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1. 发明申请

US20110303783A1 Stabilizer 有权
标题翻译：稳定剂
公开(公告)号：US20110303783A1
公开(公告)日：2011-12-15
申请号：US13150790
申请日：2011-06-01
申请人： Hanno Brenner , Christoph Kessler , Wolfgang Kreitmair-Steck
发明人： Hanno Brenner , Christoph Kessler , Wolfgang Kreitmair-Steck
IPC分类号： G05D1/02 , B64C27/00 , G05D1/10
CPC分类号： B64D1/22 , B64C27/04
摘要： The invention relates to a stabilizer for rotary wing aircraft 11 which carry a hanging sling load 12 in the direction of the ground on at least one support cable 13, and were the stabilizer is set up to generate control signals R to be applied or modulated onto the flight control of the rotorcraft 11 and set up with at least one sling load pendulum motion detecting unit 2 for detecting the pendulum motion 15, 21, 41 of the sling load 12. Additionally, the stabilizer is set up with a working range determination unit S3 for determining the space where free movement is possible in which a rotorcraft 11 with sling load 12 can move without collision and the stabilizer is set up to generate the control signals R in dependency of the determined pendulum motion 15, 31, 41 of the sling load 12 and in dependency of the of the determined working range.
摘要翻译：本发明涉及一种用于旋转飞行器11的稳定器，其在至少一个支撑缆索13上沿地面方向承载悬挂吊索12，并且设置稳定器以产生要施加或调制到旋翼航空器11的飞行控制，并设置有至少一个吊索载荷摆动检测单元2，用于检测吊索载荷12的摆动运动15,21,41。另外，稳定器设置有工作范围确定单元 S3，用于确定具有悬挂负载12的旋翼航空器11可以在没有碰撞的情况下可自由运动的空间，并且稳定器被设置为根据确定的吊架运动15,31,41产生控制信号R. 负载12并依赖于确定的工作范围。

2. 发明授权

US08622336B2 Stabilizer 有权
标题翻译：稳定剂
公开(公告)号：US08622336B2
公开(公告)日：2014-01-07
申请号：US13150790
申请日：2011-06-01
申请人： Hanno Brenner , Christoph Kessler , Wolfgang Kreitmair-Steck
发明人： Hanno Brenner , Christoph Kessler , Wolfgang Kreitmair-Steck
IPC分类号： B64C11/00
CPC分类号： B64D1/22 , B64C27/04
摘要： A rotary aircraft which carries a hanging sling load on at least one support cable, benefits from a stabilizer which generates control signals R to be applied or modulated onto the flight control of the aircraft. At least one sling load pendulum motion detecting unit provides the stabilizer with data on the pendulum motion of the sling load. Additionally, the stabilizer is set up with a working range determination unit S3 for determining the space where free movement is possible in which the rotary aircraft with sling load can move without collision. The stabilizer generates control signals R in dependency of the determined pendulum motion of the sling load and the determined working range.
摘要翻译：在至少一个支撑电缆上承载吊吊负载的旋转飞机受益于产生要应用或调制到飞行器的飞行控制上的控制信号R的稳定器。至少一个吊装载荷摆动运动检测单元为吊具提供有关吊索载荷的摆动运动的数据。此外，稳定器设置有工作范围确定单元S3，用于确定具有悬挂载荷的旋转飞行器可以在没有碰撞的情况下移动的空间。稳定器根据确定的吊架载荷的摆动和所确定的作业范围产生控制信号R.

