Patents
Literature
Patsnap Copilot is an intelligent assistant for R&D personnel, combined with Patent DNA, to facilitate innovative research.
Patsnap Copilot

352 results about "Optical depth" patented technology

In physics, optical depth or optical thickness, is the natural logarithm of the ratio of incident to transmitted radiant power through a material, and spectral optical depth or spectral optical thickness is the natural logarithm of the ratio of incident to transmitted spectral radiant power through a material. Optical depth is dimensionless, and in particular is not a length, though it is a monotonically increasing function of optical path length, and approaches zero as the path length approaches zero. The use of the term "optical density" for optical depth is discouraged.

Optical fiber temperature-depth diving mark continuous measuring system

The invention relates to marine hydrology parameter monitoring, and particularly discloses an optical fiber temperature-depth diving mark continuous measuring system. The system comprises a communication buoy, a main floating ball, an instrument bin, a demodulating system, a temperature-depth chain, a mooring rope, an acoustical releaser and an anchoring weight, wherein the communication buoy comprises a solar cell, a big dipper communication plate card and a satellite combined antenna; the demodulating system comprises a demodulation module and a lithium battery and is arranged in the instrument bin, and the temperature-depth chain integrates a temperature sensor and a pressure sensor for measuring temperature and pressure, and the communication buoy, the main floating ball, the instrument bin, the temperature-depth chain, the releaser and the anchoring weight are successively connected through the mooring rope. The optical depth diving mark continuous measuring system provided by the invention has the advantages that the high density, real time, continuation and long-term observation of a temperature-depth vertical section from a sea surface to 500m underwater are realized, the data is exact and reliable, and the economic benefit is high; the optical fiber temperature-depth diving mark continuous measuring system is widely applied in different marine observation operations and provides a novel observation means for measuring sea temperature-depth.
Owner:INST OF SEMICONDUCTORS - CHINESE ACAD OF SCI

Non-invasive blood glucose detector based on metabolic heat-optical method

The invention provides a non-invasive blood glucose detector based on a metabolic heat-optical method, and belongs to a human body blood glucose measurement device. The blood glucose detector comprises a detection probe and a data processing and displaying system, wherein the detection probe comprises a series of sensing measurement elements, such as an infrared radiation sensor, a thermistor, a humidity sensor, a light-wave receiver, a heat-conduction bar and the like, and is used for directly measuring parameters of detected positions of a human body; the data processing and displaying system comprises a microprocessor, as well as a display unit and a storage unit which are connected with the microprocessor respectively; a signal detected by the detection probe is processed by virtue of amplification filter, A/D (analog-to-digital) conversion and other modes, and then is input into the microprocessor; and the microprocessor carries out data processing according to a preset algorithm to acquire a blood glucose value detected by the detector, and displays and stores the blood glucose value. In the non-invasive blood glucose detector, a principle of combining a metabolic heat method and an optical method is adopted, so that the finally output blood glucose value has a higher reference value.
Owner:TSINGHUA UNIV +1

Focusing leveling measuring method and device

The invention discloses a measuring method and device for focusing and leveling, and relates to a new method for the focusing and leveling sensor system of a wafer applicable to the projection photolithography system, and belongs to the field of optical measurement. The invention consists of three parts, namely, a light source collimating module, a focusing subsystem and a leveling subsystem. The laser of the invention emits laser light, the laser light is collimated by a single mode fiber and then passes through a drift compensation device, and then permeates a polarized optical splitter and a Lambda fourth wave plate and then shines on a measured silicon chip. The ray is led to pass through the measured silicon chip repeatedly through a planar mirror and a corner cube prism, and then is magnified in front of a position detector by a lens system, thereby obtaining the defocusing information of the silicon chip surface. The ray is rebounded along the path by a planar optical splitter, the ray permeates a lens and shines on a position-sensitive detector, thereby obtaining the two-dimensional inclination information of the silicon chip surface. The system has high resolution as well as simple structure of optical path and needs no complicated optical design.
Owner:BEIJING INSTITUTE OF TECHNOLOGYGY

Optical method based high-speed aircraft hot surface full-field deformation measuring device

InactiveCN103558243ARealize deformation measurementGood test resultsUsing optical meansMaterial thermal analysisEngineeringRadiant heat
The invention provides an optical method based high-speed aircraft hot surface full-field deformation measuring device. The optical method based high-speed aircraft hot surface full-field deformation measuring device comprises a double-layer quartz lamp heating array, a thin-wall high-speed aircraft shell, a square transparent window, speckle particles, a thermocouple sensor, a signal amplifier, a temperature control computer, a driving power supply, a CMOS (Complementary Metal Oxide Semiconductor) camera, a lens, a narrow-band-pass optical filter and an image processing computer. In order to solve the problem of signal blockage caused by a high temperature radiant heat source between the CMOS camera and the surface of the high-speed aircraft shell, the vertical double-layer quartz lamp heating array is designed and the square transparent window with small area is formed, so that the optical camera lens can obtain images of the hot surface of the high-speed aircraft through the transparent window. The interference light ray of the quartz lamp heating array is shielded by selecting the narrow-band-pass optical filter with specific wave length, so that speckle images with high quality and no degeneration on the hot surface of the high-speed aircraft is obtained; a digital image correlation method is utilized for analyzing the speckle images under different temperatures to realize full measurement on the displacement field and the strain field of the hot surface of the high-speed aircraft in a high temperature environment.
Owner:BEIHANG UNIV
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products