✦ LIBER ✦

Design and Properties of Thermal Barrier Coatings for advanced turbine engines

✍ Scribed by Dr. M. Peters; Dr. K. Fritscher; Dr. G. Staniek; Dr. W. A. Kaysser; Dr. U. Schulz

Publisher: John Wiley and Sons
Year: 1997
Tongue: English
Weight: 712 KB
Volume: 28
Category: Article
ISSN: 0933-5137
DOI: 10.1002/mawe.19970280807

No coin nor oath required. For personal study only.

✦ Synopsis

Abstract

The efficiency and performance of advanced aircraft turbines can be markedly increased if higher gas temperatures are used. Although the highly loaded blades and vanes in the high pressure turbine are heavily cooled, today's substrate materials are unable to provide sufficient strength in the temperature range up to 1500°C and above. If thermal barrier coatings (TBCs) are applied on superalloy turbine blades a substantial temperature drop of the parts can be achieved. The resulting increase in efficiency comes from reduced cooling and/or increased gas turbine inlet temperatures of up to 150°C. TBCs are either processed by plasma spraying (PS) or electron beam physical vapour deposition (EB‐PVD). While PS is lower in cost EB‐PVD leads to superior strain and thermoshock tolerant coatings. Furthermore, cooling hole closure of turbine blades and vanes is prevented and aerodynamic design maintained. Finally, future research and development needs in TBC technology are stressed.

📜 SIMILAR VOLUMES

EB-PVD Thermal Barrier Coatings for Aero

EB-PVD Thermal Barrier Coatings for Aeroengines and Gas Turbines

✍ M. Peters; C. Leyens; U. Schulz; W. A. Kaysser 📂 Article 📅 2001 🏛 John Wiley and Sons 🌐 English ⚖ 706 KB

where his activities concentrated on weldable Ti alloys and advanced Al alloys. 1982 he joined DLR's Institute of Materials Research in Köln, where he worked as group leader on Al±Li alloys and high temperature titanium alloys. 1988 he became section head ªLight Metals and Coatingsº. Presently he is

Fatigue Testing of Ceramic Thermal Barri

Fatigue Testing of Ceramic Thermal Barrier Coatings for Gas Turbine Blades

✍ M. Bartsch; G. Marci; K. Mull; C. Sick 📂 Article 📅 1999 🏛 John Wiley and Sons 🌐 English ⚖ 173 KB 👁 1 views

ChemInform Abstract: Concept of Function

ChemInform Abstract: Concept of Functionally Graded Materials for Advanced Thermal Barrier Coating Applications

✍ W. Y. LEE; D. P. STINTON; C. C. BERNDT; F. ERDOGAN; Y.-D. LEE; Z. MUTASIM 📂 Article 📅 2010 🏛 John Wiley and Sons ⚖ 25 KB 👁 1 views

A Novel Strategy for the Design of Advan

A Novel Strategy for the Design of Advanced Engineering Alloys—Strengthening Turbine Disk Superalloys via Twinning Structures

✍ Yong Yuan; Yuefeng Gu; Chuanyong Cui; Toshio Osada; Tadaharu Yokokawa; Hiroshi H 📂 Article 📅 2010 🏛 John Wiley and Sons 🌐 English ⚖ 574 KB

Structural Evolution and Mechanical Prop

Structural Evolution and Mechanical Properties Modification of MELTPRO (in Situ Remelted) Processed Thermal Barrier Coatings during Thermal Shocks

✍ G. Antou; G. Montavon; F. Hlawka; C. Coddet; A. Cornet 📂 Article 📅 2006 🏛 John Wiley and Sons 🌐 English ⚖ 563 KB

Thermal Barrier Coatings (TBCs) are used extensively to protect components of gas turbines or diesel engines against deterioration at high temperatures, oxidation and corrosion attack by reactive species, especially sulfurs. A TBC can be manufactured by implementing atmospheric plasma spraying (APS)

Improvement of the Adherence of Thermal

Improvement of the Adherence of Thermal Barrier Coatings for Rocket Combustion Chambers

✍ S. Beyer; D. Klemm; M. Bobeth; W. Pompe; O. Trommer; P. Gawlitza 📂 Article 📅 2005 🏛 John Wiley and Sons 🌐 English ⚖ 365 KB 👁 2 views

The improvement of the adherence of thermal barrier coatings on a copper material as used in rocket combustion chambers by introducing an additional Al or Ti reaction layer and by realizing an optimum surface roughness is presented. Boundary layer reactions of Al and Ti with the copper substrate hav