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公开(公告)号：US08302903B2
公开(公告)日：2012-11-06
申请号：US13324713
申请日：2011-12-13
IPC分类号： B64C5/10
摘要： Control surfaces in an aircraft attitude control configuration provide attitude control for an aircraft at hover or low air speed conditions. The aircraft attitude control configuration includes thrusters mounted to an aircraft, a first control surface kinematically coupled to the aircraft downstream of a first thruster to enable a first vector force to be generated by a portion of thrusted air from the first thruster on the first control surface, and a second control surface kinematically coupled to the aircraft of a second thruster. The control surfaces are displaced symmetrically a longitudinal axis of the aircraft. The control surfaces are independently and differentially movable with respect to each other to enable generation of a second vector force by a portion of thrusted air from the second thruster on the second control surface.
摘要翻译： 飞机姿态控制配置中的控制面在悬停或低空速条件下为飞机提供姿态控制。 飞行器姿态控制结构包括安装在飞行器上的推进器，第一控制表面，其运动学耦合到第一推进器下游的飞行器，以使第一矢量力能够由第一推进器在第一控制表面上的一部分推动空气产生 以及与第二推进器的飞行器运动耦合的第二控制表面。 控制表面对称地移动飞行器的纵向轴线。 控制表面可相对于彼此独立且可差分地移动，从而能够通过来自第二控制表面上的第二推进器的推动空气的一部分产生第二向量力。
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公开(公告)号：US20120145834A1
公开(公告)日：2012-06-14
申请号：US13324713
申请日：2011-12-13
摘要： Control surfaces in an aircraft attitude control configuration provide attitude control for an aircraft at hover or low air speed conditions. The aircraft attitude control configuration includes thrusters mounted to an aircraft, a first control surface kinematically coupled to the aircraft downstream of a first thruster to enable a first vector force to be generated by a portion of thrusted air from the first thruster on the first control surface, and a second control surface kinematically coupled to the aircraft of a second thruster. The control surfaces are displaced symmetrically a longitudinal axis of the aircraft. The control surfaces are independently and differentially movable with respect to each other to enable generation of a second vector force by a portion of thrusted air from the second thruster on the second control surface.
摘要翻译： 飞机姿态控制配置中的控制面在悬停或低空速条件下为飞机提供姿态控制。 飞行器姿态控制结构包括安装在飞行器上的推进器，第一控制表面，其运动学耦合到第一推进器下游的飞行器，以使第一矢量力能够由第一推进器在第一控制表面上的一部分推动空气产生 以及与第二推进器的飞行器运动耦合的第二控制表面。 控制表面对称地移动飞行器的纵向轴线。 控制表面可相对于彼此独立且可差分地移动，从而能够通过来自第二控制表面上的第二推进器的推动空气的一部分产生第二向量力。
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公开(公告)号：US08074925B2
公开(公告)日：2011-12-13
申请号：US12507573
申请日：2009-07-22
IPC分类号： B64C5/10
摘要： An aircraft attitude control configuration enables control surfaces to provide attitude control for an aircraft at hover or low air speed conditions. The aircraft attitude control configuration includes a plurality of thrusters mounted to an aircraft for thrusting air, a first control surface kinematically coupled to the aircraft at a position downstream of a first thruster to enable a first vector force to be generated by a portion of the thrusted air from the first thruster on the first control surface, and a second control surface kinematically coupled to the aircraft at a position downstream of a second thruster, the first and the second control surfaces being displaced symmetrically on opposite sides of a longitudinal axis of the aircraft, the second control surface being configured to be independently and differentially movable with respect to the first control surface to enable a second vector force to be generated by a portion of the thrusted air from the second thruster on the second control surface.
摘要翻译： 飞机姿态控制配置使得控制面能够在悬停或低空气速度条件下为飞行器提供姿态控制。 飞行器姿态控制结构包括安装在飞行器上用于推动空气的多个推进器，第一控制表面，其在第一推进器下游的位置处运动学地联接到飞行器，以使第一矢量力由推动的一部分产生 来自第一控制表面上的第一推进器的空气和在第二推进器下游的位置处运动学地联接到飞行器的第二控制表面，第一和第二控制表面在飞行器的纵向轴线的相对侧对称移位 所述第二控制表面被配置为相对于所述第一控制表面独立且可差分移动，以使第二向量力由所述第二控制表面上的来自所述第二推进器的被推动空气的一部分产生。
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公开(公告)号：US07581696B2
公开(公告)日：2009-09-01
申请号：US11595525
申请日：2006-11-09
IPC分类号： B64C5/10
摘要： An aircraft attitude control configuration enables control surfaces to provide attitude control for an aircraft at hover or low air speed conditions. The aircraft attitude control configuration includes a thruster mounted to an aircraft for thrusting air, a first control surface kinematically coupled to the aircraft at a position downstream of the thruster, and a second control surface kinematically coupled to the aircraft at a position downstream of the thruster, the second control surface being differentially movable with respect to the first control surface such that a portion of the thrusted air from the thruster generates a first vector force on the first control surface and another portion of the thrusted air generates a second vector force on the second control surface, so that the first and the second vector forces provide a net roll moment about the Y-Roll axis.
摘要翻译： 飞机姿态控制配置使得控制面能够在悬停或低空气速度条件下为飞行器提供姿态控制。 飞行器姿态控制构型包括安装在飞行器上用于推动空气的推进器，在推进器下游的位置运动地联接到飞行器的第一控制表面，以及在推进器下游的位置运动地联接到飞行器的第二控制表面 所述第二控制表面可相对于所述第一控制表面差异移动，使得来自所述推进器的所述推动空气的一部分在所述第一控制表面上产生第一向量力，并且所述推动空气的另一部分在所述第二控制表面上产生第二向量力 第二控制表面，使得第一和第二向量力围绕Y-辊轴提供净滚动力矩。
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公开(公告)号：US20090283632A1
公开(公告)日：2009-11-19
申请号：US12507573
申请日：2009-07-22
IPC分类号： B64C9/00
摘要： An aircraft attitude control configuration enables control surfaces to provide attitude control for an aircraft at hover or low air speed conditions. The aircraft attitude control configuration includes a plurality of thrusters mounted to an aircraft for thrusting air, a first control surface kinematically coupled to the aircraft at a position downstream of a first thruster to enable a first vector force to be generated by a portion of the thrusted air from the first thruster on the first control surface, and a second control surface kinematically coupled to the aircraft at a position downstream of a second thruster, the first and the second control surfaces being displaced symmetrically on opposite sides of a longitudinal axis of the aircraft, the second control surface being configured to be independently and differentially movable with respect to the first control surface to enable a second vector force to be generated by a portion of the thrusted air from the second thruster on the second control surface.
摘要翻译： 飞机姿态控制配置使得控制面能够在悬停或低空气速度条件下为飞行器提供姿态控制。 飞行器姿态控制结构包括安装在飞行器上用于推动空气的多个推进器，第一控制表面，其在第一推进器下游的位置处运动学地联接到飞行器，以使第一矢量力由推动的一部分产生 来自第一控制表面上的第一推进器的空气和在第二推进器下游的位置处运动学地联接到飞行器的第二控制表面，第一和第二控制表面在飞行器的纵向轴线的相对侧对称移位 所述第二控制表面被配置为相对于所述第一控制表面独立且可差分移动，以使第二向量力由所述第二控制表面上的来自所述第二推进器的被推动空气的一部分产生。
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