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    • 7. 发明申请
    • Video Infrared Ophthalmoscope
    • 视频红外眼镜
    • US20120257163A1
    • 2012-10-11
    • US13416915
    • 2012-03-09
    • David S. DyerJames Higgins
    • David S. DyerJames Higgins
    • A61B3/12
    • A61B3/13
    • An ophthalmoscope includes a wearable headset. The wearable headset has a light source, a beam splitter reflecting infrared radiation from the light source to an eye, a camera collecting radiation reflected by the eye through the beam splitter, an analog to digital convertor receiving a raw signal from the camera based on the collected radiation, the analog to digital convertor converting the raw signal to a digital signal; a black and white to color converter converting the digital signal into a color signal, a streaming video converter processing the color signal into a video signal, and a pair of video monitors displaying an image of the eye based on the video signal. The wearable headset also has a video transmitter, the video transmitter transmitting the video signal to a computer over a network, the computer extracting a plurality of images from the video signal.
    • 检眼仪包括可戴式耳机。 可穿戴耳机具有光源,分束器,其将从光源到眼睛的红外线辐射器反射,收集由眼睛通过分束器反射的辐射的照相机;模数转换器,其基于相机收到来自照相机的原始信号 收集辐射,模数转换器将原始信号转换为数字信号; 将该数字信号转换为彩色信号的黑白变色转换器,将该彩色信号处理为视频信号的流式视频转换器,以及基于该视频信号显示该眼睛图像的一对视频监视器。 可戴式耳机还具有视频发射器,视频发射器通过网络将视频信号发送到计算机,计算机从视频信号中提取多个图像。
    • 8. 发明申请
    • VIDEO INFRARED OPHTHALMOSCOPE
    • 视频红外眼镜
    • US20100245765A1
    • 2010-09-30
    • US12606868
    • 2009-10-27
    • David S. DyerJames Higgins
    • David S. DyerJames Higgins
    • A61B3/12
    • A61B3/13
    • An opthalmoscope includes a wearable headset. The wearable headset has a light source, a beam splitter reflecting infrared radiation from the light source to an eye, a camera collecting radiation reflected by the eye through the beam splitter, an analog to digital convertor receiving a raw signal from the camera based on the collected radiation, the analog to digital convertor converting the raw signal to a digital signal; a black and white to color converter converting the digital signal into a color signal, a streaming video converter processing the color signal into a video signal, and a pair of video monitors displaying an image of the eye based on the video signal. The wearable headset also has a video transmitter, the video transmitter transmitting the video signal to a computer over a network, the computer extracting a plurality of images from the video signal.
    • 眼镜包括可戴式耳机。 可穿戴耳机具有光源,分束器,其将从光源到眼睛的红外线辐射器反射,收集由眼睛通过分束器反射的辐射的照相机;模数转换器,其基于相机收到来自照相机的原始信号 收集辐射,模数转换器将原始信号转换为数字信号; 将该数字信号转换为彩色信号的黑白变色转换器,将该彩色信号处理为视频信号的流式视频转换器,以及基于该视频信号显示该眼睛图像的一对视频监视器。 可戴式耳机还具有视频发射器,视频发射器通过网络将视频信号发送到计算机,计算机从视频信号中提取多个图像。
    • 9. 发明申请
    • AIRCRAFT INTERNAL WING AND DESIGN
    • 飞机内部设计与设计
    • US20070164147A1
    • 2007-07-19
    • US10871310
    • 2004-06-18
    • Robert CarrJames Higgins
    • Robert CarrJames Higgins
    • B64C39/08
    • B64C3/46B64C39/066B64C39/068Y02T50/14
    • An aircraft designed with three wings located on either side of the fuselage. The forward wing has a downward angle with a curved top and bottom surface. The upper wing is located towards the rear of the aircraft and above the forward wing. The lower wing is located below the upper wing and slightly forward. It is also located to the rear and below of the forward wing. The outer ends of all three wings come into contact at one point. The forward wing uses the Coanda effect to increase the airflow across the top surface of the bottom wing. The aircraft can be designed so that it is large enough to carry people and/or cargo, or to be small enough to be flown as a toy aircraft. The like design can use any type of aircraft engine commonly used today. One embodiment of the aircraft has two turbines, shaft-coupled to a power source, located on either side of the forward end of the fuselage. Each engine has part of its thrust diverted through and directed by a plenum disposed internal of the coanda toward both sides of the fuselage so that an equal amount of thrust flows through the duct and over the wings on either side of the fuselage. This ensures equal lift on the coanda and both wings on either side of the fuselage in the event that one engine malfunctions.
    • 设计有三个机翼的飞机位于机身两侧。 前翼具有向下的角度,具有弯曲的顶部和底部表面。 上翼位于飞机的后方,位于前翼的上方。 下翼位于上翼下方,稍微向前。 它也位于前翼的后方和下方。 所有三个翼的外端在一点接触。 前翼使用柯恩达效应来增加穿过底翼顶表面的气流。 该飞机可以设计成足够大以携带人和/或货物,或者足够小以作为玩具飞机飞行。 类似的设计可以使用今天普遍使用的任何类型的飞机引擎。 飞机的一个实施例具有两个位于机身前端两侧的与电源轴耦合的涡轮机。 每个发动机的一部分推力通过设置在机身内部的整流室并通过机身的两侧而被引导,以使等量的推力流过机身的导管和机身的两侧。 如果一个发动机发生故障,这样可以确保机身两侧的平均升力和机身两侧的两翼。