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1.发明授权Projectile and associated method for seeking a target identified by laser designation 有权用于寻找通过激光识别识别的目标的弹丸和相关方法公开(公告)号：US08829401B1
公开(公告)日：2014-09-09
申请号：US13162167
申请日：2011-06-16
申请人： Kevin Lutke , Aaron J. Kutzmann
发明人： Kevin Lutke , Aaron J. Kutzmann
摘要： A projectile and associated method are provided for seeking a target that has been laser designated even though the projectile does not include a laser receiver. A projectile includes an aerodynamic body and a GPS receiver configured to receive GPS signals indicative of a location of the aerodynamic body. The projectile also includes a radio receiver configured to receive radio signals from an offboard laser receiver that provide information relating to a location of the target based upon laser designation of the target. Further, the projectile includes a processor configured to direct flight of the aerodynamic body toward the target based upon the location of the aerodynamic body as determined from the GPS signals and the location of the target based upon the information provided by the offboard laser receiver.
摘要翻译： 提供射弹和相关方法用于寻求已经被激光指定的目标，即使射弹不包括激光接收器。 射弹包括空气动力体和GPS接收器，其被配置为接收指示空气动力体的位置的GPS信号。 射弹还包括无线电接收器，其被配置为从外部激光接收机接收无线电信号，所述无线电信号基于目标的激光指定来提供与目标的位置有关的信息。 此外，射弹包括处理器，其被配置为基于根据由GPS信号确定的空气动力学体的位置和基于由外侧激光接收器提供的信息的目标的位置来引导空气动力学体向目标的飞行。
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2.发明授权Aircraft configuration utilizing fuselage, wing, empennage, and exhaust flow control devices 有权飞机配置采用机身，机翼，尾翼和排气流量控制装置公开(公告)号：US08061655B1
公开(公告)日：2011-11-22
申请号：US12410813
申请日：2009-03-25
申请人： David J. Manley , Aaron J. Kutzmann , Robb Gregg, III , John C. Vassberg , Antonio B. Gonzales , Steve Hollowell , Neal Harrison , Edward Lawson , Max Kismarton , Kevin Lutke
发明人： David J. Manley , Aaron J. Kutzmann , Robb Gregg, III , John C. Vassberg , Antonio B. Gonzales , Steve Hollowell , Neal Harrison , Edward Lawson , Max Kismarton , Kevin Lutke
IPC分类号： B64C1/00
摘要： Apparatus and methods provide for an aircraft configuration that utilize structural and engine exhaust flow control devices to enhance performance. Aspects of the disclosure provide a fuselage with a pressure vessel nested within a non-cylindrical outer mold line fairing. A twin-boom empennage may be connected to the fuselage. A wing may attach in a blended wing configuration with a sweep angle that positions the aircraft center of lift to minimize any pitching moment induced by the activation or deactivation of an upper surface blown (USB) system. The USB system may include a conformal USB flap positioned downstream of an engine exhaust plume, as well as a controllable USB nozzle aperture to promote exhaust flow attachment to the conformal USB flap. A universal convergent nozzle may be utilized to connect each controllable USB nozzle aperture to a corresponding internally mounted aircraft engine.
摘要翻译： 装置和方法提供了利用结构和发动机排气流量控制装置来增强性能的飞行器配置。 本公开的方面提供了一种具有嵌套在非圆柱形外模线整流罩内的压力容器的机身。 机身可能连接双桅杆尾翼。 翼可以以具有扫掠角的混合翼构型附接，该倾斜角定位飞行器的升降机中心，以最小化由上表面吹（USB）系统的激活或停用引起的任何俯仰时刻。 USB系统可以包括位于发动机排气羽流下游的共形USB挡板以及可控制的USB喷嘴孔，以促进附着到保形USB挡板的排气流。 可以使用通用会聚喷嘴将每个可控USB喷嘴孔连接到相应的内部安装的飞机发动机。
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公开(公告)号：US08322655B1
公开(公告)日：2012-12-04
申请号：US12410865
申请日：2009-03-25
申请人： Max Kismarton , Aaron J. Kutzmann , Kevin Lutke
发明人： Max Kismarton , Aaron J. Kutzmann , Kevin Lutke
IPC分类号： B64C1/00
CPC分类号： B64C5/02
摘要： Apparatus and methods provide for an aircraft empennage that utilizes two torque tube members to create opposing sides of the empennage. The torque tube members are connected using a bridging member that is attached at opposing ends to the top portions of the torque tube members. The torque tube members and bridging member provide structural support for access cut-outs within the aircraft skin between the torque tube members for access to a payload space within. The torque tube members may include any number of walls, any of which may provide a pressure barrier to the payload space.