3. 发明授权

US08694180B2 Method and system for an optimized utilization of energy resources of an electrical system 有权
标题翻译：优化利用电力系统能源资源的方法和系统
公开(公告)号：US08694180B2
公开(公告)日：2014-04-08
申请号：US13012905
申请日：2011-01-25
申请人： Matthias Glassl , Wolfgang Kreitmair-Steck , Mustapha Ennaji , Thorsten Koenemann
发明人： Matthias Glassl , Wolfgang Kreitmair-Steck , Mustapha Ennaji , Thorsten Koenemann
IPC分类号： G06F7/00 , G06F17/00
CPC分类号： G05B9/02 , B60R25/00 , B64D2221/00 , H02J7/1461 , Y02T10/7005
摘要： A method for optimized utilization of available energy resources/sources (3) of an electrical system such as for a vehicle generator system. The steps include: determining performance parameters LIst (e.g. current I, voltage U, temperature T, power PD (Pverlust), PE (Pwirk), efficiency, etc.) of a preferred energy resource (3); entering performance parameters LIst (current I, voltage U, temperature T, altitude of the vehicle, etc.) of the energy resource (3) into a thermal model (7); comparing a performance parameter LIst of the energy resource (3) with a specified performance limit parameter LSoll at a specified threshold level; determining a value for an energy reservoir ERest of a preferred energy resource (3); and to calculate a remaining time TMax depending on the energy reservoir ERest of a preferred energy resource (3) and using the one or more identified performance parameters LIst to maintain an operational state of the vehicle.
摘要翻译：一种用于优化利用诸如用于车辆发电机系统的电气系统的可用能源/源（3）的方法。步骤包括：确定优选能量资源（3）的性能参数LIst（例如电流I，电压U，温度T，功率PD（Pverlust），PE（Pwirk），效率等）; 将能量（3）的性能参数LIst（电流I，电压U，温度T，车辆高度等）输入热模型（7）; 将能量资源（3）的性能参数LIst与规定的阈值水平的指定性能极限参数LSoll进行比较; 确定优选能量资源（3）的能量储存器ERest的值; 并且根据优选能量资源（3）的能量储存器ERest计算剩余时间TMax，并且使用所述一个或多个识别的性能参数LIst来维持车辆的操作状态。

4. 发明申请

US20110199661A1 COCKPIT FOR AN AIRCRAFT 审中-公开
标题翻译：空中客车
公开(公告)号：US20110199661A1
公开(公告)日：2011-08-18
申请号：US13023758
申请日：2011-02-09
申请人： Wolfgang Kreitmair-Steck , Stefan Haisch
发明人： Wolfgang Kreitmair-Steck , Stefan Haisch
IPC分类号： G02B27/01 , G02F1/01 , G03H1/00
CPC分类号： B64D43/00 , G02B27/01 , G02B27/0103 , G02B2027/0118 , G02B2027/0187
摘要： The invention relates to a cockpit for an aircraft, particularly for a helicopter, with transparent extensions (2, 3) to a dashboard (7) for displaying various control information for flight operation. The transparency of the extensions (2, 3) of the dashboard (7) is automatically or via pilot commands changeable depending on flight operations and environmental needs.
摘要翻译：本发明涉及一种用于飞机，特别是用于直升机的驾驶舱，其具有用于显示用于飞行操作的各种控制信息的仪表板（7）的透明延伸部（2,3）。仪表板（7）的扩展（2,3）的透明度是自动的，也可以通过根据飞行操作和环境需求而改变的导频命令。

