中科微点-全球专利检索

  1. Login
  2. Sign Up

Search Results

4 records (took 0.013 seconds)

    Controlling aircraft aerial movements, defeating icing on aircraft surfaces, aiding decontamination, and damping turbulence effects on aircraft by the method of micro-perforated airfoil coordinated precision flow management
    3.
    发明申请
    Controlling aircraft aerial movements, defeating icing on aircraft surfaces, aiding decontamination, and damping turbulence effects on aircraft by the method of micro-perforated airfoil coordinated precision flow management 审中-公开
    通过微孔翼型协调精密流量管理的方法控制飞机空中运动，击败飞机表面的结冰，辅助净化和阻尼对飞机的紊流影响

    公开(公告)号：US20090210103A1

    公开(公告)日：2009-08-20

    申请号：US11998722

    申请日：2007-12-03

    Applicant: Michael Leon Cook

    Inventor： Michael Leon Cook

    IPC: G06F17/00 ,  B64C21/10

    CPC classification number: B64C23/005 ,  B64C21/025 ,  B64C2230/04 ,  B64C2230/06 ,  B64C2230/22 ,  Y02T50/166

    Abstract: A method is provided whereby airplanes or any device with the functionality and usefulness of an airplane may be controlled without the use of any traditional effectors, such as flaps, rudders, ailerons, spoilers, and all like hinged, moveable airfoils attached to a wing or a fuselage. The means of controlling such airplanes while in flight will be by controlling the laminar air flow over all lifting surfaces so as to vary the amount and quality of the lift provided. All lifting surfaces on the airplane will be divided into dozens, hundreds, or thousands of small zones, each of which can be readily controlled by a central flight computer and each of which is capable of modifying its immediate airflow condition, whether that be laminar flow or some particular degree and variety of local eddy current. Summing over all the inputs of conditions above the multitude of zones, the central flight computer will possess algorithms and programs suitable to effect any desired change in attitude, altitude, orientation, and course of the airplane that is desired.

    Abstract translation: 提供了一种方法，其中可以控制飞机或具有飞机的功能性和有用性的任何装置，而不需要使用任何传统的执行器，例如襟翼，方向舵，副翼，扰流板以及所有类似于连接到机翼上的铰接的可移动翼型件 机身。 在飞行中控制这种飞机的手段将是通过控制所有提升表面上的层流气流，以便改变所提供的升力的数量和质量。 飞机上的所有提升表面将分为几十个，几百个或数千个小区域，每个小区域都可以由中央飞行计算机轻松控制，每个小区域都能够修改其直接气流状况，无论是层流 或一些特定程度和各种局部涡流。 总结所有在多个区域以上的条件的输入，中央飞行计算机将拥有适合于实现期望的飞机的姿态，高度，方向和航向的任何期望的改变的算法和程序。

    Centripetal reflex method of space launch
    4.
    发明授权
    Centripetal reflex method of space launch 失效
    向心反射方法的太空发射

    公开(公告)号：US07523892B2

    公开(公告)日：2009-04-28

    申请号：US11084780

    申请日：2005-03-21

    Applicant: Michael Leon Cook

    Inventor： Michael Leon Cook

    IPC: B64G1/38

    CPC classification number: B64G1/005

    Abstract: A method of launching space vehicles by towing them aloft, then twirling them around a large transport aircraft (40) at the center of a formation (AA) of other tow aircraft (28, 34) and other devices of the invention. A lengthy, semi-rigid tow pipeline (14) serves as a conduit for the transfer of fuels and oxidizers, as the tow cable, and as an energy storage device that reflexes efficiently when it is flexed. The flexing of tow pipeline (14) is caused by a parachute (22) acting in conjunction with all the aircraft making the tighest turn they are capable of doing. Tow aircraft in certain arrays (28) are joined to tow pipeline (14) by sliding trollies (26) that also host canard rotor wings for the aerodynamic support of the main tube (12). The tow trollies (26) aid the sliding tow aircraft arrays (28) in gaining mechanical advantage to accelerate the space vehicle. The space vehicle may also burn its own motors for a longer-than-usual time as it gains in angular velocity because its fuels are replenished by a pipeline that automatically increases the pressure and volume of fuel flow as the angular acceleration increases. The tow pipeline (14) features a micro-hole laminar lift foil (50) on the top surface of the wing and on the bottom. By balancing the vacuum level in the plurality of chamber underneath the plurality of lift foil 50, the pilot or autopilot has an effective way to control the flight characteristics of the tow pipeline (14). In some embodiments the micro-hole laminar lift foil (50) on the top and bottom will made of transparent hollow wire segments or other material so arranged as to pass ambient light through to photo-voltaic cells below that convert sunlight to electrical energy.

    Abstract translation: 一种通过将空中飞行器高空搬运的方法，然后将它们绕在其他牵引飞机（28,34）和本发明的其它装置的地层（AA）的中心的大型运输机（40）周围旋转。 冗长的半刚性丝束管道（14）用作用于传输燃料和氧化剂的导管，作为牵引电缆，以及作为在弯曲时有效反射的能量存储装置。 拖曳管道（14）的弯曲是由与降落伞（22）一起作用的所有飞机作出最大的转弯而产生的。 将具有某些阵列（28）的牵引飞机通过滑动涡卷（26）连接到拖曳管道（14），其也承载用于主管（12）的空气动力学支撑的芥末转子翼。 牵引绞车（26）有助于滑动牵引飞机阵列（28）获得机械优势，以加速航天器。 空间飞行器还可以将其自己的马达燃烧的时间长于平常的时间，因为它以角速度增加，因为其燃料由管道补充，管道随着角加速度的增加而自动增加燃料流量的压力和体积。 牵引管道（14）在机翼的顶部表面和底部上具有微孔层压提升箔（50）。 通过平衡多个提升箔50之下的多个室中的真空度，导向装置或自动驾驶仪具有控制牵引管道（14）的飞行特性的有效方式。 在一些实施例中，顶部和底部上的微孔层状提升箔（50）将由透明中空线段或其它材料制成，其布置成将环境光通过到将太阳光转换成电能的光伏电池。

Patent Agency Ranking