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1. 发明授权

US07716980B1 Pitot probe with water blockage prevention 有权
标题翻译：皮托探针防水防水
公开(公告)号：US07716980B1
公开(公告)日：2010-05-18
申请号：US12130222
申请日：2008-05-30
申请人： Todd M. Colten , Wade W. Brown , Ryan L. Nelson
发明人： Todd M. Colten , Wade W. Brown , Ryan L. Nelson
IPC分类号： G01P13/00
CPC分类号： G01P5/165
摘要： Pitot probes are described that are designed to prevent water blockage of the probe's air pressure orifice. The pitot probes are small, inexpensive, light weight and do not require power for heat generation. This makes the pitot probes particularly useful for use on UAV's and other small aircraft where size, cost, weight and power constraints are a major concern. The pitot probes utilize passive methods in the form of geometrical and material configurations to prevent blockage of the pitot probes by water droplets. The probes can also include water reservoirs that store collected water.
摘要翻译：描述了皮托探测器，其设计用于防止探头气压孔的水堵塞。皮托探头小巧，便宜，重量轻，不需要发热的电源。这使得皮托探测器对于使用无人机和其他小型飞机而言尤其有用，其尺寸，成本，重量和功率限制是主要关注的问题。皮托探测器采用几何和材料结构形式的被动方法，以防止水滴探测皮托管探测器的堵塞。探头还可以包括储存收集水的储水器。

2. 发明授权

US07699261B2 Small unmanned airborne vehicle airframe 有权
标题翻译：小型无人机载机体
公开(公告)号：US07699261B2
公开(公告)日：2010-04-20
申请号：US11714436
申请日：2007-03-05
申请人： Todd M. Colten , Scott E. Morgan , Christopher A. Launer
发明人： Todd M. Colten , Scott E. Morgan , Christopher A. Launer
IPC分类号： B64C39/00
CPC分类号： B64C39/024 , B64C2201/021 , B64C2211/00
摘要： An unmanned aerial vehicle (UAV) is designed for low-speed, low altitude, long endurance missions typical to UAVs of this size and class. The UAV structure is configured to be substantially impervious to small arms fire and to have a very small representative radar cross-section. The UAV is modular such that the main wings and tail wing assembly are quickly and easily, detached from the fuselage for ease of transport and to provide an airframe that is quickly and easily adapted to any particular mission.
摘要翻译：无人机（UAV）专为低速，低空，长寿命的任务而设计，适用于这种规模和类别的无人机。 UAV结构被配置为基本上不受小武器的威胁，并且具有非常小的代表性雷达横截面。无人机是模块化的，使得主翼和尾翼组件快速容易地从机身脱离，以便于运输，并提供快速且容易地适应于任何特定任务的机身。

3. 发明授权

US08282040B1 Composite aircraft wing 有权
标题翻译：复合飞机机翼
公开(公告)号：US08282040B1
公开(公告)日：2012-10-09
申请号：US12432901
申请日：2009-04-30
申请人： Aaron L. Westman , Todd M. Colten
发明人： Aaron L. Westman , Todd M. Colten
IPC分类号： B64C1/00
CPC分类号： B64C3/24
摘要： A composite aircraft wing that includes a core, a first composite material disposed over the upper surface of the core, and a second composite material over the lower surface of the core. The second composite material is a different composite material than the first composite material. In addition, a first wood veneer layer is disposed over the first composite material and a second wood veneer layer disposed over the second composite material. The wing is lightweight, has an airfoil shape, and is easy to construct without using molds, while also being strong enough to support the weight of the aircraft. When used on a UAV-type aircraft having a wing-mounted antenna, the wing construction has little or no RF impact on the antenna.
摘要翻译：一种复合飞机机翼，其包括芯，设置在所述芯的上表面上的第一复合材料，以及位于所述芯的下表面上的第二复合材料。第二复合材料是与第一复合材料不同的复合材料。此外，第一木材单板层设置在第一复合材料上方，第二木材单板层设置在第二复合材料上。机翼重量轻，具有翼型形状，并且易于构造而不使用模具，同时也足够坚固以支撑飞机的重量。当在具有机翼安装天线的UAV型飞机上使用时，机翼结构对天线几乎没有或没有RF冲击。

4. 发明申请

US20080217486A1 Small unmanned airborne vehicle airframe 有权
标题翻译：小型无人机载机体
公开(公告)号：US20080217486A1
公开(公告)日：2008-09-11
申请号：US11714436
申请日：2007-03-05
申请人： Todd M. Colten , Scott E. Morgan , Christopher A. Launer
发明人： Todd M. Colten , Scott E. Morgan , Christopher A. Launer
IPC分类号： B64C3/38
CPC分类号： B64C39/024 , B64C2201/021 , B64C2211/00
摘要： An unmanned aerial vehicle (UAV) is designed for low-speed, low altitude, long endurance missions typical to UAVs of this size and class. The UAV structure is configured to be substantially impervious to small arms fire and to have a very small representative radar cross-section. The UAV is modular such that the main wings and tail wing assembly are quickly and easily, detached from the fuselage for ease of transport and to provide an airframe that is quickly and easily adapted to any particular mission.
摘要翻译：无人机（UAV）专为低速，低空，长寿命的任务而设计，适用于这种规模和类别的无人机。 UAV结构被配置为基本上不受小武器的威胁，并且具有非常小的代表性雷达横截面。无人机是模块化的，使得主翼和尾翼组件快速容易地从机身脱离，以便于运输，并提供快速且容易地适应于任何特定任务的机身。

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