5. 发明申请

US20110190963A1 METHOD AND SYSTEM FOR AN OPTIMIZED UTILIZATION OF ENERGY RESOURCES OF AN ELECTRICAL SYSTEM 有权
标题翻译：用于电力系统能源资源优化利用的方法和系统
公开(公告)号：US20110190963A1
公开(公告)日：2011-08-04
申请号：US13012905
申请日：2011-01-25
申请人： Matthias Glassl , Wolfgang Kreitmair-Steck , Mustapha Ennaji , Thorsten Koenemann
发明人： Matthias Glassl , Wolfgang Kreitmair-Steck , Mustapha Ennaji , Thorsten Koenemann
IPC分类号： G05D1/00
CPC分类号： G05B9/02 , B60R25/00 , B64D2221/00 , H02J7/1461 , Y02T10/7005
摘要： A method for optimized utilization of available energy resources/sources (3) of an electrical system such as for a vehicle generator system. The steps include: determining performance parameters LIst (e.g. current I, voltage U, temperature T, power PD (Pverlust), PE (Pwirk), efficiency, etc.) of a preferred energy resource (3); entering performance parameters LIst (current I, voltage U, temperature T, altitude of the vehicle, etc.) of the energy resource (3) into a thermal model (7); comparing a performance parameter LIst of the energy resource (3) with a specified performance limit parameter LSoll at a specified threshold level; determining a value for an energy reservoir ERest of a preferred energy resource (3); and to calculate a remaining time TMax depending on the energy reservoir ERest of a preferred energy resource (3) and using the one or more identified performance parameters LIst to maintain an operational state of the vehicle.
摘要翻译：一种用于优化利用诸如用于车辆发电机系统的电气系统的可用能源/源（3）的方法。步骤包括：确定优选能量资源（3）的性能参数LIst（例如电流I，电压U，温度T，功率PD（Pverlust），PE（Pwirk），效率等）; 将能量（3）的性能参数LIst（电流I，电压U，温度T，车辆高度等）输入热模型（7）; 将能量资源（3）的性能参数LIst与规定的阈值水平的指定性能极限参数LSoll进行比较; 确定优选能量资源（3）的能量储存器ERest的值; 并且根据优选能量资源（3）的能量储存器ERest计算剩余时间TMax，并且使用所述一个或多个识别的性能参数LIst来维持车辆的操作状态。

6. 发明申请

US20110208373A1 SYSTEM FOR CONTROL OF UNMANNED AERIAL VEHICLES 审中-公开
标题翻译：无人驾驶飞机的控制系统
公开(公告)号：US20110208373A1
公开(公告)日：2011-08-25
申请号：US13031823
申请日：2011-02-22
申请人： Thilo Lees , Florian Regenfelder , Dominik Vogel , Sandra Lorenz , Wolfgang Kreitmair-Steck , Stefan Haisch
发明人： Thilo Lees , Florian Regenfelder , Dominik Vogel , Sandra Lorenz , Wolfgang Kreitmair-Steck , Stefan Haisch
IPC分类号： G05D1/00
摘要： A system (1) for the control of at least one unmanned aerial vehicle (2) from at least one aircraft (3), preferably a helicopter. The system (1) comprises at least one computer system (4), at least one satellite communication system (5) online with a satellite (6) and at least one radio set (7) for bidirectional data transfer between the aircraft (3) and the at least one unmanned aerial vehicle (2).
摘要翻译：一种用于从至少一架飞机（3），优选直升机控制至少一个无人机（2）的系统（1）。系统（1）包括至少一个计算机系统（4），至少一个与卫星（6）在线的卫星通信系统（5）和用于飞行器（3）之间的双向数据传输的至少一个无线电设备（7）和所述至少一个无人驾驶飞行器（2）。

7. 发明授权

US08654001B2 Wide-band HIRF detector- and analysis system for aircraft 有权
标题翻译：用于飞机的宽带HIRF探测器和分析系统
公开(公告)号：US08654001B2
公开(公告)日：2014-02-18
申请号：US13201653
申请日：2010-02-04
申请人： Wolfgang Tauber , Wolfgang Kreitmair-Steck , Bernd Wolff
发明人： Wolfgang Tauber , Wolfgang Kreitmair-Steck , Bernd Wolff
IPC分类号： G01S7/40
CPC分类号： G01S7/36 , G01R29/0892 , G01R31/008
摘要： A method for detecting electromagnetic threats to an aircraft, wherein electromagnetic fields are measured, and in the case of an arising threat to the aircraft being detected, countermeasures are taken, characterized by the following steps: measuring the frequency and the amplitude of at least one electromagnetic field in the frequency range from 9 KHz to 40 GHz; analyzing the measured results and determining the field intensity in relation to each measured frequency; comparing the field intensity in relation to each measured frequency with stored limiting values or qualification values, wherein the aircraft is qualified for field intensities that are lower than the limiting values; and providing the result in the form of a warning signal in the case of approaching or exceeding a limiting value.
摘要翻译：一种用于检测对飞机的电磁威胁的方法，其中测量电磁场，并且在对被检测的飞行器产生威胁的情况下，采取对策，其特征在于以下步骤：测量至少一个频率范围为9KHz至40GHz的电磁场; 分析测量结果并确定与每个测量频率有关的场强; 将与每个测量频率相关的场强与存储的限制值或限定值相比较，其中飞行器对于低于限制值的场强进行限定; 并且在接近或超过限制值的情况下以警告信号的形式提供结果。

