公开(公告)号：US20070126602A1

公开(公告)日：2007-06-07

申请号：US11164808

申请日：2005-12-06

Applicant: Charles Bateman ,  David Fleming

Inventor： Charles Bateman ,  David Fleming

IPC: G08G5/00 ,  G08G1/123

CPC classification number: G08G5/0021 ,  B64D45/0005 ,  B64D2045/001

Abstract: A processor, software code, and a method for generating warning indicating that flaps are not suitably in a take-off position. A first component is configured to receive a first signal indicative of one of a group of flaps positions, the group including a take-off position. A second component is configured to receive a second signal indicative of an aircraft position. A third component is configured to compare the aircraft position to the contents of a database and to, by the comparison, determine whether the aircraft position is within a runway perimeter. A fourth component is configured to generate an alarm when the aircraft is within the runway perimeter and the flaps position is not the take-off position.

公开(公告)号：US20070115140A1

公开(公告)日：2007-05-24

申请号：US11164392

申请日：2005-11-21

Applicant: Charles Bateman ,  David Fleming

Inventor： Charles Bateman ,  David Fleming

IPC: G08B21/00

CPC classification number: G08B25/08 ,  B64D45/0005 ,  B64D2045/001

Abstract: A processor, software code, and a method for generating warning indicating that flaps are not suitably in a take-off position. A first component is configured to receive a first signal indicative of one of a group of flaps positions, the group including a take-off position. A second component is configured to receive a second signal indicative of an aircraft position. A third component is configured to compare the aircraft position to the contents of a database and to, by the comparison, determine whether the aircraft position is within a runway perimeter. A fourth component is configured to generate an alarm when the aircraft is within the runway perimeter and the flaps position is not the take-off position.

Abstract translation: 处理器，软件代码和用于产生警告的方法，其指示襟翼不适合处于起飞位置。 第一部件被配置为接收指示一组襟翼位置中的一个的第一信号，该组包括起飞位置。 第二部件被配置为接收指示飞机位置的第二信号。 第三组件被配置为将飞机位置与数据库的内容进行比较，并且通过比较来确定飞机位置是否在跑道周边内。 第四组件被配置为当飞行器在跑道周边内并且襟翼位置不是起飞位置时产生报​​警。

公开(公告)号：US20070013446A1

公开(公告)日：2007-01-18

申请号：US11250292

申请日：2005-10-14

Applicant: Sharath Navil ,  David Fleming

Inventor： Sharath Navil ,  David Fleming

IPC: H03L7/00

CPC classification number: H03L7/093

Abstract: A method for controlling loop bandwidth of a phase locked loop is described. The method includes setting the loop bandwidth to a value, calculating at least one of a phase error and a frequency change that occur subsequent to any setting or adjusting of loop bandwidth, and adjusting the loop bandwidth based on at least one of the phase error and the frequency change

Abstract translation: 描述了一种用于控制锁相环路环路带宽的方法。 该方法包括将环路带宽设置为一个值，计算在任何设置或调整环路带宽之后发生的相位误差和频率变化中的至少一个，以及基于相位误差和 频率变化

公开(公告)号：US20060192566A1

公开(公告)日：2006-08-31

申请号：US11383705

申请日：2006-05-16

Applicant: David Fleming

Inventor： David Fleming

IPC: H01H31/02

CPC classification number: G01R31/026 ,  G01R1/06788

Abstract: A continuity testing device has a probe element for contacting a conductor. A continuity testing circuit is coupled to the probe element. The continuity testing circuit will indicate continuity when a resistance level below a predetermined set-point is monitored. The continuity testing circuit has at least one of a vibrating or audible sensor to indicate electrical continuity of the conductor. The vibrating and/or audible sensor indicates a strength of the resistance level of the circuit tested by a quality of vibration or sound from the vibrating and/or audible sensor. A grounding wire is coupled to the continuity testing circuit. The grounding wire has a magnetic contact coupled thereto to ground the continuity testing device to any ferrous metallic grounded element. A housing is provided for holding and storing the probe element and the continuity testing circuit.

Abstract translation: 连续性测试装置具有用于接触导体的探针元件。 连续性测试电路耦合到探针元件。 当监测到低于预定设定点的电阻值时，连续性测试电路将指示连续性。 连续性测试电路具有用于指示导体的电连续性的振动或听觉传感器中的至少一个。 振动和/或听觉传感器表示通过来自振动和/或听觉传感器的振动或声音的质量测试的电路的电阻水平的强度。 接地线连接到连续性测试电路。 接地线具有耦合到其上的磁性接触，以将连续性测试装置接地到任何铁金属接地元件。 提供用于保持和存储探针元件和连续性测试电路的壳体。