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    • 3. 发明授权
    • Means to detect damage in composite material panels
    • 检测复合材料板材损坏的手段
    • US08964172B1
    • 2015-02-24
    • US12890758
    • 2010-09-27
    • Arlen E. BreiholzPeter J. MorganThomas A. Potts
    • Arlen E. BreiholzPeter J. MorganThomas A. Potts
    • G01N21/00G01J1/04G01J1/42G01J5/08G01M11/08G01M11/00G01L1/24
    • G01M11/086G01L1/242G01M5/0033G01M5/0091G01M11/083G01M11/3109G01M11/3136
    • The present disclosure describes an apparatus including a composite panel. The apparatus includes a first composite panel including a first optical fiber embedded therein, the first optical fiber being arranged in a pattern, and a first input port connected to a first end of the first optical fiber, the first input port configured to receive an optical signal from an optical time domain reflectometer. The optical time domain reflectometer is configured to send the optical signal through the first input port and measure a strength of a reflected optical signal that is reflected back from the first optical fiber, wherein the strength indicates a measured optical impedance of the first optical fiber. A measured optical impedance that is substantially the same as a baseline optical impedance for the fiber indicates no damage, while a measured optical impedance that differs from the baseline optical impedance by a predetermined threshold indicates damage.
    • 本公开描述了包括复合面板的装置。 该装置包括第一复合面板,其包括嵌入其中的第一光纤,第一光纤布置成图案,第一输入端口连接到第一光纤的第一端,第一输入端口被配置为接收光学 来自光时域反射计的信号。 光时域反射计被配置为通过第一输入端发送光信号,并测量从第一光纤反射回的反射光信号的强度,其中强度表示第一光纤的测量的光阻抗。 与光纤的基线光阻抗基本上相同的测量光阻抗表示没有损坏,而与基准光阻抗不同的预测阈值的测量光阻抗指示损坏。
    • 4. 发明授权
    • Optical system for vehicle flight control
    • 车辆飞行控制光学系统
    • US07039292B1
    • 2006-05-02
    • US10936928
    • 2004-09-09
    • Arlen E. Breiholz
    • Arlen E. Breiholz
    • G02B6/00
    • G02B26/0816G05D1/102H04N5/2259
    • A switchable optical system includes a primary optical system positioned to receive a forward view image, forward from the vehicle, during a reconnaissance mode of operation. A secondary optical system is operatively associated with the primary optical system for receiving opposing side images, side-looking from the vehicle. An imaging sensor is operatively associated with the primary optical system and with the secondary optical system. A mode switch is operatively associated with the primary optical system and the secondary optical system for switching between the reconnaissance mode of operation and a biomimetic mode of operation. The forward view image is sensed by the imaging sensor during the reconnaissance mode of operation; and, a portion of the forward view image and the opposing side images are simultaneously sensed by the imaging sensor for balancing the optic flow during the biomimetic mode of operation.
    • 可切换光学系统包括主要光学系统,其被定位成在侦察操作模式期间从车辆向前接收前视图像。 辅助光学系统与主要光学系统可操作地相关联,用于接收来自车辆的侧视图像。 成像传感器与初级光学系统和辅助光学系统可操作地相关联。 模式开关可操作地与主光学系统和辅助光学系统相关联,用于在侦察操作模式和仿生模式之间切换。 在侦察操作模式期间,摄像传感器检测正视图; 并且通过成像传感器同时感测前视图像和相对侧图像的一部分,以在仿生模式操作期间平衡光流。
    • 5. 发明授权
    • Aircraft groundspeed measurement system and technique
    • 飞机地面速度测量系统和技术
    • US4594676A
    • 1986-06-10
    • US453676
    • 1982-12-27
    • Arlen E. BreiholzRobert H. PoolGlenn W. Sellers
    • Arlen E. BreiholzRobert H. PoolGlenn W. Sellers
    • G01S13/58G01S13/60
    • G01S13/60G01S13/583
    • A system and technique is disclosed which enables the measurement and display of aircraft groundspeed using a modified FMCW radar altimeter. The system is constructed to have a conventional FMCW altimeter transmitter and receiver for transmitting and receiving vertical return signals, and a narrowbeam forward-looking antenna and associated receiver for detecting return signals from the forward angle. The transmitted signal is triangularly modulated to produce returns on both the upsweep and downsweep of the modulation and the difference between the frequencies of those returns, as detected by the forward looking antenna, is proportional to aircraft slant velocity. The system also detects slant range and altitude and combines them with slant velocity to produce an output representing the aircraft groundspeed.
    • 公开了一种使用改进的FMCW雷达高度计测量和显示飞机地速的系统和技术。 该系统被构造成具有用于发送和接收垂直返回信号的常规FMCW高度计发射器和接收器,以及用于从前向角检测返回信号的窄带前视天线和相关联的接收器。 传输的信号被三角调制,以在调制的上升和下降两者产生返回,并且由正向天线检测到的那些返回的频率之间的差异与飞机倾斜速度成比例。 该系统还检测倾斜范围和高度,并将其与倾斜速度相结合,以产生代表飞机地速的输出。
    • 8. 发明授权
    • Modulation of aircraft guidance lights
    • 飞机导向灯调制
    • US07679528B1
    • 2010-03-16
    • US11494939
    • 2006-07-28
    • Timothy J. EtheringtonArlen E. Breiholz
    • Timothy J. EtheringtonArlen E. Breiholz
    • G08B21/00
    • G08G5/0021B64F1/20G01S1/70G08G5/025
    • An aircraft landing and/or taxiing system has a plurality of landing zone, runway, and/or taxiway lights capable of receiving information signals and transmitting optically signals representative of the information signals. A processing system for providing the information signals to the plurality of lights is also used. The system also comprises a sensor tuned to receive light of a specific range of wavelengths, the light being emitted from the lights. Also, a processing system coupled to the sensor and configured with software to interpret signals received by the sensor is used. Program code runs on the processing system. The program code is configured to determine the location of an aircraft on the taxiway based on the light signal received from one or more of the taxiway lights. Also, the aircraft landing and/or taxiing system utilizes modulated lights to provide information pertinent to aircraft landing and/or taxiing operations.
    • 飞机着陆和/或滑行系统具有能够接收信息信号并发送表示信息信号的光信号的多个着陆区,跑道和/或滑行道灯。 还使用用于向多个灯提供信息信号的处理系统。 该系统还包括被调谐以接收特定波长范围的光的传感器,光从灯发射。 此外,使用耦合到传感器并配置有用于解释由传感器接收的信号的软件的处理系统。 程序代码在处理系统上运行。 程序代码被配置为基于从一个或多个滑行道灯接收到的光信号来确定飞行器在滑行道上的位置。 此外,飞机着陆和/或滑行系统利用调制光提供与飞机着陆和/或滑行操作有关的信息。