CENTRIFUGAL COMPRESSOR ANNULAR COMBUSTOR AND DIFFUSER ARRANGEMENT FOR A GAS TURBINE

• 1. 布置在一种燃气轮机的压缩机和燃烧室之间的扩散器 [P] . 中国专利： CN100390387C . 2008.05.28
• 2. 布置在一种燃气轮机的压缩机和燃烧室之间的扩散器 [P] . 中国专利： CN1836097A . 2006-09-20
• 3. Bi-centrifugal compressor assembly for turbine engine of helicopter, has compression stage, and diffuser joint that is coupled to compressor stage of centrifugal compressor via air return channel that is inclined upstream [P] . 法国专利： FR2970508A1 . 2012-07-20

  机译： 用于直升机涡轮发动机的双离心压缩机组件，具有压缩级和扩散器接头，该扩散器接头通过向上游倾斜的回风通道连接到离心压缩机的压缩机级

• 4. Can combustor for a can-annular combustor arrangement in a gas turbine [P] . 美国专利： US10422535B2 . 2019-09-24

  机译： 罐式燃烧器，用于燃气轮机中的罐式环形燃烧器

• 5. CAN-ANNULAR GAS TURBINE ENGINE COMBUSTOR ARRANGEMENT HAVING TANGENTIALLY ORIENTED COMBUSTOR CANS WITH RADIAL MIDFRAME BAFFLES [P] . 欧洲知识产权局专利： EP3044422B1 . 2018-06-27

  机译： 带有径向中间框的切向定向燃烧室罐的环形燃气轮机发动机燃烧室布置

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