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    • 1. 发明授权
    • Resolution advisory display instrument for TCAS guidance
    • TCAS指导解决咨询显示工具
    • US5382954A
    • 1995-01-17
    • US068337
    • 1993-05-27
    • Thomas W. Kennedy, Jr.Donald F. Fenstermaker
    • Thomas W. Kennedy, Jr.Donald F. Fenstermaker
    • G01C23/00G01S13/93G08G5/04
    • G01S13/9303G01C23/005
    • An aircraft indicating system for displaying a resolution advisory signal from a Traffic Advisory and Collision Avoidance System provides an indicating pitch attitude symbol to the pilot engendering an instinctive response to avoid a collision. A driving circuit converts a TCAS signal in the form of a vertical speed command to a pitch command for energizing the indicating symbol by effecting a vertical displacement thereof in accordance with the guidance resolution advisory. The display signal is generated in accordance with the relationship: ##EQU1## where: .PHI.=aircraft roll attitude, limited to + or - 30.degree..THETA..sub.CMD =commanded pitch attitude defining the upper and lower pitch limits of the resolution advisory symbology.THETA..sub.EXIST =current pitch angleV.sub.ZTCAS =TCAS vertical speed commandV.sub.ZEXIST =current vertical speedV.sub.T =true airspeedK=conversion constant.
    • 用于显示来自交通咨询和碰撞避免系统的分辨率咨询信号的飞行器指示系统为飞行员提供指示音高姿态符号,产生本能反应以避免碰撞。 驱动电路以垂直速度指令的形式将TCAS信号转换成用于通过根据引导分辨率咨询进行其垂直位移来激励指示符号的音调命令。 根据以下关系生成显示信号:mited = +或 - 30°THETA CMD =定义分辨率咨询符号的上下限极限的指令俯仰姿态THETA EXIST =当前音调角VZTCAS = TCAS垂直速度指令VZEXIST = 当前垂直速度VT =真空速K =转换常数。
    • 2. 发明授权
    • Semi-automatic takeoff control system for aircraft
    • 半自动起飞控制系统
    • US3945590A
    • 1976-03-23
    • US543210
    • 1975-01-23
    • Thomas W. Kennedy, Jr.Harry D. Smith
    • Thomas W. Kennedy, Jr.Harry D. Smith
    • B64C13/16G05D1/06B64C13/18
    • G05D1/0661
    • A semi-automatic takeoff flight control system for automatically capturing a predetermined takeoff pitch attitude at a predetermined pitch rate during the aircraft takeoff rotation maneuver. In response to the manual rotation command from the pilot, control circuitry generates a pitch rate command to the elevator, limited to the predetermined pitch rate. As the craft rotates to an intermediate pitch attitude less than the desired predetermined takeoff climb attitude, circuitry is included to provide a pitch attitude command with regard to the predetermined reference attitude, which by virtue of rate, displacement, and integral control provides asymptotic capture of the predetermined reference attitude.
    • 一种半自动起飞飞行控制系统,用于在飞机起飞旋转动作期间以预定的俯仰速率自动捕获预定的起飞俯仰姿态。 响应于来自导频的手动旋转命令,控制电路产生对电梯的俯仰速率指令,限制到预定的俯仰速率。 当工艺旋转到小于期望的预定起飞爬升姿态的中间俯仰姿态时,包括电路以提供关于预定参考姿态的俯仰姿态指令,其通过速率,位移和积分控制提供渐近捕获 预定的参考态度。
    • 5. 发明授权
    • Hot dog cutter apparatus and method
    • 热狗切割设备及方法
    • US4976029A
    • 1990-12-11
    • US464364
    • 1990-01-12
    • Thomas W. Kennedy
    • Thomas W. Kennedy
    • A47J43/28B26D3/08
    • A47J43/28B26D3/08
    • A hot dog or sausage cutter apparatus for making partial cuts in a hot dog or sausage wherein the apparatus has generally curved body sections hingedly connected to permit the sections to move between an open position for the insertion of a hot dog or sausage to be cut and a closed position to make partial cuts in the body of the hot dog or sausage and a plurality of cutting blades extending upwardly from the interior surface of the pair of body sections and typically angular and longitudinal to the longitudinal axis of the hot dog or sausage whereby in placing the hot dog or sausage within the holder and closing the holder, the cutting blades penetrate and partially cut the hot dog or sausage so that the hot dog or sausage thereafter may be removed for cooking or further processing.
