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71 results about "Cavity loss" patented technology

Self Raman yellow light laser of composite cavity structure

The invention discloses a self Raman yellow light laser of a composite cavity structure. A laser diode pumping source emits pump light in an absorption belt of a gain medium, the pump light is focused inside the gain medium through a transmitting energy fiber and a coupling lens set, the gain medium absorbs the pump light to form population inversion, and base frequency laser generation is formed under the feedback action of a laser resonant cavity composed of a resonant cavity shared reflector and a laser total reflector; when base frequency laser passes through the gain medium, Raman gains are generated, and after the Raman gains are greater than the cavity loss of a Raman resonant cavity composed of the resonant cavity shared reflector, a beam splitter and a yellow light output mirror, stable Stokes light generation is formed in the Raman resonant cavity; the frequency of Stokes light is doubled in a frequency doubling crystal, and the generated yellow light secondary harmonic wave is output by the yellow light output mirror. The composite cavity structure is adopted, the length of a base frequency laser resonant cavity is largely decreased, and therefore the stable area of the resonant cavity is effectively enlarged, and the effect of improving the output power of the self Raman yellow light laser is achieved by applying higher pumping power.
Owner:TIANJIN UNIV

Laser gyroscope resonator loss measuring device and method

The present invention first provides a device and method capable of accurately measuring the loss of the laser gyroscope optical resonant cavity in real time. The main components of the basic equipment are sequentially installed with a laser light source assembly, an acousto-optic modulator, and an optical path adjustment assembly according to the direction of light propagation. etc. After the optical path passes through the half-mirror installed in the optical path adjustment component, the laser gyro resonator loss measurement and the real-time imaging of the diaphragm and light spot in the resonant cavity are respectively completed through the photoelectric detection component and the CCD component. The present invention also solves the problem of low accuracy of measuring the loss of the unknown laser gyro resonator by a single method. When the loss of the laser gyro resonator is high, the resonance path is selected for measurement, and when the loss is low, the time attenuation path is selected for measurement by switching the switch. After the device is completed, the relative position of the diaphragm and the laser spot in the resonant cavity can also be measured in real time. High measurement accuracy and low measurement cost. The signal-to-noise ratio of the measuring device is high, the device is easy to debug, compact in structure and small in size.
Owner:XIAN TECHNOLOGICAL UNIV

Low-threshold-value femtosecond pulse fiber laser

The invention relates to a low-threshold-value femtosecond pulse fiber laser. The low-threshold-value femtosecond pulse fiber laser consists of an optical-fiber coupling semiconductor laser, a wavelength division multiplexer, a ytterbium-doped single-mode gain fiber, two optical-fiber collimators, two quarter slides, two half slides, a polarization beam splitter, a faraday rotator, two reflection gratings, a reflection mirror and an optical isolator. The femtosecond laser adopts a semi-space semi-fiber annular cavity structure, the combined action of the faraday rotator and the half slides is adopted, and a group of grating pairs is adopted to carry out intra-cavity chromatic dispersion management on the laser, so that the polarization direction of the laser which passes through the faraday rotator twice is enabled to rotate for 90DEG and to be reflected from a vertical reflection port of the polarization beam splitter, a light path can be prevented from being lowered, and the introduction of an additional reflection mirror can be avoided; The polarization direction of the incident light which radiates on the first reflection grating is adjusted through the half slides, so that the highest diffraction efficiency can be achieved, the intra-cavity loss of the laser can be reduced, and an effect for reducing a mode locking threshold value can be realized.
Owner:UNIV OF SHANGHAI FOR SCI & TECH

Method for measuring diffraction loss of laser gyro

InactiveCN104713573ASolve the problem of inaccurate measurementShort operating cycleMeasurement devicesResonant cavityClassical mechanics
The invention belongs to a method for measuring the loss parameter of a laser gyro, and relates to a method for measuring the diffraction loss of the laser gyro. The measurement method comprises the following steps: assembling a matched reflector to an unapertured cavity, starting a frequency sweep laser, adjusting a light path matching part to make laser enter a resonant cavity composed of an unapertured diaphragm and the reflector, and measuring the initial cavity loss L1 of the unapertured diaphragm resonant cavity through a loss measurement system; disassembling the matched reflector from the unapertured resonant cavity [5], assembling the matched reflector to an apertured cavity, adjusting the light path matching part to make the laser enter a resonant cavity composed of the apertured cavity and the reflector, and measuring the cavity loss L2 of the apertured diaphragm resonant cavity through the loss measurement system [4]; and calculating a difference between the cavity loss L2 and the cavity loss L1 to obtain the diffraction loss of the apertured diaphragm resonant cavity. The method has the advantages of strong operationality, small error and high measurement precision, solves a problem that the measuring diffraction loss of the laser gyro cannot be accurately measured in the prior art, and has good application values.
Owner:FLIGHT AUTOMATIC CONTROL RES INST

Phase-insensitive recovery of clock pulses of wavelength division multiplexed optical signals

