公开(公告)号：US20100222993A1

公开(公告)日：2010-09-02

申请号：US11455482

申请日：2006-06-19

申请人： Steven J. Brainard ,  David R. Houy ,  Anthony Z. Stobiecki ,  Mark W. Scott ,  Steven D. Weiner

发明人： Steven J. Brainard ,  David R. Houy ,  Anthony Z. Stobiecki ,  Mark W. Scott ,  Steven D. Weiner

IPC分类号： G06F19/00

CPC分类号： B64D1/22 ,  G01D7/02 ,  G01M1/127 ,  G05D1/0858

摘要： An interactive aircraft load management system automates calculation and provides simulation capability to changes in an aircraft C.G. limit for display on a three-dimensional aircraft symbology. The aircraft load management system also communicates with a fly by wire (FBW) flight control system wherein the aircraft's control system is programmed to automatically compensate for C.G. excursions and to alter control laws. The aircraft load management system also selectively reels-in and reels out sling lines as the aircraft pitches and rolls to maintain a load vector from a slung load along the aircraft centerline. Load vector travel is accomplished by coupling a winch control system into the flight control system.

摘要翻译： 交互式飞机负载管理系统自动计算并提供对飞机C.G.的变化的模拟能力。 限制在三维飞机符号系统上显示。 飞机负载管理系统还与飞行（FBW）飞行控制系统进行通信，其中飞行器的控制系统被编程为自动补偿C.G. 游览和改变控制法。 航空器负载管理系统还可以选择性地卷起并卷起吊索，因为飞机的间距和滚动以沿着飞机中心线从静止载荷维持载荷矢量。 通过将绞盘控制系统连接到飞行控制系统来实现负载矢量行驶。

公开(公告)号：US07954766B2

公开(公告)日：2011-06-07

申请号：US11455482

申请日：2006-06-19

申请人： Steven J. Brainard ,  David R. Houy ,  Anthony Z. Stobiecki ,  Mark W. Scott ,  Steven D. Weiner

发明人： Steven J. Brainard ,  David R. Houy ,  Anthony Z. Stobiecki ,  Mark W. Scott ,  Steven D. Weiner

IPC分类号： B64D47/00

CPC分类号： B64D1/22 ,  G01D7/02 ,  G01M1/127 ,  G05D1/0858

摘要： An interactive aircraft load management system automates calculation and provides simulation capability to changes in an aircraft C.G. limit for display on a three-dimensional aircraft symbology. The aircraft load management system also communicates with a fly by wire (FBW) flight control system wherein the aircraft's control system is programmed to automatically compensate for C.G. excursions and to alter control laws. The aircraft load management system also selectively reels-in and reels out sling lines as the aircraft pitches and rolls to maintain a load vector from a slung load along the aircraft centerline. Load vector travel is accomplished by coupling a winch control system into the flight control system.

摘要翻译： 交互式飞机负载管理系统自动计算并提供对飞机C.G.的变化的模拟能力。 限制在三维飞机符号系统上显示。 飞机负载管理系统还与飞行（FBW）飞行控制系统进行通信，其中飞行器的控制系统被编程为自动补偿C.G. 游览和改变控制法。 航空器负载管理系统还可以选择性地卷起并卷起吊索，因为飞机的间距和滚动以沿着飞机中心线保持来自悬挂载荷的载荷矢量。 通过将绞盘控制系统连接到飞行控制系统来实现负载矢量行驶。