BLADE

The invention relates to a blade and particularly, the blade for a gas turbine includes a root (2), a platform (3) and an airfoil (4). The blade (1) further has a cooling channel (5) with an inlet (6) located at the root (2) or platform (3) and outlets (7). The outlets (7) are located at the platfor...

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Bibliographic Details
Main Authors SHAILENDRA NAIK, IVAN LUKETIC
Format Patent
LanguageChinese
English
Published 16.11.2016
Subjects
BLASTING
ENGINE PLANTS IN GENERAL
HEATING
INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS
INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
STEAM ENGINES
WEAPONS
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Summary:The invention relates to a blade and particularly, the blade for a gas turbine includes a root (2), a platform (3) and an airfoil (4). The blade (1) further has a cooling channel (5) with an inlet (6) located at the root (2) or platform (3) and outlets (7). The outlets (7) are located at the platform (3). 本发明涉及叶片，更具体地涉及种用于燃气轮机的叶片（1）；该叶片（1）包括根部（2）、平台（3）和翼型部（4）。叶片（1）还具有冷却通道（5）；该冷却通道（5）具有位于根部（2）或平台（3）处的个进口（6）并具有出口（7）。出口（7）位于平台（3）处。
Bibliography:Application Number: CN20161299814