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1. 发明授权

US06755374B1 Anti-Torque and yaw-control system for a rotary-wing aircraft 失效
标题翻译：用于旋翼飞机的反扭矩和偏航控制系统
公开(公告)号：US06755374B1
公开(公告)日：2004-06-29
申请号：US10353162
申请日：2003-01-27
申请人： Franklin D. Carson
发明人： Franklin D. Carson
IPC分类号： B64C2782
CPC分类号： B64C27/82 , B64C2027/8245
摘要： A preferred embodiment of a rotary-wing aircraft comprises a main rotor, a tail boom extending through an area of downwash from the main rotor, and a linear nozzle fixedly coupled to the tail boom and having an opening extending along the tail boom for discharging a sheet of fluid in a direction substantially tangential to an outer surface of the tail boom. A preferred embodiment also comprises a yaw-control device movably coupled to the tail boom and having an opening formed therein for discharging fluid in a direction away from the yaw-control device and into the area of downwash from the main rotor.
摘要翻译：旋转翼飞行器的优选实施例包括主转子，延伸穿过来自主转子的下流区域的尾斗和固定地联接到尾悬臂的线性喷嘴，并且具有沿着尾臂延伸的开口，用于排出在与起重臂的外表面大致相切的方向上的流体片。优选实施例还包括一个偏转控制装置，其可动地联接到尾悬臂上，并具有形成在其中的开口，用于沿远离偏航控制装置的方向排出流体并进入从主转子进入下流区域。

2. 发明申请

US20130209601A1 PROCESSES AND SYSTEMS FOR MANUFACTURING SPARS AND OTHER HOLLOW STRUCTURES 失效
标题翻译：制造SPARS和其他中空结构的工艺和系统
公开(公告)号：US20130209601A1
公开(公告)日：2013-08-15
申请号：US13832538
申请日：2013-03-15
申请人： Franklin D. Carson
发明人： Peter G.C. Dixon
IPC分类号： B29D22/00
CPC分类号： B29D22/00 , B29C70/446 , B29C70/547 , B29L2031/082
摘要： Processes for manufacturing hollow structures such as spars for helicopter rotor blades, fixed wings for aircraft, and other aerostructures can include the provision of a path for gases to exit the material from which the spar is formed as the material is heated and cured, to help eliminate voids within the material caused by the presence of such gases.
摘要翻译：用于制造中空结构的方法，例如用于直升机转子叶片的翼梁，用于飞行器的固定翼和其它航空结构的空心结构可以包括：当材料被加热和固化时，提供用于离开形成翼梁的材料的路径，以帮助消除由这种气体的存在引起的材料内的空隙。

3. 发明授权

US07037072B2 Rotor head for a rotary-wing aircraft 失效
标题翻译：转翼头用于旋翼飞机
公开(公告)号：US07037072B2
公开(公告)日：2006-05-02
申请号：US10792189
申请日：2004-03-03
申请人： Franklin D. Carson
发明人： Franklin D. Carson
IPC分类号： B64C27/52
CPC分类号： F03B1/00 , Y02E10/223
摘要： A preferred embodiment of a rotor head for a rotary-wing aircraft having a plurality of rotor blades and a drive shaft includes a gimbal mechanically coupled to the drive shaft so that the gimbal rotates with the drive shaft, and a hub pivotally coupled to the gimbal for receiving the rotor blades. The rotor head also includes an actuator mechanically coupled to the hub for causing the hub to pivot about the gimbal.
摘要翻译：用于具有多个转子叶片和驱动轴的旋转翼飞行器的转子头的优选实施例包括机械地联接到驱动轴的万向架，使得万向架与驱动轴一起旋转，并且枢轴枢转地联接到万向节用于接收转子叶片。转子头还包括机械联接到轮毂的致动器，用于使轮毂围绕万向节枢转。

