Simulation Analysis on the Profile Accuracy of High Precision Carbon Fiber Composite (CFC) Reflector Antenna
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1.Shanghai Composite Material Science & Technology Co., Shanghai 201112;2.Shanghai Engineering Technology & Research Center of Aerospace Resin Based Composites,Shanghai 201112;3.Collaborative Innovation Center For Civil Aviation Composite Materials of Donghua University,Shanghai 201620

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V46

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    Abstract:

    The influence of the outer skin assembly deviation, self-weight, forming and service temperature difference on the profile accuracy especially the R.M.S value of reflector working face is specially analyzed. The results show that through 0.5mm assembly offset of the outer skin, the reflector working face theoretical R.M.S value changes 0.47μm. Under the forming and placing condition, the 11kg self-weight has 0.55 μm deviation on the theoretical R.M.S value of the reflector working face. The temperature difference of it between the forming and service the reflector brings 17.79μm change of the theoretical R.M.S value.

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History
  • Received:September 17,2021
  • Revised:November 12,2021
  • Adopted:November 16,2021
  • Online: December 23,2022
  • Published: December 30,2022