公开(公告)号：WO1992007180A1

公开(公告)日：1992-04-30

申请号：PCT/US1991005794

申请日：1991-08-15

Applicant: SUNDSTRAND CORPORATION

Inventor： SUNDSTRAND CORPORATION ,  VESSA, Phillip ,  GARCIA, Jesus, Aguilar

IPC: F02G03/00

CPC classification number: F01D21/045

Abstract: In order to avoid penetration of the housing (38) of a gas turbine (10) in the event of burst failure, the gas turbine (10) includes a containment ring system (32). The gas turbine (10) is of the type which includes a rotor (12) having a turbine wheel (14) with blades (16) and a nozzle (18) outwardly of the turbine blades (16). The nozzle (18) is adapted to direct hot gases at the turbine blades (16) to cause rotation of the rotor (12). The gas turbine (10) is also of the type having an annular combustor (20) about the rotor (12) along with an outlet (22) to the nozzle (18). The annular combustor (20) is defined by spaced inner and outer walls (24 and 26) connected by a generally radially extending wall (28). With this arrangement, the gas turbine (10) utilizes a radial turbine containment ring system (32) which has a first containment ring (34) outwardly of the rotor (12) and the nozzle (18) and a second containment ring (36) at least partially about the rotor (12) outwardly of the turbine blades (16) to deflect fragments toward the first containment ring (34) while dissipating fragment energy in the event of burst failure.

Abstract translation: 为了避免在爆裂故障的情况下燃气轮机（10）的壳体（38）的穿透，燃气轮机（10）包括容纳环系统（32）。 燃气轮机（10）是包括具有叶片（16）的涡轮机叶轮（14）和涡轮机叶片（16）外侧的喷嘴（18）的转子（12）的类型。 喷嘴（18）适于引导涡轮叶片（16）处的热气体引起转子（12）的旋转。 燃气轮机（10）也具有围绕转子（12）的环形燃烧器（20）以及与喷嘴（18）的出口（22）的类型。 环形燃烧器（20）由通过大致径向延伸的壁（28）连接的间隔开的内壁和外壁（24和26）限定。 利用这种布置，燃气轮机（10）利用径向涡轮机容纳环系统（32），其具有位于转子（12）和喷嘴（18）外部的第一容纳环（34）和第二容纳环（36） 至少部分地围绕所述涡轮机叶片（16）向外的所述转子（12），以使碎片朝向所述第一容纳环（34）偏转，同时在爆裂故障的情况下消散碎片能量。