8. 发明申请

US20120032832A1 WIDE-BAND HIRF DETECTOR- AND ANALYSIS SYSTEM FOR AIRCRAFT 有权
标题翻译：用于飞机的宽带探测器和分析系统
公开(公告)号：US20120032832A1
公开(公告)日：2012-02-09
申请号：US13201653
申请日：2010-02-04
申请人： Wolfgang Tauber , Wolfgang Kreitmair-Steck , Bernd Wolff
发明人： Wolfgang Tauber , Wolfgang Kreitmair-Steck , Bernd Wolff
IPC分类号： G01S7/38
CPC分类号： G01S7/36 , G01R29/0892 , G01R31/008
摘要： A method for detecting electromagnetic threats to an aircraft, wherein electromagnetic fields are measured, and in the case of an arising threat to the aircraft being detected, countermeasures are taken, characterized by the following steps: measuring the frequency and the amplitude of at least one electromagnetic field in the frequency range from 9 KHz to 40 GHz; analysing the measured results and determining the field intensity in relation to each measured frequency; comparing the field intensity in relation to each measured frequency with stored limiting values or qualification values, wherein the aircraft is qualified for field intensities that are lower than the limiting values; and providing the result in the form of a warning signal in the case of approaching or exceeding a limiting value.
摘要翻译：一种用于检测对飞机的电磁威胁的方法，其中测量电磁场，并且在对被检测的飞行器产生威胁的情况下，采取对策，其特征在于以下步骤：测量至少一个频率范围为9KHz至40GHz的电磁场; 分析测量结果并确定与每个测量频率有关的场强; 将与每个测量频率相关的场强与存储的限制值或限定值相比较，其中飞行器对于低于限制值的场强进行限定; 并且在接近或超过限制值的情况下以警告信号的形式提供结果。

9. 发明授权

US5614907A All weather visual system for helicopters 失效
标题翻译：所有天气视觉系统的直升机
公开(公告)号：US5614907A
公开(公告)日：1997-03-25
申请号：US616003
申请日：1996-03-14
申请人： Wolfgang Kreitmair-Steck , Helmut Klausing
发明人： Wolfgang Kreitmair-Steck , Helmut Klausing
IPC分类号： G01C15/14 , G01S13/86 , G01S13/90 , G01S7/04
CPC分类号： G01S13/9035 , G01C15/14 , G01S13/86 , G01S2013/9082
摘要： The invention relates to an all weather visual system that combines information from a ROSAR type radar sensor with navigation and flight information to provide artificial vision for the pilot. The radar utilizes the movements of rotating arms fixedly mounted on the rotor head of a helicopter. For this purpose, a turnstile is used as the central carrier structure, which is protected by an aerodynamically shaped body against atmospheric forces. The radar transmitter and radar receiver are located on the rotor head and in the tips of the rotating arms, respectively.
摘要翻译：本发明涉及一种将来自ROSAR型雷达传感器的信息与导航和飞行信息相结合的全天候视觉系统，为飞行员提供人工视觉。雷达利用固定安装在直升机转子头上的旋转臂的运动。为此目的，使用十字转门作为中央载体结构，由空气动力学形状的体保护抵抗大气力。雷达发射器和雷达接收器分别位于转子头部和旋转臂的尖端。

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