| 摘要 |
<p>PROBLEM TO BE SOLVED: To decrease the number of elements necessary for fixing and centering of guide blade supports so as to realize a compact configuration of a turbomachine.SOLUTION: Provided is a turbomachine (1), particularly gas turbine, including: a stator-side housing (2); a plurality of stator-side guide blade supports (21, 18) fixed to the housing (2); stator-side guide blades (5, 19) fixed to the guide blade supports (21, 18) while forming guide blade rings (35, 36) separated axially; and a rotor carrying a plurality of rotor blades. At least two guide blade supports (21, 18) are both fixed to a flange (22) of the housing (2) and subjected to centering.</p> |
