• Chinese Journal of Lasers
  • Vol. 47, Issue 6, 601005 (2020)
Liu Jianning*, Bian Xiaoyun, Weng Jun, and Jiao Mingxing
Author Affiliations
  • School of Mechanical and Precision Instrument Engineering, Xi''an University of Technology,Xi''an, Shaanxi, 710048, China
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    DOI: 10.3788/CJL202047.0601005 Cite this Article Set citation alerts
    Liu Jianning, Bian Xiaoyun, Weng Jun, Jiao Mingxing. Temperature Segment Frequency Stabilization Control Technology in Prisms Laser Gyroscope[J]. Chinese Journal of Lasers, 2020, 47(6): 601005 Copy Citation Text show less
    Simplified structure of TRPLG
    Fig. 1. Simplified structure of TRPLG
    Simplified structure diagram of heater
    Fig. 2. Simplified structure diagram of heater
    Meshing division of finite element model
    Fig. 3. Meshing division of finite element model
    Temperature distributions of ring resonator and frequency stabilization gas channel with temperature from -25 ℃ to 70 ℃. (a) Isogram; (b) curves
    Fig. 4. Temperature distributions of ring resonator and frequency stabilization gas channel with temperature from -25 ℃ to 70 ℃. (a) Isogram; (b) curves
    Temperature distributions of ring resonator and frequency stabilization gas channel with temperature from -70 ℃ to 25 ℃. (a) Isogram; (b) curves
    Fig. 5. Temperature distributions of ring resonator and frequency stabilization gas channel with temperature from -70 ℃ to 25 ℃. (a) Isogram; (b) curves
    Fitting curves of temperature of frequency stabilization gas center and time. (a) 25 ℃→70 ℃; (b) 70 ℃→25 ℃
    Fig. 6. Fitting curves of temperature of frequency stabilization gas center and time. (a) 25 ℃→70 ℃; (b) 70 ℃→25 ℃
    Test device diagram of variable temperature experiment
    Fig. 7. Test device diagram of variable temperature experiment
    MaterialThermal conductivity /(W·m-1·℃1)Specific heat capacity C /(J·kg-1·℃-1)Density ρ /(kg·m-3)
    Glass-ceramic1.468002530
    Dry air262.47201.199
    Table 1. Thermodynamic parameters of materials involved in finite element analysis
    Temperature range /℃Temperature rise and fall process [y=aexp(bx)+cexp(dx)]Insulation process [y=aexp(bx)]
    abcdab
    25→7059.67-9.25×10-5-59.91-0.0004122.7-0.00056
    70→25-59.67-9.25×10-559.91-0.0004-122.7-0.00056
    25→-40-35.77-8.89×10-636.10-0.00055-270.6-0.00056
    -40→2535.77-8.89×10-6-36.10-0.00055-270.6-0.00056
    Table 2. Fitting curve coefficients of temperature difference between inner and outer of cavity and time
    Temperature range /℃Gyroscop numberGyroscope accuracy controlled by old program /[(°)·h-1]Gyroscope accuracy controlled by temperature segment /[(°)·h-1]
    1#0.01120.0110
    25→702#0.01220.0120
    3#0.01150.0101
    1#0.01530.0112
    70→252#0.01720.0168
    3#0.01590.0135
    1#0.02170.0187
    25→-402#0.02380.0229
    3#0.02810.0253
    1#0.03100.0211
    -40→252#0.02890.0206
    3#0.03090.0176
    Table 3. Comparison of gyroscope accuracy under different frequency stabilization control methods
    Liu Jianning, Bian Xiaoyun, Weng Jun, Jiao Mingxing. Temperature Segment Frequency Stabilization Control Technology in Prisms Laser Gyroscope[J]. Chinese Journal of Lasers, 2020, 47(6): 601005
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