摘要翻译： 装置和方法为飞行器尾翼提供了利用两个扭矩管构件来产生尾翼的相对侧面的装置和方法。 扭矩管构件使用在相对端附接到扭矩管构件的顶部的桥接构件连接。 扭矩管构件和桥接构件提供用于在扭矩管构件之间的用于进入有效载荷空间的飞行器皮肤内的通路切口的结构支撑。 扭矩管构件可以包括任何数量的壁，其中任何一个可以为有效负载空间提供压力屏障。
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公开(公告)号：US08353478B1
公开(公告)日：2013-01-15
申请号：US12410880
申请日：2009-03-25
申请人： Max Kismarton , Aaron J. Kutzmann , Kevin Lutke
发明人： Max Kismarton , Aaron J. Kutzmann , Kevin Lutke
IPC分类号： B64C1/00
摘要： Apparatus and methods provide for a blended wing passenger or cargo aircraft. Aspects of the disclosure provide an aircraft having wings with spars having a thickness at the wing root corresponding to a height of the payload space within the fuselage to which the wings are attached. The wing spars within the wings on each side of the aircraft may each be spliced into an aircraft frame that is part of the fuselage. The wing thickness provides mounting locations for aircraft engines and other components within the wing and passing through the wing spars. With this mid-wing configuration, the fuselage provides support for the various loads experienced by the wings without the use of a conventional structural wing box.
摘要翻译： 装置和方法为混合翼乘客或货机提供。 本公开的方面提供具有翼片的飞行器的飞行器，翼梁具有在机翼底部的厚度，其对应于机翼附接到的机身中的有效载荷空间的高度。 飞机每侧的机翼中的翼翼可以拼接成机身的一部分的飞机框架。 机翼厚度为机翼内的飞机发动机和其他部件提供安装位置，并穿过机翼翼梁。 凭借这种中翼配置，机身为不需要常规结构机翼的机翼的各种负载提供支持。
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公开(公告)号：US08302908B1
公开(公告)日：2012-11-06
申请号：US13428095
申请日：2012-03-23
申请人： Max Kismarton , Aaron J. Kutzmann , Kevin Lutke
发明人： Max Kismarton , Aaron J. Kutzmann , Kevin Lutke
IPC分类号： B64C1/00
摘要： Apparatus and methods provide for a blended wing passenger or cargo aircraft. Aspects of the disclosure provide an aircraft having wings with spars having a thickness at the wing root corresponding to a height of the payload space within the fuselage to which the wings are attached. The wing spars within the wings on each side of the aircraft may each be spliced into an aircraft frame that is part of the fuselage. The wing thickness provides mounting locations for aircraft engines and other components within the wing and passing through the wing spars. With this mid-wing configuration, the fuselage provides support for the various loads experienced by the wings without the use of a conventional structural wing box.
摘要翻译： 装置和方法为混合翼乘客或货机提供。 本公开的方面提供具有翼片的飞行器的飞行器，翼梁具有在机翼底部的厚度，其对应于机翼附接到的机身中的有效载荷空间的高度。 飞机每侧的机翼中的翼翼可以拼接成机身的一部分的飞机框架。 机翼厚度为机翼内的飞机发动机和其他部件提供安装位置，并穿过机翼翼梁。 凭借这种中翼配置，机身为不需要常规结构机翼的机翼的各种负载提供支持。
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公开(公告)号：US08226035B1
公开(公告)日：2012-07-24
申请号：US12410880
申请日：2009-03-25
申请人： Max Kismarton , Aaron J. Kutzmann , Kevin Lutke
发明人： Max Kismarton , Aaron J. Kutzmann , Kevin Lutke
IPC分类号： B64C1/00
摘要： Apparatus and methods provide for a blended wing passenger or cargo aircraft. Aspects of the disclosure provide an aircraft having wings with spars having a thickness at the wing root corresponding to a height of the payload space within the fuselage to which the wings are attached. The wing spars within the wings on each side of the aircraft may each be spliced into an aircraft frame that is part of the fuselage. The wing thickness provides mounting locations for aircraft engines and other components within the wing and passing through the wing spars. With this mid-wing configuration, the fuselage provides support for the various loads experienced by the wings without the use of a conventional structural wing box.
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