发明名称 DOUBLE-FLOW TURBOJET ENGINE WITH THE INTERMEDIATE JACKET, WITH THE DRIVE SHAFT OF TRANSFER GEARBOX FOR TURBOJET ENGINE ACCESSORY DRIVE
摘要 FIELD: turbojet engine. ^ SUBSTANCE: double-flow turbojet engine contains the intermediate jacket, with installed drive shaft of transfer gearbox in its radial arm designed to auxiliary drives. The drive shaft of output transfer gearbox is connected on its first end with the mechanical transfer mechanism placed on the drive shaft of the turbojet engine, and on the second end with the mechanical transmission to the abovementioned gearbox. The drive shaft of output transfer gearbox has a conic gearwheel between two ends of this shaft and allows providing mechanical linkage with additional auxiliary equipment. The drive shaft of output transfer gearbox in combination with the abovementioned gearwheel is encased forming an oil circuit, sealed in relation to the radial arm. ^ EFFECT: allows limiting a inflammable area at the expense oil leak elimination. ^ 16 cl, 6 dwg
申请公布号 RU2442000(C2) 申请公布日期 2012.02.10
申请号 RU20070137998 申请日期 2007.10.12
申请人 SNEKMA 发明人 SHAR'E ZHIL' ALEN;MOREL' PATRIK SHARL' ZHORZH;SERVAN REZHI EHZHEN ANRI
分类号 F01D25/18;F02C7/32 主分类号 F01D25/18
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