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    • 5. 发明授权
    • Dynamic adjustment of wing surfaces for variable camber
    • 可变弧度的翼面动态调整
    • US08447445B2
    • 2013-05-21
    • US12620698
    • 2009-11-18
    • Dan OnuJohn D. WinterCandy L. CarrPaul M. VijgenGary A. EmchMichael E. Renzelmann
    • Dan OnuJohn D. WinterCandy L. CarrPaul M. VijgenGary A. EmchMichael E. Renzelmann
    • B64C13/00
    • B64C9/12Y02T50/32Y02T50/44
    • The movable surfaces affecting the camber of a wing are dynamically adjusted to optimize wing camber for optimum lift/drag ratios under changing conditions during a given flight phase. In a preferred embodiment, an add-on dynamic adjustment control module provides command signals for optimum positioning of trailing edge movable surfaces, i.e., inboard flaps, outboard flaps, ailerons, and flaperons, which are used in place of the predetermined positions of the standard flight control system. The dynamic adjustment control module utilizes inputs of changing aircraft conditions such as altitude, Mach number, weight, center of gravity (CG), vertical speed and flight phase. The dynamic adjustment control module's commands for repositioning the movable surfaces of the wing are transmitted through the standard flight control system to actuators for moving the flight control surfaces.
    • 在给定的飞行阶段期间,在变化的条件下,动态地调整影响机翼弧度的可移动表面,以优化机翼弧度以获得最佳升力/牵引比。 在优选实施例中,附加动态调节控制模块提供用于最终定位后缘可移动表面(即,内侧翼片,外侧翼片,副翼和襟翼)的命令信号,其用于代替标准的预定位置 飞行控制系统。 动态调整控制模块利用高度,马赫数,重量,重心(CG),垂直速度和飞行阶段等改变飞机状态的输入。 动态调整控制模块用于重新定位机翼的可移动表面的命令通过标准飞行控制系统传输到用于移动飞行控制表面的致动器。
    • 6. 发明授权
    • Gas handling for plastics liquefaction
    • 气体处理塑料液化
    • US6121334A
    • 2000-09-19
    • US230133
    • 1999-05-13
    • John D. Winter
    • John D. Winter
    • C10G1/00C10G1/10C08J11/10B01D53/14C08J11/14
    • C10G1/002C10G1/10
    • The present invention relates to a method for removing high molecular weight high melting point hydrocarbon vapors from a hydrocarbon vapor offgas stream produced during the liquefaction of a solid waste plastic material to produce an oil that serves as a liquid feedstock for a partial oxidation reaction. The hydrocarbon vapor offgas stream (2) is directly contacted with a water spray (4) at a condensation temperature above the melting point of the high molecular weight hydrocarbons contained in the offgas. This results in the condensation and convenient removal of the high melting point hydrocarbons, referred to as "waxes." One or more subsequent condensation steps can be conducted at lower condensation temperatures to remove the lower temperature condensable hydrocarbons. The remaining uncondensed vapors are then recycled to serve as a heater fuel for the liquefaction of the waste plastic material.
