAFT WITH A CONTROL DEVICE 审中-公开
    带有控制装置的飞机

    公开(公告)号：WO2011076427A3

    公开(公告)日：2011-11-10

    申请号：PCT/EP2010007923

    申请日：2010-12-23

    Applicant: AIRBUS OPERATIONS GMBH ,  GOELLING BURKHARD ,  HAUCKE FRANK ,  BAUER MATTHIAS ,  NITSCHE WOLFGANG ,  PELTZER INKEN

    Inventor： GOELLING BURKHARD ,  HAUCKE FRANK ,  BAUER MATTHIAS ,  NITSCHE WOLFGANG ,  PELTZER INKEN

    IPC: B64C9/18 ,  B64C13/00

    CPC classification number: B64C23/005 ,  B64C9/16 ,  B64C9/38 ,  B64C13/18 ,  B64C21/04 ,  B64C29/0025 ,  Y02T50/166

    Abstract: An aircraft (F) with aerofoils (1a, 1b) comprising a main wing (M) and at least one control flap (S) that is arranged so as to be adjustable relative to the aforesaid, and comprising at least one adjustment flap (K), with the aircraft comprising: - an actuator (21 ) for operating the at least one control flap (S), as well as a sensor device (24) for acquiring the set position of the control flap (S), - at least one arrangement (15; 15K) of flow-influencing devices (16; 16K), which extends on the main wing (M) and/or of at least one adjustment flap (K) of each aerofoil (M; 1a, 1b), for the purpose of influencing the fluid that flows over the surface segment (10; 10K) and - at least one arrangement of flow-state sensor devices (17; 17K) for measuring the flow state on the respective segment (10; 11a, 12a; 11b, 12b), - a flight control device (50) which on the input side is functionally connected to the sensor device (24) for acquiring the set position of the control flap (S) and to the flow-state sensor devices (16; 16K) and which flight control device (50) for the purpose of transmitting actuating commands (50a) on the output side is functionally connected to the actuator (21) and the flow-influencing devices (16;16K), - a flight-state sensor device (40) functionally connected to the flight control device (50) for transmitting flight states, wherein the flight control device (50) comprises a function that for the purpose of optimising local lift coefficients on the aerofoil depending on the flight state carries out a selection of the flow-influencing devices (16; 16K) that are to be operated.

    Abstract translation: 一种具有翼型件（1a，1b）的飞机（F），其包括主翼（M）和至少一个控制襟翼（S），所述控制襟翼被布置成相对于前述可调节并且包括至少一个调节襟翼 ），其中所述飞机包括： - 用于操作所述至少一个控制襟翼（S）的致动器（21），以及用于获取所述控制襟翼（S）的设定位置的传感器装置（24）， - 至少 在每个机翼（M; 1a，1b）的主机翼（M）和/或至少一个调整襟翼（K）上延伸的流动影响装置（16; 16K）的一个装置（15; 15K） ，以便影响在表面区段（10; 10K）上流动的流体以及 - 用于测量相应区段（10; 11a，12a）上的流动状态的流动状态传感器装置（17; 17K） ; 11b，12b）; - 飞行控制装置（50），其在输入侧功能性地连接到传感器装置（24）以获取控制襟翼（S）的设定位置和f 低状态传感器设备（16; 16K），并且用于在输出侧传输致动命令（50a）的飞行控制装置（50）功能性地连接到致动器（21）和流动影响装置（16; 16K）， - 飞行状态 传感器装置（40）功能性地连接到所述飞行控制装置（50）以传输飞行状态，其中所述飞行控制装置（50）包括以下功能：为了根据所述飞行状态优化所述机翼上的局部升力系数 选择要操作的流动影响装置（16; 16K）。

    AIRCRAFT WITH A CONTROL DEVICE
    4.
    发明申请
    AIRCRAFT WITH A CONTROL DEVICE 审中-公开
    具有控制装置的飞机

