Bottom thermal protecting and thermal sealing structure for tail section of guided missile

The invention provides a bottom thermal protecting and thermal sealing structure for a tail section of a guided missile. The structure comprises an annular laminated high silica/ phenolic aldehyde heatproof plate, a metal-based flexible graphite seal ring and an annular metal bottom plate; the inner...

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Bibliographische Detailangaben
Hauptverfasser: LIANG ZUDIAN, LEI BAO, XU JUNWEI, LIU JUNYI, CHEN SONG, ZHANG HAO, SHI HANG, YU HE, LIU XIAOMING, LI XINTIAN, CHEN SHILI, SHAN YIJIAO, XIA YAN, CHEN HAO, LU XIN, CHEN XINMIN, YIN LIZHONG, CHEN ZENGKUI, FAN XINZHONG, WANG YURUI, WEI HEYI
Format: Patent
Sprache:chi ; eng
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Beschreibung
Zusammenfassung:The invention provides a bottom thermal protecting and thermal sealing structure for a tail section of a guided missile. The structure comprises an annular laminated high silica/ phenolic aldehyde heatproof plate, a metal-based flexible graphite seal ring and an annular metal bottom plate; the inner section of the annular metal bottom plate is step-like; the annular metal bottom plate is fixedly connected to the annular laminated high silica/ phenolic aldehyde heatproof plate to form an annular groove inside; the metal-based flexible graphite seal ring is spliced by an annular plane and an annular wall surface, wherein the annular section thereof is in a shape of a formula, the annular plane of the metal-based flexible graphite seal ring is embedded into the annular groove, the annular wall surface, vertical to the annular plane, of the metal-based flexible graphite seal ring extends toward the annular metal bottom plate, the annular metal bottom plate is fixedly mounted on a bottom metal shell of the tail se