An optically-pumped mode-locked fiber ring laser for optical clock recovery of multiple wavelength division multiplexed optical signals actively mode-locks a plurality of outputs of the laser as a plurality of recovered clocks for a plurality of the multiple wavelength division multiplexed optical signals. The laser cavity has a cavity length corresponding to an integer multiple of bit periods of at least one of the multiplexed optical signals for receiving a pre-amplified version of the plurality of wavelength division multiplexed optical signals to provide gain modulation through a phase-insensitive parametric amplification and recirculating a proportion of the output from the laser cavity back through the laser cavity for spatially mode-locking the output of the laser cavity as a recovered clock whereby the recovered optical clock each having a periodic train of optical pulses with a repetition rate corresponding to the clock rate of the corresponding multiplexed optical signal is generated by mode-locking of the optically-pumped laser produced by a spatial modulation of the phase-insensitive parametric gain produced by the pulsed nature of the wavelength division multiplexed optical signals. A nonlinear gain medium disposed in the cavity has a sufficiently large dispersion at all of the wavelengths corresponding to the multiple wavelength multiplexed optical signals for minimizing four-wave mixing crosstalk among the multiple wavelength multiplexed optical signals, among the recovered clocks, and between the plurality of multiple wavelength multiplexed optical signals and the recovered clocks. The gain medium is pumped by the plurality of pre-amplified multiplexed optical signals to provide efficient gain modulation through the phase-insensitive parametric amplification at a plurality of narrow wavelength bands, each of the plurality of narrow wavelength bands immediately adjacent to a wavelength of a corresponding optical signal and each of the plurality of narrow wavelength bands including a corresponding recovered optical clock wavelength, and each of the corresponding optical signals copropagating in the laser cavity through the nonlinear gain medium with the recovered optical clocks. A parametric optical amplifier or a Raman amplifier having an inhomogenously broadened gain amplifies the plurality of recovered clocks for compensating a portion of the cavity loss at all wavelengths of the plurality of recovered clocks. A wavelength selector passes the light at the plurality of wavelengths of the recovered clocks for recirculation in the laser cavity and preventing the light from the multiple wavelength division multiplexed optical signals and a plurality of idler waves generated by four wave mixing between the multiple wavelength division multiplexed optical signals and recovered optical clocks from recirculating in the laser cavity.
Owner:CORNING INC

Silicon optical coupling assembly, silicon optical integrated module and integrated resonant fiber-optic gyroscope

The invention relates to a silicon optical coupling assembly, a silicon optical integrated module and an integrated resonant fiber-optic gyroscope. The integrated resonant fiber-optic gyroscope comprises a silicon light integration module and a photonic crystal fiber. An integrated light source in the silicon optical integration module emits light, the light is divided into two paths from the waveguide to the integrated Y waveguide, and then the light reaches the silicon optical coupling assembly after passing through the integrated optical modulator; a part of light enters the detector through the silicon optical coupling assembly, and the other light is coupled into the photonic crystal fiber and then enters the fiber from the other end through the silicon optical coupling assembly to form circulating light, and part of the circulating light is reflected into the detector. After the integrated optical modulator receives feedback of the detector, optical frequency shift is locked on aforward and reverse resonance peak, a frequency shift difference value is a gyro output signal, and a position error is compensated through the lens and the optical fiber control assembly so as to reduce cavity loss. The silicon optical coupling assembly has the characteristics of no melting point and integration, miniaturization of the gyroscope is facilitated, the signal-to-noise ratio of the gyroscope is high, and the gyroscope has high practical application value.
Owner:XIAN FLIGHT SELF CONTROL INST OF AVIC

Bragg grating, preparation method thereof and distributed feedback laser

The invention provides a Bragg grating, a preparation method thereof and a distributed feedback laser, and belongs to the technical field of semiconductor lasers. The Bragg grating is arranged in a distributed feedback laser. The Bragg grating comprises a lower grating waveguide layer, a middle grating waveguide layer and an upper grating waveguide layer which are sequentially formed and have different refractive indexes; the refractive index of the middle grating waveguide layer is lower than the refractive index of the lower grating waveguide layer and the refractive index of the upper grating waveguide layer; the doping types of the lower grating waveguide layer and the middle grating waveguide layer are the same; the doping type of the upper grating waveguide layer is opposite to the doping types of the adjacent layers, so that a reverse biased PN junction can be formed on the upper grating waveguide layer; a plurality of grooves are formed in the upper grating waveguide layer at intervals in the cavity length direction of the distributed feedback laser; and the grooves are filled with buried layers to flatten the upper grating waveguide layer. The coupling coefficient of the Bragg grating can be increased along with the increase of the current of the distributed feedback laser, so that the cavity loss of the distributed feedback laser is reduced, and the response bandwidthis expanded.
Owner:XIAMEN SANAN INTEGRATED CIRCUIT

Optical fiber pressure sensor based on micro ellipsoidal air cavity and manufacturing method thereof

The present invention relates to an optical fiber pressure sensor based on a micro ellipsoidal air cavity and a manufacturing method of an optical fiber pressure sensor based on a micro ellipsoidal air cavity, belonging to the technical field of optical fiber pressure sensors. The optical fiber pressure sensor comprises a single-mode optical fiber and a pressure-sensitive film; the upper end of the single-mode optical fiber is fixedly connected with the lower end of the pressure-sensitive film; and the single-mode optical fiber and the pressure-sensitive film are connected with an air Fabry-Perot cavity. The materials of the optical fiber pressure sensor are silicon dioxide, so that the thermal expansion coefficients of the optical fiber pressure sensor are the same, thereby avoiding structural failure due to high temperature mismatch of different materials and achieving small temperature crosstalk and low cost. The manufacturing process of the sensor head only needs welding, cutting and grinding, and the process is simple; the confocal Fabry-Perot cavity in the device has the advantages of small interference cavity loss and high interference fringe contrast ratio and high demodulation precision compared with the Fabry-Perot cavity made by the etching process or the femtosecond laser in the prior art.
Owner:NANJING UNIV OF INFORMATION SCI & TECH
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