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81. 发明公开

EP3224135A1 FLIGHT CONTROL SYSTEM FOR A ROTARY WING AIRCRAFT 有权
标题翻译：旋翼式飞机的飞行控制系统
公开(公告)号：EP3224135A1
公开(公告)日：2017-10-04
申请号：EP15863227.3
申请日：2015-09-24
申请人： Sikorsky Aircraft Corporation
发明人： WULFF, Ole
IPC分类号： B64C5/10 , B64C27/57 , G05D1/08
CPC分类号： G05D1/0858 , B64C13/16 , B64C27/10 , B64C27/57 , B64C27/82 , B64C2027/8236 , B64C2027/8272 , B64C2027/8281
摘要： A rotary wing aircraft includes an airframe including an extending tail. The airframe includes a longitudinal axis that extends through the extending tail. The rotary wing aircraft also includes a main rotor assembly including at least one rotor hub supporting a plurality of rotor blades configured and disposed to rotate about a main rotor axis, at least one elevator arranged at the extending tail, and a control system operably connected to the main rotor assembly and the at least one elevator. The control system is configured and disposed to adjust each of a pitch rate and an attitude of the airframe by selectively adjusting a position of the at least one elevator.
摘要翻译：旋翼飞机包括具有延伸尾部的机身。机身包括延伸穿过延伸尾部的纵向轴线。该旋翼飞行器还包括主旋翼组件，该主旋翼组件包括支撑多个转子叶片的至少一个转子轮毂，该多个转子叶片被构造和布置成围绕主转子轴线旋转，至少一个电梯布置在该延伸尾部处，以及控制系统，可操作地连接到主转子组件和至少一个电梯。控制系统被配置和设置为通过选择性地调整至少一个电梯的位置来调整机身的俯仰速率和姿态中的每一个。

82. 发明公开

EP3218806A1 CENTRALIZED PROCESSING FOR AIRCRAFT OPERATIONS 审中-公开
标题翻译：航空器运行的集中处理
公开(公告)号：EP3218806A1
公开(公告)日：2017-09-20
申请号：EP15859282.4
申请日：2015-11-12
申请人： Sikorsky Aircraft Corporation
发明人： CHEREPINSKY, Igor , DELLARIPA, Daniel , THORNBERG, Christopher A. , HOWLAND, Gary
IPC分类号： G06F9/46
CPC分类号： G06F9/4881 , B64C27/06 , G05B15/02 , G06F9/4887 , G06F9/5083 , Y02D10/24
摘要： A system for centralizing computing operations for an aircraft, including a plurality of aircraft subsystems associated with the aircraft, a plurality of aircraft sensors associated with the aircraft, and a centralized processor to process the computing operations requested by each of the plurality of aircraft subsystems.
摘要翻译：一种用于集中包括与飞机相关联的多个飞机子系统的飞机的计算操作的系统，与飞机相关联的多个飞机传感器和集中处理器以处理由多个飞机子系统中的每一个请求的计算操作。

83. 发明公开

EP3218529A2 MASKING PLUG FOR COLD SPRAY REPAIR AT COUNTERBORE HOLE 审中-公开
标题翻译：用于防止冷喷涂修复反螺纹孔
公开(公告)号：EP3218529A2
公开(公告)日：2017-09-20
申请号：EP15859926.6
申请日：2015-10-28
申请人： Sikorsky Aircraft Corporation
发明人： LE DO, Young Hanh
IPC分类号： C23C4/00 , B05D1/32 , B05B15/04
CPC分类号： F16H57/032 , B05B12/26 , B05D3/12 , B23P2700/06 , B64F5/40 , C23C4/01 , C23C4/02 , C23C4/06 , C23C4/18 , C23C24/04 , F16H2057/02043
摘要： A method of improving a structure of a component adjacent a feature is provided including removing a portion of the structure including at least one area where damage of corrosion has occurred or is likely to occur to expose a surface of the structure. A masking plug is installed into the feature such that a base of the masking plug is coupled to a first portion of the feature and a head of the masking plug is arranged adjacent a second portion of the feature. A structural deposit is formed on the surface and is integral with the structure. Excess material of the structural deposit and a portion of the head of the masking plug is removed. The second portion of the feature is reformed and the masking plug is removed from the feature.
摘要翻译：提供了一种改善与特征相邻的部件的结构的方法，包括去除包括至少一个已发生或可能发生腐蚀损坏的区域的结构的一部分以暴露结构的表面。遮蔽插头安装到特征中，使得遮蔽插头的基部联接到特征的第一部分并且遮蔽插头的头部布置在特征的第二部分附近。结构沉积物形成在表面上并与结构成一体。去除结构沉积物的过量材料和掩蔽塞的一部分头部。该功能的第二部分进行了重新组装，并将遮罩插头从该功能中移除。

