Gamma Titanium Aluminide Alloys 2014 -  - E-Book

Gamma Titanium Aluminide Alloys 2014 E-Book

0,0
82,99 €

oder
-100%
Sammeln Sie Punkte in unserem Gutscheinprogramm und kaufen Sie E-Books und Hörbücher mit bis zu 100% Rabatt.

Mehr erfahren.
Beschreibung

This book is a collection of papers presented at the 4th International Symposium on Gamma TiAl Alloys (ISGTA 2014) that was held in conjunction with the 2014 Annual Meeting of The Minerals, Metals & Materials Society. Papers discuss and assess advances in application and implementation experience in current alloys, fundamental aspects in current gamma alloy materials technology, new processes development and assessment, and emerging new alloys, their potentials and limitations, and breakthroughs. Papers that originated in the panel discussion of the symposium are intended to help the scientific community realize the limitations of current alloys materials and processes and discuss possible solutions. Six topic areas selected for this purpose included: * Wrought-processed alloys: status, dilemmas and pathways to future * Cast alloys for aero engine applications: status, issues, and barriers to advances * Cast alloys for turbocharger wheels: status and barriers to widespread applications * Emerging new alloys: justification, potentials, status, and future * Novel processes: justification, potential vs. realization issues, and future * Future applications and realistic pathways to them

Sie lesen das E-Book in den Legimi-Apps auf:

Android
iOS
von Legimi
zertifizierten E-Readern

Seitenzahl: 572

Veröffentlichungsjahr: 2014

Bewertungen
0,0
0
0
0
0
0
Mehr Informationen
Mehr Informationen
Legimi prüft nicht, ob Rezensionen von Nutzern stammen, die den betreffenden Titel tatsächlich gekauft oder gelesen/gehört haben. Wir entfernen aber gefälschte Rezensionen.



Contents

Cover

Half Title page

Title page

Copyright page

Preface

Editors

Alloy Design and Development

Alloy Design Concepts for Wrought High Temperature TiAl Alloys

Abstract

Introduction

Effect of Nb addition in the phase transformation of TiAl alloy

Strengthening Mechanism in high temperature TiAl alloy

Deformation behavior and workability

Oxidation resistance and mechanical properties

Conclusion

Acknowledgement

References

Physical Metallurgy and Performance of the TNB and γ-Md Alloys

Abstract

Introduction

Constitution and Microstructure

Yield Stress and Ductility

Fracture Toughness

Creep

Fatigue

Processing

Conclusions

Acknowledgements

References

A Quarter Century Journey of Boron as a Grain Refiner in TiAl Alloys

Abstract

Introduction

Impact To TiAl Physical Metallurgy

Facilitating Fine-Grained Cast TiAl Alloys

Grain Refinement Mechanisms

Boron Effects In Wrought And Powder Alloys

Ductility Of Cast Alloys With Boron Addition

Remaining Issues

References

Composition Optimization of β-γ TiAl Alloys Containing High Niobium

Abstract

Introduction

Experimental

Results and discussion

Conclusions

Acknowledgement

References

Processing and Fabrication

Impact of ISM Crucible Tilting Process on Mould Filling and Yield of Near-net Shape TiAl Turbine Blades

Abstract

Introduction

Experimental

Results and Discussion

Conclusions

Acknowledgements

References

The Effect of Mould Pre-Heat Temperature and Casting Dimensions on the Reaction Between TiAl Alloy and the Zirconia Investment Casting Moulds

Abstract

Introduction

Experimental Procedure

Results and Discussion

Conclusion

Acknowledgements

Reference

Experimental Research on the Recycling Potential of Precision Cast γ-TiAl During Electroslag Remelting

Abstract

Introduction and Thermodynamics

Consolidation by VIM

Deoxidation by Electroslag Remelting

Vacuum Arc Remelting

Investment Casting

Summary

Outlook

References

Influence of the Slag Composition on the Fluorine Absorption in γ-TiAl During IESR

Abstract

Introduction

Experimental

Results

Conclusion

Outlook

References

Response of Melt Treatment on the Solidified Microstructure of Ti-48Al-2Cr-2Nb Alloy

