The Control of Hot Corrosion in Marine Gas Turbines

1981 ◽  
Vol 103 (1) ◽  
pp. 188-197 ◽  
Author(s):  
J. F. G. Conde´ ◽  
C. G. McCreath

Ingestion of sea salt and sulphur from fuel can lead to aggressive environments in gas turbines operating in marine conditions resulting in corrosion damage to hot end components, even in well-filtered engines. The nature of the environment in the engine and the factors which influence this are indicated. The chemistry of salt contaminant particles in the engine and combustion environments and temperature levels prevailing in naval engines are described in relation to the normal operating profile and the incidence of corrosion effects in relation to temperature. Results of rig evaluation of materials and coatings are given. Erosion resistance, the combined effects of erosion/corrosion and the mechanisms of hot corrosion are discussed together with the effects of material composition and the use of inhibition as a control procedure. The effects of a salt environment on the creep and stress-rupture behavior of superalloys are covered briefly.

Author(s):  
J. F. G. Condé ◽  
C. G. McCreath

Ingestion of sea salt and sulphur from fuel can lead to aggressive environments in gas turbines operating in marine conditions resulting in corrosion damage to hot end components, even in well-filtered engines. The nature of the environment in the engine and the factors which influence this are indicated. The chemistry of salt contaminant particles in the engine and combustion environments and temperature levels prevailing in naval engines are described in relation to the normal operating profile and the incidence of corrosion effects in relation to temperature. Results of rig evaluation of materials and coatings are given. Erosion resistance, the combined effects of erosion/corrosion and the mechanisms of hot corrosion are discussed together with the effects of material composition and the use of inhibition as a control procedure. The effects of a salt environment on the creep and stress-rupture behavior of superalloys are covered briefly.


Author(s):  
Dipankar Dua ◽  
Mohammad Khajavi ◽  
Gary White ◽  
Deepak Thirumurthy ◽  
Jaskirat Singh

Abstract Siemens Energy has a large fleet of aero-derivative gas turbines. The performance and durability of these power turbines largely depend on the capability of hot section components to resist high-temperature surface attacks and to maintain their mechanical properties. Hot corrosion attack occurs due to exposure of turbine components to sulfur-bearing fuels/air together with other corrosive compounds during turbine operation. This paper investigates the impact of low-temperature hot corrosion on the stress rupture of commonly used gas turbine disk alloys, including Inconel 718, Incoloy 901, and A-286. The results indicate that Inconel 718 and Incoloy 901 maintain their creep strength advantage over A-286 in a low-temperature hot corrosion inducing environment at 1100°F. All three materials exhibited an equivalent life reduction in the corrosive environments at 1100°F. Moreover, the results demonstrate that the stress-rupture life of materials in hot-corrosion environments depends on the combined and cumulative effects of corrosion-resistant and hardening elements.


JOM ◽  
1951 ◽  
Vol 3 (10) ◽  
pp. 909-916 ◽  
Author(s):  
Italo S. Servi ◽  
Nicholas J. Grant

1994 ◽  
Vol 77 (5) ◽  
pp. 1235-1241 ◽  
Author(s):  
Mamballykalathil N. Menon ◽  
Ho T. Fang ◽  
David C. Wu ◽  
Michael G. Jenkins ◽  
Mattison K. Ferber

1994 ◽  
Vol 77 (5) ◽  
pp. 1217-1227 ◽  
Author(s):  
Mamballykalathil N. Menon ◽  
Ho T. Fang ◽  
David C. Wu ◽  
Michael G. Jenkins ◽  
Mattison K. Ferber ◽  
...  

1992 ◽  
Vol 288 ◽  
Author(s):  
Wego Wang ◽  
Li-Tusng Chien

Author(s):  
J. T. Hageboeck ◽  
W. S. Roberts

A new modification of an economical casting material is presented for use in the intermediate temperature range, which is considered to be 800 to 1300 F. An illustration is given of two large castings actually produced for the 1500-hp ATAC regenerative gas turbines engine. Comparisons are made with other materials, giving information stress-rupture at various temperature levels and some cost information. Also included are design suggestions for better utilization of foundry techniques.


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