84. 发明公开

EP3208023A1 CONVEX GEAR TOOTH EDGE 有权
标题翻译：凸面齿轮齿缘
公开(公告)号：EP3208023A1
公开(公告)日：2017-08-23
申请号：EP17154189.9
申请日：2017-02-01
申请人： Sikorsky Aircraft Corporation
发明人： Bittner, Edward H. , Hansen, Bruce D. , Mussel, Christopher John
IPC分类号： B23F19/12 , B23F1/02 , B23F5/02 , B23F9/02
CPC分类号： B23F19/12 , B23F1/02 , B23F5/02 , B23F9/02 , B23H5/08 , B23H9/003 , F16H1/08 , F16H55/0873 , F16H2055/0866
摘要： A method of manufacturing a gear (100) is provided. The method includes forming a plurality of gear teeth (108) in a surface of a gear, the gear teeth having tooth faces (110) defining tooth edges including tooth edge flanks (314) and tooth edge top land (316) and generating a convex contour at an edge break (318) of at least one of the tooth edge flanks and tooth edge top land.
摘要翻译：提供了一种制造齿轮（100）的方法。该方法包括在齿轮的表面中形成多个齿轮齿（108），所述齿轮齿具有限定包括齿边缘侧翼（314）和齿边缘顶部凸肩（316）的齿边缘的齿面（110）并且产生凸面轮廓在齿边缘侧面和齿边缘顶部平面中的至少一个的边缘断裂（318）处。

85. 发明公开

EP3207391A1 MAGNETIC IDENTIFICATION ASSEMBLY AND METHOD OF IDENTIFYING A COMPONENT 有权
标题翻译：磁性识别组件和识别组件的方法
公开(公告)号：EP3207391A1
公开(公告)日：2017-08-23
申请号：EP15850717.8
申请日：2015-10-16
申请人： Sikorsky Aircraft Corporation
发明人： MANTESE, Joseph V. , SOLDNER, Nicholas Charles , KLECKA, Michael A. , VIENS, Daniel V.
IPC分类号： G01R33/12 , G01R33/02 , G06K7/08
CPC分类号： G06K7/08 , G01R33/0094 , G01R33/02 , G01R33/10 , G01R33/12 , G01R33/1276 , G06K19/06187
摘要： An embedded magnetic identification assembly includes a base component formed of a material. Also included is a plurality of elements formed in an array at a surface of the base component, wherein the plurality of elements is formed of a magnetic material.
摘要翻译：嵌入式磁性识别组件包括由材料形成的基座部件。还包括在基部部件的表面处以阵列形成的多个元件，其中多个元件由磁性材料形成。

86. 发明公开

EP3201085A1 DUAL ROTOR, ROTARY WING AIRCRAFT 有权
标题翻译：双转子，旋翼飞机
公开(公告)号：EP3201085A1
公开(公告)日：2017-08-09
申请号：EP15846784.5
申请日：2015-09-25
申请人： Sikorsky Aircraft Corporation
发明人： ELLER, Erez , LUSZCZ, Matthew T. , EADIE, William J. , WEINER, Steven D.
IPC分类号： B64C27/22
CPC分类号： F16F15/02 , B64C13/04 , B64C13/50 , B64C27/001 , B64C27/006 , B64C27/10 , B64C27/14 , B64C27/467 , B64C27/57 , B64C2027/004 , B64C2027/8236 , B64D35/06 , G05D1/0816 , G05D1/0858
摘要： An aircraft includes an airframe having an empennage, a counter rotating, coaxial main rotor assembly located at the airframe including an upper rotor assembly and a lower rotor assembly, and a translational thrust system positioned at the empennage and providing translational thrust to the airframe. At least two control surfaces located at the empennage are independently operable via commands from one or more flight control computers. A method of operating an aircraft includes transmitting a first signal from one or more flight control computers to a first control surface located at a first lateral side of a translational thrust system, and actuating the first control surface to a first position via the first signal. A second signal is transmitted to a second control surface located at a second lateral side opposite the first lateral side, and the second control surface is actuated to a second position via the second signal.
摘要翻译：提供了一种包括机身，延伸尾部和反向旋转同轴主转子组件的飞机，该同轴主旋翼组件包括具有上部叶片的上部转子组件和具有下部叶片的下部转子组件。上叶片和下叶片中的一个中的第一天线以及上叶片和下叶片中的另一个中的第二天线。将激励信号施加到第一天线的振荡器。一种叶片接近监测器，用于监测激励信号的大小和来自第二天线的输出信号，以确定上叶片和下叶片之间的距离。