    公开(公告)号：WO2011076427A8

    公开(公告)日：2011-09-01

    申请号：PCT/EP2010007923

    申请日：2010-12-23

    Applicant: AIRBUS OPERATIONS GMBH ,  GOELLING BURKHARD ,  HAUCKE FRANK ,  BAUER MATTHIAS ,  NITSCHE WOLFGANG ,  PELTZER INKEN

    Inventor： GOELLING BURKHARD ,  HAUCKE FRANK ,  BAUER MATTHIAS ,  NITSCHE WOLFGANG ,  PELTZER INKEN

    IPC: B64C9/18

    CPC classification number: B64C23/005 ,  B64C9/16 ,  B64C9/38 ,  B64C13/18 ,  B64C21/04 ,  B64C29/0025 ,  Y02T50/166

    Abstract: An aircraft (F) with aerofoils (1a, 1b) comprising a main wing (M) and at least one control flap (S) that is arranged so as to be adjustable relative to the aforesaid, and comprising at least one adjustment flap (K), with the aircraft comprising: - an actuator (21 ) for operating the at least one control flap (S), as well as a sensor device (24) for acquiring the set position of the control flap (S), - at least one arrangement (15; 15K) of flow-influencing devices (16; 16K), which extends on the main wing (M) and/or of at least one adjustment flap (K) of each aerofoil (M; 1a, 1b), for the purpose of influencing the fluid that flows over the surface segment (10; 10K) and - at least one arrangement of flow-state sensor devices (17; 17K) for measuring the flow state on the respective segment (10; 11a, 12a; 11b, 12b), - a flight control device (50) which on the input side is functionally connected to the sensor device (24) for acquiring the set position of the control flap (S) and to the flow-state sensor devices (16; 16K) and which flight control device (50) for the purpose of transmitting actuating commands (50a) on the output side is functionally connected to the actuator (21) and the flow-influencing devices (16;16K), - a flight-state sensor device (40) functionally connected to the flight control device (50) for transmitting flight states, wherein the flight control device (50) comprises a function that for the purpose of optimising local lift coefficients on the aerofoil depending on the flight state carries out a selection of the flow-influencing devices (16; 16K) that are to be operated.

    Abstract translation: 一种具有机翼（1a，1b）的飞机（F），包括主翼（M）和至少一个控制翼片（S），其布置成相对于前述可调节，并且包括至少一个调节翼片 ），所述飞行器包括： - 用于操作所述至少一个控制翼片（S）的致动器（21）以及用于获取所述控制翼片（S）的设定位置的传感器装置（24），至少 在主翼（M）和/或每个机翼（M; 1a，1b）的至少一个调节片（K）上延伸的流量影响装置（16; 16K）的一个排列（15; 15K） 用于影响在表面段（10; 10K）上流动的流体;以及 - 用于测量相应段（10; 11a，12a）上的流动状态的流态传感器装置（17; 17K）的至少一个布置 ; 11b，12b）， - 飞行控制装置（50），其在所述输入侧上功能性地连接到所述传感器装置（24），用于获取所述控制翼片（S）的设定位置和所述f 低状态传感器装置（16; 16K），并且用于在输出侧发送致动指令（50a）的目的的飞行控制装置（50）功能地连接到致动器（21）和流量影响装置（16; 16K）， - 飞行状态 传感器装置（40）功能上连接到用于传送飞行状态的飞行控制装置（50），其中飞行控制装置（50）包括用于根据飞行状态来优化机翼上的局部升力系数的功能， 选择将被操作的流量影响装置（16; 16K）。

    A HIGH LIFT SYSTEM FOR AN AIRCRAFT
    6.
    发明申请
    A HIGH LIFT SYSTEM FOR AN AIRCRAFT 审中-公开
    一种用于飞机的高升降系统