    • PCT No.PCT / US97 / 12481 Sec。 371日期1999年5月13日 102(e)1999年5月13日PCT PCT 1997年7月14日PCT公布。 出版物WO98 / 02504 日期1998年1月22日本发明涉及一种从在固体废塑料材料液化期间产生的烃蒸汽废气流中除去高分子量高熔点烃蒸汽的方法,以产生用作液体原料的油 部分氧化反应。 烃蒸汽废气流(2)在高于废气中所含的高分子量烃的熔点的冷凝温度下与水喷雾(4)直接接触。 这导致冷凝和方便地去除被称为“蜡”的高熔点烃。 一个或多个随后的冷凝步骤可以在较低的冷凝温度下进行以除去较低温度的可冷凝烃。 然后将剩余的未冷凝的蒸气再循环用作用于液化废塑料的加热器燃料。
    • 7. 发明申请
    • DYNAMIC ADJUSTMENT OF WING SURFACES FOR VARIABLE CAMBER
    • 用于变幅摄像机的表面动态调整
    • US20100152926A1
    • 2010-06-17
    • US12620698
    • 2009-11-18
    • Dan OnuJohn D. WinterCandy L. CarrPaul M. VijgenGary A. EmchMichael E. Renzelmann
    • Dan OnuJohn D. WinterCandy L. CarrPaul M. VijgenGary A. EmchMichael E. Renzelmann
    • G05D1/00
    • B64C9/12Y02T50/32Y02T50/44
    • The movable surfaces affecting the camber of a wing are dynamically adjusted to optimize wing camber for optimum lift/drag ratios under changing conditions during a given flight phase. In a preferred embodiment, an add-on dynamic adjustment control module provides command signals for optimum positioning of trailing edge movable surfaces, i.e., inboard flaps, outboard flaps, ailerons, and flaperons, which are used in place of the predetermined positions of the standard flight control system. The dynamic adjustment control module utilizes inputs of changing aircraft conditions such as altitude, Mach number, weight, center of gravity (CG), vertical speed and flight phase. The dynamic adjustment control module's commands for repositioning the movable surfaces of the wing are transmitted through the standard flight control system to actuators for moving the flight control surfaces.
    • 在给定的飞行阶段期间,在变化的条件下,动态地调整影响机翼弧度的可移动表面,以优化机翼弧度以获得最佳升力/牵引比。 在优选实施例中,附加动态调节控制模块提供用于最终定位后缘可移动表面(即,内侧翼片,外侧翼片,副翼和襟翼)的命令信号,其用于代替标准的预定位置 飞行控制系统。 动态调整控制模块利用高度,马赫数,重量,重心(CG),垂直速度和飞行阶段等改变飞机状态的输入。 动态调整控制模块用于重新定位机翼的可移动表面的命令通过标准飞行控制系统传输到用于移动飞行控制表面的致动器。
    • 10. 发明授权
    • Dynamic adjustment of wing surfaces for variable camber
    • 可变弧度的翼面动态调整
    • US07641152B2
    • 2010-01-05
    • US11734842
    • 2007-04-13
    • Dan OnuJohn D. WinterCandy L. CarrPaul M. VijgenGary A. EmchMichael E. Renzelmann
    • Dan OnuJohn D. WinterCandy L. CarrPaul M. VijgenGary A. EmchMichael E. Renzelmann
    • G05D1/00
    • B64C9/12Y02T50/32Y02T50/44
    • The movable surfaces affecting the camber of a wing are dynamically adjusted to optimize wing camber for optimum lift/drag ratios under changing conditions during a given flight phase. In a preferred embodiment, an add-on dynamic adjustment control module provides command signals for optimum positioning of trailing edge movable surfaces, i.e., inboard flaps, outboard flaps, ailerons, and flaperons, which are used in place of the predetermined positions of the standard flight control system. The dynamic adjustment control module utilizes inputs of changing aircraft conditions such as altitude, Mach number, weight, center of gravity, vertical speed and flight phase. The dynamic adjustment control module's commands for repositioning the movable surfaces of the wing are transmitted through the standard flight control system to actuators for moving the flight control surfaces.
    • 在给定的飞行阶段期间,在变化的条件下,动态地调整影响机翼弧度的可移动表面,以优化机翼弧度以获得最佳升力/牵引比。 在优选实施例中,附加动态调节控制模块提供用于最终定位后缘可移动表面(即,内侧翼片,外侧翼片,副翼和襟翼)的命令信号,其用于代替标准的预定位置 飞行控制系统。 动态调整控制模块利用改变飞行器条件的输入,如高度,马赫数,重量,重心,垂直速度和飞行阶段。 动态调整控制模块用于重新定位机翼的可移动表面的命令通过标准飞行控制系统传输到用于移动飞行控制表面的致动器。