GAS TURBINE

• Main Authors: SHIMMYO, Tetsuya, TORII, Shunsuke, IIDA, Koichiro, SATO, Kenji, TOKUYAMA, Kentaro, KITAGAWA, Hitoshi
• Format: Patent
• Language: English; French; Japanese
• Published: 07.02.2019
• 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

In this gas turbine, a first stage stationary blade (23A) and a first side wall portion (54A) and a second side wall portion (54B) of a combustor outlet satisfy one of the following conditions (a) and (b). If an axial direction from an upstream side to a downstream side is defined as an x-axis and a...