    • 一种用于在热狗或香肠中进行部分切割的热狗或香肠切割装置,其中所述装置具有铰接地连接的大致弯曲的主体部分,以允许所述部分在用于插入待热切割的热狗或要被切割的香肠的打开位置和 在热狗或香肠的身体中进行部分切割的封闭位置和从该对主体部分的内表面向上延伸并且通常与热狗或香肠的纵向轴线成角度和纵向的多个切割刀片,由此 在将热狗或香肠放置在保持器内并关闭保持器的情况下,切割刀片穿透并部分切割热狗或香肠,使得之后的热狗或香肠可以被去除以进行烹饪或进一步加工。
    • 6. 发明授权
    • Hand tool, such as a sledgehammer, with replaceable head
    • 手工工具,如大锤,带可更换头
    • US4753137A
    • 1988-06-28
    • US33590
    • 1987-04-01
    • Thomas W. Kennedy
    • Thomas W. Kennedy
    • B25D1/12B25G1/01B25G3/28B25G3/12
    • B25G3/28B25D1/12B25G1/01
    • A hand tool, such as striking device like a sledgehammer, having replaceable head elements, which device comprises a handle having a raised extension on one end and a threaded cavity therein, and a replaceable head element, having a cavity therein; an insert having a hole therein to fit into the top part of the cavity of the head element, a threaded bolt, an a retaining tubular, elastomeric element, subject to expansion on axial compression, whereby various head elements of different cavity size may be secured to the extension of the handle by placing the threaded bolt through the insert hole and through tubular retaining element and threading the bolt into a threaded cavity of the raised extension to axially compress and expand outwardly the tubular elastomeric element into a frictional and shock-absorbing relationship with the interior surface of the head element cavity, thereby providing a hand tool device by which head elements having various cavity dimensions may be rapidly and efficiently secured to the handle.
    • 诸如大锤之类的打击装置的手工工具具有可更换的头部元件,该装置包括一把手,该把手在一端具有凸起的延伸部,其中具有螺纹腔,以及在其中具有空腔的可更换的头元件; 插入件,其中具有孔以装配到头元件的空腔的顶部,螺栓,保持管,弹性体元件,在轴向压缩时经受膨胀,由此可以固定不同腔体尺寸的各种头部元件 通过将螺栓穿过插入孔并穿过管状保持元件并将螺栓穿入凸起延伸部的螺纹腔中以将管状弹性体元件向外压缩并向外膨胀成摩擦和减震关系 与头元件空腔的内表面,从而提供手工工具装置,具有各种空腔尺寸的头元件可以快速且有效地固定到手柄上。
    • 7. 发明授权
    • Side slip angle command SCAS for aircraft
    • 飞机侧滑指令SCAS
    • US4094479A
    • 1978-06-13
    • US781226
    • 1977-03-25
    • Thomas W. Kennedy, Jr.
    • Thomas W. Kennedy, Jr.
    • B64C13/18G05D1/08G05D1/10
    • G05D1/0816
    • A yaw axis stability and command augmentation system (SCAS) particularly applicable to STOL type aircraft includes three primary control terms proportional to side slip angle, side slip angle rate and rudder pedal force, wherein side slip angle rate is synthesized from measures of yaw rate, bank angle and lateral acceleration. These primary system feedback terms are supplied to the rudder electro-hydraulic secondary actuator which is positioned in accordance with their sum. The system serves to provide improved automatic damping of the Dutch roll modes, to suppress aircraft motion transients in yaw and roll under engine failure situations, to provide automatic turn-coordination in maneuvering flight, and to provide a side slip angle command capability to improve manual control precision in approach and landing under crosswind and lateral wind shear conditions.
    • 特别适用于STOL型飞机的偏航轴稳定性和指令增强系统(SCAS)包括与侧滑角,侧滑角速率和方向舵踏力成比例的三个主要控制项,其中侧滑角速率由横摆率, 横倾角和横向加速度。 这些主要的系统反馈术语被提供给根据其总和定位的方向舵电液二次致动器。 该系统用于提供荷兰滚动模式的改进的自动阻尼,以抑制在发动机故障情况下的偏航和滚转中的飞行器运动瞬变,以提供机动飞行中的自动转向协调,以及提供侧滑角度指令能力以改善手动 在侧风和侧风剪切条件下控制接近和着陆的精度。
    • 8. 发明授权
    • Ring laser gyroscope with a tube assembly
    • 环形激光陀螺与管组件
    • US5022761A
    • 1991-06-11
    • US431993
    • 1989-11-06
    • Thomas W. Kennedy
    • Thomas W. Kennedy
    • G01C19/66H01S3/083
    • G01C19/66H01S3/083H01S3/0835
    • A ring laser gyroscope, which has a triangular quartz block with a triangular quartz tube assembly forming an outer cavity for one rotating beam and an inner cavity for an oppositely rotating beam, is provided. The problem of lock-in of the beams is avoided. A pair of anodes and cathode means are provided for energizing the beams. A mirror is mounted at each corner of the block for reflecting the beams with one mirror being a partly reflective mirror for passing through portions of the inner beam and the outer beam. Outside the partly reflective mirror are mounted a first mirror for reflecting the inner beam, a second mirror for reflecting the outer beam, and a beam combiner mirror for combining the beams. A frusto-conical mirror receives the combined beams and reduces the mean diameter of the outer beam. A fringe detector receives the inner beam and outer beam on an area or point on a face of the fringe detector, which provides a gyroscope output.
    • 提供一种环形激光陀螺仪,其具有三角形石英块,其具有三角形石英管组件,其形成用于一个旋转梁的外腔和用于相反旋转梁的内腔。 避免了梁的锁定问题。 提供一对阳极和阴极装置用于激励光束。 镜子安装在块的每个角上,用于反射光束,其中一个反射镜是用于穿过内光束和外光束的部分反射镜。 在部分反射镜外部安装有用于反射内光束的第一反射镜,用于反射外光束的第二反射镜和用于组合光束的光束组合器镜。 截头圆锥镜接收组合光束并减小外光束的平均直径。 边缘检测器在条纹检测器的面上的区域或点上接收内束和外束,其提供陀螺仪输出。