| 摘要 |
The module has two consecutive stages of turbine wheel separated by annular distributors inside a casing (120). The distributors comprise several units (114A) provided in the form of a ring sector and are wedged inside the casing by an axial hook (121A) integrated to the casing or to the units (114A). The units (114A) cooperate with a pair of axial hooks (113A1, 113A2) integrated to the units (114A) or to the casing respectively. An independent claim is also included for a gas turbine engine comprising a low pressure turbine module. |
