Exhaust diffuser for a gas turbine, and method thereof
a technology of exhaust diffuser and gas turbine, which is applied in the direction of machines/engines, stators, liquid fuel engines, etc., can solve the problems of reducing the pressure recovery of the diffuser, and achieve the effects of increasing the elasticity of adjustment, increasing the geometric control, and increasing the accuracy
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[0026]Referring now to FIG. 1 is illustrated an exhaust diffuser assembly 1 (also referred to as “diffuser 1”) for a stationary gas turbine, for example, used in power generation and mechanical drives in land based applications. The diffuser 1 has an inlet 3 having a first cross-sectional area A1 for receiving a mainflow gas from a last stage of a turbine section 60. The gas 5 flows along a longitudinal axis 2 through a conduit defined by a diverging diffuser wall 7 extending from the diffuser inlet 3 to a diffuser outlet 4 having a second cross-sectional area A2. The diffuser outlet 4 directs the gas 5 to an exhaust duct 80.
[0027]The diffuser wall 7 serves to recover pressure from the gas by expanding the gas between the inlet 3 and the outlet 4. This reduces the total head loss of the gas, thereby increasing the work extracted from the gas 5. The diffuser wall 7 makes an angle of divergence ‘α’ with respect to the longitudinal axis 2. In conventional diffusers, the divergence angl...
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