发明名称 Anti-vibration fairings for reservoirs on spacecraft launchers - using central fairings between two cylindrical reservoirs ring-clamped with spring-loaded tensioners and seal body fairings
摘要 The anti-vibration fairing carries two similar cylindrical accessories (20) on the spacecraft. Two end fairings are connected by central fairings (28,30a,30b), containing tensioning devices (34) for accessory clamps (32). At least three rings (32) clamp around each accessory, with tensioners (34) between these and adjacent accessories. The central fairing comprises two lateral deflectors (28), end fixed, with seals (58) against the spacecraft body. Complementary crossbeams (30a,30b) fasten by three tensioners (74), each with springing and a ring around the fastener. USE/ADVANTAGE - Space shuttle servo reservoirs, improving aerodynamics, rigidity and absorbing vibrations, with little weight penalty.
申请公布号 FR2691425(A1) 申请公布日期 1993.11.26
申请号 FR19920006368 申请日期 1992.05.25
申请人 AEROSPATIALE STE NATIONALE INDLE 发明人 DEMANGE CLAUDE
分类号 B64C7/00;B64G1/22;(IPC1-7):B64G1/22 主分类号 B64C7/00
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