发明名称 GAS TURBINE MOVING VANE
摘要 PURPOSE:To effectively cool the whole vane while decreasing thermal stress, by forming a portion, which must be cooled, of this turbine moving vane by an aggregate manufactured by bundling thin tubes while opening cooling passages to a web portion and the back of the vane. CONSTITUTION:A vane portion except a dovetail 3 of this moving vane 2 is molded by means of an aggregate produced by bundling thin tubes 7 molded by heat-proof materials, and is root portion is fixed to a platform 8. Each thin tube 7 is opened 11 to a header 9 mounted to the inside of the dovetail. Meanwhile, the other ends of each thin tube 7 are opened 12 to the surfaces of the vane of a web portion, the back, etc. by working a flank and a nose portion of the aggregate in vane-like shapes after welding each thin tube 7 because the B-B sectional area of the vane contracts toward the direction that its radius becomes larger. Thus, air introduced into the dovetail 3 through a disc 1 is distributed to a passage 13 by means of the header 9, uniformly cools the vane while flowing out from openings 12, and forms air films.
申请公布号 JPS5532915(A) 申请公布日期 1980.03.07
申请号 JP19780102909 申请日期 1978.08.25
申请人 HITACHI LTD 发明人 MATSUMOTO MANABU;SAKAMOTO TAKESHI;ANZAI SHIYUNICHI;KOBAYASHI SHIGEYOSHI
分类号 F01D5/14;F01D5/18 主分类号 F01D5/14
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