4. 发明授权

US08758006B2 Processes and systems for manufacturing spars and other hollow structures 失效
标题翻译：制造翼梁和其他中空结构的工艺和系统
公开(公告)号：US08758006B2
公开(公告)日：2014-06-24
申请号：US13832538
申请日：2013-03-15
申请人： Franklin D. Carson
发明人： Peter G. C. Dixon
IPC分类号： B28B7/32 , B28B7/30
CPC分类号： B29D22/00 , B29C70/446 , B29C70/547 , B29L2031/082
摘要： Processes for manufacturing hollow structures such as spars for helicopter rotor blades, fixed wings for aircraft, and other aerostructures can include the provision of a path for gases to exit the material from which the spar is formed as the material is heated and cured, to help eliminate voids within the material caused by the presence of such gases.
摘要翻译：用于制造中空结构的方法，例如用于直升机转子叶片的翼梁，用于飞行器的固定翼和其它航空结构的空心结构可以包括：当材料被加热和固化时，提供用于气体离开形成翼梁的材料的路径，以帮助消除由这种气体的存在引起的材料内的空隙。

5. 发明授权

US06830214B2 Rotary-wing aircraft 失效
标题翻译：旋翼飞机
公开(公告)号：US06830214B2
公开(公告)日：2004-12-14
申请号：US10194672
申请日：2002-07-12
申请人： Franklin D. Carson
发明人： Franklin D. Carson
IPC分类号： B64C2752
CPC分类号： B64C27/82 , B64C27/605 , B64C2027/8281
摘要： A preferred embodiment of a rotary-wing aircraft includes a fuselage, a tail boom fixedly coupled the fuselage, a pylon fixedly coupled to the tail boom, and a main rotor assembly rotatably coupled to the fuselage and comprising a hub and a plurality of rotor blades pivotally coupled to the hub. The preferred embodiment also includes a cyclic control adapted to vary an orientation of the rotor blades in relation to the hub on a cyclical basis, and a horizontal stabilizer mounted on one of the pylon and the tail boom. At least a portion of the horizontal stabilizer is movable in relation to the one of the pylon and the tail boom and a position of the at least a portion of the horizontal stabilizer is controllable independent of the cyclic control.
摘要翻译：旋转翼飞行器的优选实施例包括机身，固定地连接机身的尾臂，固定地连接到尾吊杆的挂架和可旋转地联接到机身的主转子组件，并且包括毂和多个转子叶片枢转地联接到轮毂。优选实施例还包括循环控制，其适于在循环的基础上改变转子叶片相对于轮毂的取向，以及安装在塔架和尾吊杆中的一个上的水平稳定器。水平稳定器的至少一部分可相对于塔架和尾梁中的一个移动，并且水平稳定器的至少一部分的位置可以独立于循环控制来控制。

6. 发明授权

US5661649A Airborne gravity and magnetic field surveying method 失效
标题翻译：机载重力和磁场测量方法
公开(公告)号：US5661649A
公开(公告)日：1997-08-26
申请号：US363970
申请日：1994-12-23
申请人： Franklin D. Carson , William R. Gumert
发明人： Franklin D. Carson , William R. Gumert
IPC分类号： G01V7/16 , G06F19/00
CPC分类号： G01V7/16
摘要： A method is disclosed for airborne gravity and magnetic field surveying, in which the airborne vehicle is stabilized with respect to speed, direction of heading, and center of gravity, and in which the gravity meter is of adequate sensitivity and provides signals that are recorded at a high sample rate on a magnetic tape, with magnetic data collected and preserved which can be used alone or as a reference for checking the accuracy of the gravity data, and with the aircraft's position computed using a satellite positioning system, or a multi-range navigation system that is geodetically located.
摘要翻译：公开了一种用于机载重力和磁场测量的方法，其中机载车辆相对于速度，航向方向和重心被稳定，并且其中重力计具有足够的灵敏度并且提供记录在在磁带上采样率高，采集和保存的磁数据可单独使用或用作检查重力数据精度的参考，以及使用卫星定位系统或多范围计算的飞机位置位于地理位置的导航系统

