Probabilistic Lifetime Prediction of Thermal Barrier Coating Systems Depending on Manufacturing Scatter

Author(s):  
Hans-Peter Bossmann ◽  
Thomas Duda ◽  
Joerg Krueckels ◽  
Sebastian Mihm ◽  
Roland Mücke ◽  
...  

The assessment of Bondcoat/Thermal barrier coating systems is an inherent part of the lifing process of gas turbine component. On the one hand, coatings are considered in the constitutive modelling — e.g. in the thermal model and for the prediction of eigenfrequencies of gas turbine blades. On the other hand, the influence of the coating system on the lifetime of the part (target cyclic life and target operation hours) needs to be assessed. This paper addresses the prediction of coating lifetime. Lifing models of Bondcoat/Thermal barrier coating systems (BC/TBC) are commonly built using isothermal furnace cyclic tests (FCT). The lifetime of the BC/TBC under such test conditions has been shown to depend on multiple coating parameters like TBC thickness, TBC porosity, BC thickness, BC roughness, and also on testing temperature. For example, the TBC life (defined as time to partial TBC spallation) is reduced with increasing temperature, with increasing TBC thickness and decreasing porosity and BC roughness. When operating in a gas turbine (GT), the TBC surface temperature and the BC temperature depend on engine operating conditions, heat transfer of combustion gas and cooling air, coating microstructure and thickness. For instance, a TBC with high porosity typically demonstrates a lower thermal conductivity than that with low porosity. For otherwise same boundary conditions, the BC temperature will decrease with increasing TBC porosity and increasing TBC thickness. The benefit of having a high coating porosity observed in FCT is further amplified by its impact on reducing the BC temperature in GT operation. To the contrary, the positive impact of a reduced TBC thickness observed in FCT is reduced by its negative impact on an increased BC temperature during GT operation. Taking these effects into account a probabilistic lifing model is proposed based on Monte Carlo simulations. Using this model the impact of the manufacturing scatter on the BC/TBC life can be assessed, and enables improved manufacturing by focusing on those parameters that are most critical for coating lifetime.

2019 ◽  
Vol 11 ◽  
pp. 912-919 ◽  
Author(s):  
Vishnu Sankar ◽  
PB. Ramkumar ◽  
Deepak Sebastian ◽  
Doyel Joseph ◽  
Jithu Jose ◽  
...  

JOM ◽  
2015 ◽  
Vol 67 (7) ◽  
pp. 1528-1539 ◽  
Author(s):  
Albert Manero ◽  
Stephen Sofronsky ◽  
Kevin Knipe ◽  
Carla Meid ◽  
Janine Wischek ◽  
...  

2019 ◽  
pp. 146808741989348 ◽  
Author(s):  
Eric Gingrich ◽  
Michael Tess ◽  
Vamshi Korivi ◽  
Peter Schihl ◽  
John Saputo ◽  
...  

Thermal barrier coatings of various thickness and surface roughness were applied to the piston crown of a single-cylinder research engine and tested over a range of high-output diesel operating conditions, some near 30 bar gross indicated mean effective pressure. Three yttria-stabilized zirconia coated pistons were compared to a baseline metal piston. At each operating condition, a start-of-injection sweep was conducted to generate efficiency trends and find the optimal combustion phasing. Three variations of pistons coated with a graded-layer thermal barrier coating were tested: (1) 0.185 mm coating thickness with a surface roughness of approximately Ra = 11.8 µm, (2) 0.325 mm thickness with Ra = 11.8 µm, and (3) 0.325 mm thickness with Ra = 6.0 µm. Both coated pistons with Ra = 11.8 µm did not show any statistically significant improvement to engine performance when compared to the metal baseline piston, but did produce higher filter smoke numbers. The coated piston with Ra = 6.0 µm and 0.325 mm showed an increase of gross indicated thermal efficiency of up to 3.5% (relative) compared to the metal baseline piston for operating conditions comparable to standard engine operation and a reduction of filter smoke number back to the metal baseline. The increase in efficiency was found to correlate with additional late-cycle apparent heat release and a reduction in in-cylinder heat transfer. The very high-output conditions showed statistically insignificant changes in performance or heat transfer, which may have been related to the long injection duration used for these cases targeting outside of the piston bowl.


Author(s):  
Stephanie A. Wimmer ◽  
Virginia G. DeGiorgi ◽  
Edward Gorzkowski ◽  
Scooter Johnson

Thermal barrier coatings are used to reduce base metal temperature and can be found on many engine components such as turbine blades and exhausts. The presented work is part of a broader effort which is focused on maintaining mechanical properties while improving thermal properties of candidate thermal barrier coating materials. Specifically this effort is investigating new and novel processing techniques to improve thermal properties while maintaining sufficient mechanical properties so that coatings do not fail due to the loads inherent to normal operation of the component. Processing methods have been investigated that create new microstructures by the inclusion of spherical, micron size pores to reflect radiation (i.e. heat) at high temperatures providing additional thermal protection while maintaining strength. This paper computationally examines the size, distribution, and structure of pores that develop during bulk processing of a model material, yttria-stabilized zirconia (YSZ) to aid in the formulation of an optimized process. Heat transfer and stress-displacement analyses are performed to determine effective bulk material properties. Two-dimensional microstructures are the first step towards understanding the impact of pores, voids and microcracks on thermal and mechanical characteristics. In this work two-dimensional microstructures are computer generated to determine the influence on variations in pore number, size and relative percent of pores and cracks. Comparisons are made to experimental measurements when appropriate.


2016 ◽  
Vol 2 (2) ◽  
pp. 273-278
Author(s):  
Yongchan Jung ◽  
Mintae Kim ◽  
Juhyeung Lee ◽  
Jamin Ahn ◽  
Kihong Kim

Materials ◽  
2021 ◽  
Vol 14 (15) ◽  
pp. 4214
Author(s):  
Kranthi Kumar Maniam ◽  
Shiladitya Paul

The increased demand for high performance gas turbine engines has resulted in a continuous search for new base materials and coatings. With the significant developments in nickel-based superalloys, the quest for developments related to thermal barrier coating (TBC) systems is increasing rapidly and is considered a key area of research. Of key importance are the processing routes that can provide the required coating properties when applied on engine components with complex shapes, such as turbine vanes, blades, etc. Despite significant research and development in the coating systems, the scope of electrodeposition as a potential alternative to the conventional methods of producing bond coats has only been realised to a limited extent. Additionally, their effectiveness in prolonging the alloys’ lifetime is not well understood. This review summarises the work on electrodeposition as a coating development method for application in high temperature alloys for gas turbine engines and discusses the progress in the coatings that combine electrodeposition and other processes to achieve desired bond coats. The overall aim of this review is to emphasise the role of electrodeposition as a potential cost-effective alternative to produce bond coats. Besides, the developments in the electrodeposition of aluminium from ionic liquids for potential applications in gas turbines and the nuclear sector, as well as cost considerations and future challenges, are reviewed with the crucial raw materials’ current and future savings scenarios in mind.


2000 ◽  
Vol 66 (650) ◽  
pp. 1841-1846
Author(s):  
Hiroshige ITOH ◽  
Kazuhiro SAITOH ◽  
Takahiro KUBO ◽  
Masashi TAKAHASHI ◽  
Hideo KASHIWAYA

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