| 摘要 |
<p>There is described a base frame (4) for a gas turbine (1) and optional driven machinery (2, 3) such as generators and the like, which base frame (4) includes a centrally arranged hollow section (8) which acts as a torsion-absorbing body, sections or wings (9) which extend from the hollow section (8) and form an angle of approximately 90° with the longitudinal axis of the hollow profile (8), one or more plate-shaped bodies (10, 11, 12) arranged to cover wholly or partly the hollow section (8) and the sections (9), wherein between the plate-shaped bodies (10, 11, 12), the sections (9) and the hollow section (8) there is formed at least one chamber (13) on each side of the longitudinal axis of the hollow section (8), in which chambers (13) there are provided pull-out modules (15) which can house operating and control systems for the gas turbine (1), and that the hollow section (8) is in the form of a hollow section having a rectangular, preferably square cross section.</p> |