7. 发明授权

US4435981A Airborne gravity surveying 失效
标题翻译：机载重力测量
公开(公告)号：US4435981A
公开(公告)日：1984-03-13
申请号：US309906
申请日：1981-10-09
申请人： Franklin D. Carson , William R. Gumert
发明人： Franklin D. Carson , William R. Gumert
IPC分类号： G01V7/16
CPC分类号： G01V7/16
摘要： Method and apparatus are disclosed for airborne gravity surveying in which the airborne vehicle is stabilized with respect to speed, direction of heading and altitude, and in which the gravity meter has adequate sensitivity and signals that are recorded at a high sample rate on a magnetic tape, in which the aircraft position is computed using a multi-range navigation system that is located geodetically.
摘要翻译：公开了一种用于空中重力测量的方法和装置，其中，空中车辆相对于速度，航向方向和高度稳定，并且其中重力计具有足够的灵敏度和以高采样率记录在磁带上的信号，其中使用位于地质上的多范围导航系统来计算飞机位置。

8. 发明申请

US20160207623A1 ROTARY-WING AIRCRAFT WITH DUCTED ANTI-TORQUE DEVICE 审中-公开
标题翻译：带旋转扭矩装置的旋转式飞机
公开(公告)号：US20160207623A1
公开(公告)日：2016-07-21
申请号：US14632674
申请日：2015-02-26
申请人： Franklin D. Carson
发明人： Franklin D. Carson
IPC分类号： B64C27/82 , B64C27/46 , B64C27/04 , B64C5/16 , B64C1/26
CPC分类号： B64C27/82 , B64C1/26 , B64C5/16 , B64C27/04 , B64C27/46 , B64C2027/8254
摘要： Embodiments of rotary-wing aircraft include a fuselage, and a main rotor assembly mounted for rotation on the fuselage. The rotary-wing aircraft also have an anti-torque device. The anti-torque device has a body that is contiguous with the fuselage, and a rotor mounted within a duct defined by the body.
摘要翻译：旋转翼飞行器的实施例包括机身和安装成在机身上旋转的主转子组件。旋翼飞机还具有抗扭矩装置。抗扭矩装置具有与机身相邻的主体，以及安装在由主体限定的导管内的转子。

9. 发明授权

US06416015B1 Anti-torque and yaw-control system for a rotary-wing aircraft 有权
标题翻译：用于旋翼飞机的反扭矩和偏航控制系统
公开(公告)号：US06416015B1
公开(公告)日：2002-07-09
申请号：US09846072
申请日：2001-05-01
申请人： Franklin D. Carson
发明人： Franklin D. Carson
IPC分类号： B64C2782
CPC分类号： B64C27/82 , B64C2027/8245
摘要： A rotary-wing aircraft comprises a main rotor, a tail boom extending through an area of downwash from the main rotor, and first and second linear nozzles fixedly coupled to the tail boom. The first nozzle is adapted to discharge a sheet of fluid in a direction substantially tangential to an outer surface of the tail boom to divert the rotor downwash and thereby produce a force that counteracts the biasing torque of the main rotor. The rotary-wing aircraft further comprises a yaw-control member movably coupled to the tail boom. The second nozzle is adapted to discharge a sheet of fluid in a direction substantially tangential to an outer surface of the yaw-control member to further divert the rotor downwash and thereby increase the force that counters the main-rotor torque.
摘要翻译：旋转翼飞行器包括主转子，延伸穿过主转子下降区域的尾臂以及固定地联接到尾吊杆的第一和第二线性喷嘴。第一喷嘴适于在基本上与尾臂的外表面相切的方向上排放流体片，以使转子下降，从而产生抵消主转子的偏置扭矩的力。旋转翼飞机还包括可移动地联接到尾吊杆的偏航控制构件。第二喷嘴适于在基本上与偏转控制构件的外表面相切的方向上排出流体片，以进一步转动转子下洗液，从而增加与主转子扭矩相反的力。

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