GAS TURBINE STATOR BLADE AND GAS TURBINE

• Main Authors: MIZUKAMI, Satoshi, MATSUO, Saki, MIYAHISA, Yasuo
• Format: Patent
• Language: English; French; Japanese
• Published: 04.01.2024
• Subjects: AIR INTAKES FOR JET-PROPULSION PLANTS; BLASTING; COMBUSTION ENGINES; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS; ENGINE PLANTS IN GENERAL; GAS-TURBINE PLANTS; HEATING; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS; LIGHTING; MACHINES OR ENGINES IN GENERAL; MECHANICAL ENGINEERING; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES; STEAM ENGINES; WEAPONS

This gas turbine stator blade is provided with: a leading edge part partition that divides a cavity inside the blade into a leading edge side cavity and a trailing edge side cavity; a negative pressure surface side partition wall that is integrally formed with a blade body, divides the leading edge...