Highly loaded turbine blading
AssigneeAsea Brown Boveri AG
InventorsRalf Greim, Said Havakechian, Harald Romer, Peter Szincsak
Life of this patent
Estimating the term…
Loading patent…
AssigneeAsea Brown Boveri AG
InventorsRalf Greim, Said Havakechian, Harald Romer, Peter Szincsak
Estimating the term…
To reduce the number of stages of a turbine and, associated therewith, the overall length and the costs, blading having high stage-specific enthalpy transfer is to be used. In this case, the disadvantages of conventional highly loaded blading, such as increased secondary flow losses due to blades of large chord length and comparatively small height and the design of the turbine in the complicated chamber type of construction, are to be avoided. Resulting from these requirements is a highly loaded slim blade type of construction having considerable deflection. A turbine having blading according to the invention is characterized by a loading parameter RBL, which in the HRBL blading according to the invention, in contrast to conventional types of construction, is greater than 1.
A turbine having at least one essentially axial-flow stage, which stage consists of a guide-blade row (LE) and a moving-blade row (LA), which are accommodated in a common casing (30) , which casing has at least one inflow section (31) and at least one outflow section (32), and furthermore the degree of reaction of a stage being greater than 0.15, wherein, for a turbine part which lies between an inflow section (31) and an outflow section (32) of the casing (30), for the essentially axial-flow blade rows (LE, LA), the ratio of their axial chord length (sax) to their height (h) is selected in such a way that a characteristic factor RBL is greater than 1, RBL being defined by RBL = 1.1 · π · 10 - 15 · P 2 · p _ 4 z 8 · m . 6 · N 8 · ∑ i = 1 2 · z h i 8 D M , i 2 · s ax , i 6
Dependencies are inferred from the claim text.