87. 发明公开

EP3201083A1 ROTORCRAFT FOOTPRINT 审中-实审
公开(公告)号：EP3201083A1
公开(公告)日：2017-08-09
申请号：EP15846761.3
申请日：2015-07-14
申请人： Sikorsky Aircraft Corporation
发明人： ALBER, Mark R. , EADIE, William J.
IPC分类号： B64C27/10
CPC分类号： B64C27/82 , B64C1/0009 , B64C7/00 , B64C13/04 , B64C13/18 , B64C13/50 , B64C13/503 , B64C19/00 , B64C27/001 , B64C27/006 , B64C27/008 , B64C27/08 , B64C27/10 , B64C27/12 , B64C27/14 , B64C27/16 , B64C27/32 , B64C27/322 , B64C27/33 , B64C27/467 , B64C27/473 , B64C27/48 , B64C27/51 , B64C27/52 , B64C27/54 , B64C27/57 , B64C27/78 , B64C27/80 , B64C2027/004 , B64C2027/8209 , B64C2027/8227 , B64C2027/8236 , B64C2027/8263 , B64C2027/8272 , B64C2027/8281 , B64C2201/024 , B64D35/06 , B64D39/00 , B64D39/06 , B64D45/02 , F02C9/28 , F05D2220/329 , F05D2270/021 , F16D13/52 , F16D13/72 , F16D13/74 , F16H37/02 , G05D1/0077 , G05D1/0202 , G05D1/0204 , G05D1/08 , G05D1/0816 , G05D1/0858 , G06F19/00
摘要： A method of controlling a rotary wing aircraft includes accelerating the aircraft in a fore direction independently of cyclic control of the main rotor and pitch of the aircraft.
摘要翻译：提供了一种包括机身，延伸尾部和反向旋转同轴主转子组件的飞机，该同轴主旋翼组件包括具有上部叶片的上部转子组件和具有下部叶片的下部转子组件。上叶片和下叶片中的一个中的第一天线以及上叶片和下叶片中的另一个中的第二天线。将激励信号施加到第一天线的振荡器。一种叶片接近监测器，用于监测激励信号的大小和来自第二天线的输出信号，以确定上叶片和下叶片之间的距离。

88. 发明公开

EP3201076A1 ACTIVE VIBRATION CONTROL OF A ROTORCRAFT 有权
标题翻译：旋翼机的主动振动控制
公开(公告)号：EP3201076A1
公开(公告)日：2017-08-09
申请号：EP15845825.7
申请日：2015-08-06
申请人： Sikorsky Aircraft Corporation
发明人： WELSH, William, A. , WEINER, Steven, D. , BLACKWELL, Robert, H., Jr.
IPC分类号： B64C27/00 , B64C27/08 , B64C27/10
CPC分类号： B64C27/82 , B64C1/0009 , B64C7/00 , B64C13/04 , B64C13/18 , B64C13/50 , B64C13/503 , B64C19/00 , B64C27/001 , B64C27/006 , B64C27/008 , B64C27/08 , B64C27/10 , B64C27/12 , B64C27/14 , B64C27/16 , B64C27/32 , B64C27/322 , B64C27/33 , B64C27/467 , B64C27/473 , B64C27/48 , B64C27/51 , B64C27/52 , B64C27/54 , B64C27/57 , B64C27/78 , B64C27/80 , B64C2027/004 , B64C2027/8209 , B64C2027/8227 , B64C2027/8236 , B64C2027/8263 , B64C2027/8272 , B64C2027/8281 , B64C2201/024 , B64D35/06 , B64D39/00 , B64D39/06 , B64D45/02 , F02C9/28 , F05D2220/329 , F05D2270/021 , F16D13/52 , F16D13/72 , F16D13/74 , F16H37/02 , G05D1/0077 , G05D1/0202 , G05D1/0204 , G05D1/08 , G05D1/0816 , G05D1/0858 , G06F19/00
摘要： A method of controlling a rotary wing aircraft includes accelerating the aircraft in a fore direction independently of cyclic control of the main rotor and pitch of the aircraft.
摘要翻译：提供了一种包括机身，延伸尾部和反向旋转同轴主转子组件的飞机，该同轴主旋翼组件包括具有上部叶片的上部转子组件和具有下部叶片的下部转子组件。上叶片和下叶片中的一个中的第一天线以及上叶片和下叶片中的另一个中的第二天线。将激励信号施加到第一天线的振荡器。一种叶片接近监测器，用于监测激励信号的大小和来自第二天线的输出信号，以确定上叶片和下叶片之间的距离。

