One-dimensional global rainbow measurement device and measurement method
    3.
    发明授权
    One-dimensional global rainbow measurement device and measurement method 有权
    一维全球彩虹测量装置及测量方法

    公开(公告)号:US09217669B2

    公开(公告)日:2015-12-22

    申请号:US14356723

    申请日:2013-05-10

    Abstract: The present invention provides a one-dimensional global rainbow measurement device and a measurement method. The measurement device comprises three parts, i.e., a laser emission unit, a signal collection unit and a signal processing unit. The laser emission unit is modulated to be a light sheet by a laser beam emitted by a laser, and configured to irradiate droplets in a spray field to generate rainbow signals. The signal collection unit is configured to separately image, by an optical system unit, the rainbow signals at measurement points of different height onto different row pixels of a CCD signal collector. The signal processing unit is configured to convert the received rainbow signals and process by a computer the rainbow signals in a form of data to obtain the measured values. The present invention can analyze gas-liquid phase flow fields during the injection, realize the online measurement of fuel atomization, spray and other processes, and can measure the refractive index, size, temperature and other parameters of the spray droplets in a real-time and non-contact manner.

    Abstract translation: 本发明提供一维全球彩虹测量装置和测量方法。 测量装置包括三部分,即激光发射单元,信号收集单元和信号处理单元。 通过激光发射的激光束将激光发射单元调制成光片,并配置为在喷射场中照射液滴以产生彩虹信号。 信号收集单元被配置为通过光学系统单元将不同高度的测量点处的彩虹信号分开地映射到CCD信号收集器的不同行像素上。 信号处理单元被配置为转换所接收的彩虹信号,并且由计算机以数据的形式处理彩虹信号以获得测量值。 本发明可以在注射期间分析气液相流场,实现燃料雾化,喷雾等工艺的在线测量,并可实时测量喷雾液滴的折射率,尺寸,温度等参数 和非接触的方式。

    Supercritical carbon dioxide state monitoring and control system based on infrared spectrum characteristic analysis

    公开(公告)号:US11662306B2

    公开(公告)日:2023-05-30

    申请号:US17368044

    申请日:2021-07-06

    CPC classification number: G01N21/3504 G01N2021/3536

    Abstract: A supercritical carbon dioxide state monitoring and control system based on infrared spectrum characteristic analysis. The system includes: a test section for carbon dioxide to pass through; an infrared light source emitting a detection beam to the carbon dioxide passing through the test section; an infrared spectrometer receiving and analyzing the detection beam passing through the carbon dioxide; and a pressure control module controlling pressure of the carbon dioxide at a set value. In addition, the system also includes a temperature control module capable of monitoring and adjusting temperature of the supercritical carbon dioxide. The supercritical carbon dioxide state monitoring and control system may monitor and control a state of the carbon dioxide at an inlet of an apparatus under an actual operation condition in a Brayton cycle system, which improves working performance of the apparatus in the Brayton cycle system, thereby improving overall efficiency of the Brayton cycle system.

    TURBINE AND BRAYTON CYCLE INCLUDING SAME
    7.
    发明申请

    公开(公告)号:US20200263552A1

    公开(公告)日:2020-08-20

    申请号:US16444580

    申请日:2019-06-18

    Abstract: A turbine for solar thermal power generation and a Brayton cycle are disclosed. The turbine includes a blade which has a cooling working medium inlet and a cooling working medium jet orifice. The blade is provided as a cavity with hollow interior; the cooling working medium inlet is located inside the blade; the cooling working medium jet orifice is provided on the blade surface on which is provided a spectral conversion coating; the spectral conversion coating converts heat on the blade surface into conversion characteristic band radiation which is radiation energy adjacent to cooling working medium characteristic band radiation of a cooling working medium. The turbine adopts a characteristic spectral coating and a jet cooling to enhance the cooling effect for a turbine blade and to improve the system efficiency of the Brayton cycle.

    Turbine and brayton cycle including same

    公开(公告)号:US11015463B2

    公开(公告)日:2021-05-25

    申请号:US16444580

    申请日:2019-06-18

    Abstract: A turbine for solar thermal power generation and a Brayton cycle are disclosed. The turbine includes a blade which has a cooling working medium inlet and a cooling working medium jet orifice. The blade is provided as a cavity with hollow interior; the cooling working medium inlet is located inside the blade; the cooling working medium jet orifice is provided on the blade surface on which is provided a spectral conversion coating; the spectral conversion coating converts heat on the blade surface into conversion characteristic band radiation which is radiation energy adjacent to cooling working medium characteristic band radiation of a cooling working medium. The turbine adopts a characteristic spectral coating and a jet cooling to enhance the cooling effect for a turbine blade and to improve the system efficiency of the Brayton cycle.

Patent Agency Ranking