发明名称 STRUCTURE OF NOZZLE OF ROCKET
摘要 PURPOSE:To prevent damage due to the heat of a flexible joint from occurring, by making the maximum external diameter of a radiation shielder smaller than an inner diameter of an insertion hole by providing a shield part on an insulator of a motor case. CONSTITUTION:An insulator 5 is provided on the inside of a motor case 1. A nozzle 25 is provided on the tip of a flexible joint 6. A shield part 42 extending inward in a radiation direction is provided on the insulator 5. An inside edge of a radiation direction of a shield part 42 is positioned inward in a radiation direction of a radiation shielder 16 by a distance l from its extreme point. The maximum external diameter D of the radiation shielder 16 is made smaller than an inner diameter (d) of an insertion hole 2. Swing of the nozzle 25 can be performed without damaging the flexible joint 6 through heat in this manner. In addition to the above, incorporating work and replacing work are facilitated.
申请公布号 JPS5968546(A) 申请公布日期 1984.04.18
申请号 JP19820180484 申请日期 1982.10.13
申请人 NISSAN JIDOSHA KK 发明人 TANIGUCHI RIYUUICHI
分类号 F02K9/84;(IPC1-7):02K9/84 主分类号 F02K9/84
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