89. 发明公开

EP3198349A1 HAPTIC FEEDBACK FOR REALTIME TRAJECTORY CONSTRAINTS 有权
标题翻译：实时轨迹约束的HAPTIC反馈
公开(公告)号：EP3198349A1
公开(公告)日：2017-08-02
申请号：EP15843757.4
申请日：2015-09-15
申请人： Sikorsky Aircraft Corporation
发明人： CHEREPINSKY, Igor , SANE, Harshad S.
IPC分类号： G05D1/00
摘要： A system for receiving feedback in a flight plan of a vehicle includes a haptic-enabled device comprising a crew seat with an inceptor mounted thereto; and a processor with memory having instructions stored thereon that, when executed by the processor, cause the system to: receive signals indicative of the flight plan for the vehicle; receive deviation signals indicative of a proposed deviation in a trajectory for the flight plan; and transmit signals to the haptic-enabled device representing trajectory constraints in the proposed deviation in response to the receiving of the deviation signals.
摘要翻译：一种用于在车辆的飞行计划中接收反馈的系统包括：触觉使能设备，其包括安装有感应器的乘员座椅; 以及具有存储器的处理器，所述存储器上存储有指令，所述指令在由所述处理器执行时使得所述系统：接收指示所述车辆的所述飞行计划的信号; 接收指示所述飞行计划的轨迹中的建议偏差的偏差信号; 并且响应于偏差信号的接收而将信号发送到代表所提议偏差中的轨迹约束的启用触觉的设备。

90. 发明公开

EP3197687A1 MICROCLIMATE CONTROLLED PAD FOR EFFECTIVE PAINT STRIPPING 审中-公开
标题翻译：用于有效涂漆的微孔控制垫
公开(公告)号：EP3197687A1
公开(公告)日：2017-08-02
申请号：EP15843802.8
申请日：2015-09-23
申请人： Sikorsky Aircraft Corporation
发明人： YU, Xiaomei , MAURO, Julie Anne , NTANYI, Lesly
IPC分类号： B44D3/16 , C09D9/04 , F24J1/00 , F28D20/02
CPC分类号： B44D3/16 , B44D3/166 , C09D9/04 , F24V30/00 , F28D20/02
摘要： An assembly for removing a desired portion of one or more layers of paint or another coating from a designated area is provided including a pad soaked with a chemical paint remover and an adhesive layer arranged about the pad configured to couple the assembly to the designated area. A removable first protective layer is positioned upwardly adjacent and is coupled to the adhesive layer. A flexible support layer is positioned adjacent the adhesive layer and the pad, opposite the removable first protective layer. A heat pad is arranged downwardly adjacent the flexible support layer. The heat pad is configured to control a microclimate adjacent the assembly when activated. A removable second protective layer is coupled to a surface of the heat pad. Removal of the second protective layer activates the heat pad.
摘要翻译：提供了用于从指定区域去除一层或多层涂料或另一涂层的期望部分的组件，包括用化学除漆剂浸湿的垫和布置在垫周围的粘合层，所述粘合层被配置为将组件连接到指定区域。可移除的第一保护层位于上方并与粘合层相连。与可移除的第一保护层相对，柔性支撑层邻近粘合剂层和垫设置。热垫与柔性支撑层相邻地向下布置。加热垫被配置为在激活时控制组件附近的微气候。可移除的第二保护层耦合到热垫的表面。去除第二保护层激活热垫。

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