    公开(公告)号：WO2011110327A3

    公开(公告)日：2011-12-01

    申请号：PCT/EP2011001130

    申请日：2011-03-08

    Applicant: AIRBUS OPERATIONS GMBH ,  GOELLING BURKHARD

    Inventor： GOELLING BURKHARD

    IPC: B64C9/18 ,  B64C21/04 ,  B64C21/08

    CPC classification number: B64C21/04 ,  B64C9/18 ,  B64C21/06 ,  B64C21/08 ,  B64C2230/04 ,  B64C2230/06 ,  Y02T50/166 ,  Y02T50/44

    Abstract: A high lift system with a main wing and control flaps, wherein the respective guiding device are at least partially provided with a fairing, having a flow control device for purposes of controlling the flow around the high lift system with at least two inlet ducts running along the main wing chordwise direction with in each case at least one inlet, which device is located on or underneath the lower surface of the high lift system, wherein at least one outlet duct for air is furthermore provided, which is connected with the inlet ducts in a fluid-communicating manner, and has at least one outlet, which is located on the upper surface of at least one regulating flap and/or with respect to the main wing chordwise direction in the rear third of the main wing of the high lift system.

    Abstract translation: 具有主翼和控制翼片的高升力系统，其中相应的引导装置至少部分地设置有整流罩，具有用于控制高升力系统周围的流动的流量控制装置，其中至少两个进气道沿着 主翼翼弦方向分别具有至少一个入口，该装置位于高升力系统的下表面上或下方，其中还设置有至少一个用于空气的出口管道，该出口管道与入口管道连接 并且具有至少一个出口，该出口位于高升力系统的主翼的后三分之一中的至少一个调节襟翼的上表面上和/或相对于主翼弦向方向 。

    A HIGH LIFT SYSTEM FOR AN AIRCRAFT
    8.
    发明申请
    A HIGH LIFT SYSTEM FOR AN AIRCRAFT 审中-公开
    用于飞机的高升程系统

    公开(公告)号：WO2011076428A3

    公开(公告)日：2011-10-13

    申请号：PCT/EP2010007924

    申请日：2010-12-23

    Applicant: AIRBUS OPERATIONS GMBH ,  GOELLING BURKHARD ,  LORKOWSKI THOMAS

    Inventor： GOELLING BURKHARD ,  LORKOWSKI THOMAS

    IPC: B64C9/18

    CPC classification number: B64C21/04 ,  B64C9/16 ,  B64C9/38 ,  Y02T50/166 ,  Y02T50/44

    Abstract: A high lift system (100) with a main wing (112) and regulating flaps (110), also bearing devices (130) for the mounting of the regulating flaps (110), and positioning devices (120) for the positioning of the regulating flaps (110), wherein the respective bearing device (130) and/or positioning device (120) is at least partially provided with a fairing (118), having a flow control device (10) for purposes of controlling the flow around the high lift system (100) with at least one inlet duct (20) with at least one inlet (22), which device is located on or underneath the lower face (104) of the high lift system (10), wherein at least one outlet duct (30) for air is furthermore provided, which is connected with the inlet duct (20) in a fluid - communicating manner, and has at least one outlet (110), which is located on the upper face (102) in the region of at least one regulating flap of the high lift system (100).

    Abstract translation: 具有主翼（112）和调节翼片（110）的高升程系统（100）以及用于安装调节翼片（110）的轴承装置（130）和用于定位调节板的定位装置（120） 翼片（110），其中相应的轴承装置（130）和/或定位装置（120）至少部分地设置有整流罩（118），其具有流量控制装置（10），用于控制围绕高度的流动 提升系统（100），其具有至少一个具有至少一个入口（22）的入口管道（20），该装置位于高升降系统（10）的下表面（104）上或下方，其中至少一个出口 进一步提供用于空气的管道（30），其以流体连通的方式与入口管道（20）连接，并且具有至少一个出口（110），其位于区域中的上表面（102）上 的至少一个高升程系统（100）的调节挡板。

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