发明名称 |
MOVING BLADE OF GAS-TURBINE ENGINE TURBINE |
摘要 |
FIELD: machine building.SUBSTANCE: moving blade of a gas turbine engine turbine comprises an upper end platform with labyrinth seal teeth being set on it. The platform is fitted by a through hole for cooling air and is made as a parallelogram with two sides of the latter being oriented in the rotation direction and the other two being fitted by oppositely directed cuts with contact surfaces and strain compensators embracing them. The platform is equipped by support and control ribs. The support rib is set between the strain compensators with the length of (0.7 - 0.9)H and at the distance of (0.1 - 0.9)L from the cut vertex. The control rib is provided on the side edge of the platform on the side of the convex surface of the profile part between the strain compensator and the labyrinth seal tooth with the height of (0.7 - 0.85)h of the seal tooth height. The height of the strain compensators and the support rib respectively amounts to (1 - 2)d and (1.5 - 3)d, where H stands for the distance between the strain compensators; L - distance from the cut vertex to the rear side of the platform oriented in the rotation direction; h - seal tooth height; d - platform thickness.EFFECT: longer service life of engine turbine blade at keeping the necessary air consumption via the cooling system for a moving blade and insignificant increase of weight.3 cl, 5 dwg |
申请公布号 |
RU2529273(C1) |
申请公布日期 |
2014.09.27 |
申请号 |
RU20130141515 |
申请日期 |
2013.09.11 |
申请人 |
OTKRYTOE AKTSIONERNOE OBSHCHESTVO "UFIMSKOE MOTOROSTROITEL'NOE PROIZVODSTVENNOE OB"EDINENIE" OAO "UMPO";OTKRYTOE AKTSIONERNOE OBSHCHESTVO "AVIATSIONNAJA KHOLDINGOVAJA KOMPANIJA SUKHOJ" |
发明人 |
KONONOV NIKOLAJ ALEKSANDROVICH;KRYLOV NIKOLAJ VLADIMIROVICH;MARKOVICHEV DMITRIJ SERGEEVICH;SHCHERBAKOV MIKHAIL ALEKSANDROVICH |
分类号 |
F01D5/20;F01D5/18 |
主分类号 |
F01D5/20 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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