Abstract

Introduction

Experimental

Results and Discussion

Conclusion

Acknowledgement

Reference

Recent Development and Optimization of Forging Process of High Nb-TiAl Alloy

Abstract

Introduction

State of Art of Forging Ti-45Al-8.5Nb-0.2W-0.2B-0.02Y Alloy

Dilemmas of the Existing Process

New Works in Forging Process

Summary

Acknowledgements

References

Fabrication of TiAl Alloys by Alternative Powder Methods

Abstract

1. Introduction

2. Alternative PM methods

3. Conclusions

4. References

Manufacturing and Properties of High Nb-TiAl Sheet Materials

Abstract

Introduction

Experimental

Results and discussion

Conclusion

Acknowledgement

References

Reaction Behavior During Heating of Multilayered Ti/Al Foils

Abstract

Introduction

Experimental

Results and Discussion

Conclusion

Acknowledgement

References

High Nb Content TiAl Alloys Specified to Cast Process

Abstract

Introduction

Experimental Procedures

Results and Discussion

Conclusions

Acknowledgements

References

Joining and Surface Protection

Electron Beam Joining of γ-Titanium Aluminide

Abstract

Introduction

Materials and experimental details

Results and Discussion

Summary and conclusions

References

Mechanical Properties and Microstructure of a TNM Alloy Protected by the Fluorine Effect and Coated with a Thermal Barrier

Abstract

Introduction

Experimental

Results and Discussion

Conclusions

Acknowledgement

References

Wear Protection for Turbine Blades Made of Titanium Aluminide

Abstract

Introduction

Wear phenomena at low pressure turbine blades

Behavior of titanium aluminid materials under different wear conditions

Wear protection

Conclusion

Acknowledgement

Literature

Effect of Er Addition on Microstructure and Oxidation Resistance of High Nb Containing TiAl Alloys

Abstract

Introduction

Experimental

Results and Discussion

Conclusions

References

Fundamentals

Fundamental and Application-Oriented Research on Gamma Alloys

Abstract

Introduction

Interactions Among Point Defects and Solutes

First Principles Study of Oxidation Process

MD Simulation of Dislocation Reactions

Texture Evolution During Extrusion

Near Net-Shape Investment Casting

Forming via Prealloyed Powder Metallurgy

Summary and Conclusion

Acknowledgements

References

Deformation of PST Crystals of Ti46Al8Nb and Ti46Al8Ta

Abstract

Introduction

Experimental procedure

Results and discussion

Conclusions

References

Seeded Growth of Ti-47Al-2Cr-2Nb PST Crystals

Abstract

Introduction

Experimental Procedure

Results and Discussion

Conclusion

References

Textures of Rectangular Extrusions of Ti-47Al-2Cr-2Nb-0.15B

Abstract

Introduction

Experimental Procedure

Results

Discussion

Conclusions

References

Microstructure and Properties

Origin and Magnitude of Internal Stresses in TiAl Alloys

Abstract

Introduction

Alloys

Stress Reduction and Anticipated Dislocation Behaviour

Reliability of the Method

Internal Stresses

Conclusions

Acknowledgements

References

Effects of Microstructure, Alloying and C and Si Additions on Creep of Gamma TiAl Alloys

Abstract

Introduction

Experiments

Results and Discussion

Summary

Acknowledgment

References

Microstructure and Properties of Cast Ti-46Al-8Ta Alloy

Abstract

Introduction

Experimental Procedure

Results and Discussion

Conclusions

Acknowledgements

References

Effect of the Microstructure on the Deformation and Fatigue Damage in a Gamma-TiAl Produced by Additive Manufacturing

Abstract

Introduction

Material and specimens

Fatigue experiments: procedures and results

Micromechanical analysis of damage accumulation

Conclusions

References

Effect of Powder Pre-Treatment on the Mechanical Properties of Powder Metallurgy Ti-47Al-2Cr-2Nb-0.15B

Abstract

Introduction

Experimental

Results and Discussion

Conclusion

References

Microstructure and Mechanical Properties of TiAl Alloys Produced by Powder Metallurgy

Abstract

Introduction

Experimental

Result and discussion

Conclusion

References

Author Index

Subject Index

GAMMA TITANIUM ALUMINIDE ALLOYS 2014

A collection of research on innovation and commercialization of gamma alloy technology

Copyright © 2014 by The Minerals, Metals & Materials Society.All rights reserved.

Published by John Wiley & Sons, Inc., Hoboken, New Jersey.Published simultaneously in Canada.

No part of this publication may be reproduced, stored in a retrieval system, or transmitted in any form or by any means, electronic, mechanical, photocopying, recording, scanning, or otherwise, except as permitted under Section 107 or 108 of the 1976 United States Copyright Act, without either the prior written permission of The Minerals, Metals, & Materials Society, or authorization through payment of the appropriate per-copy fee to the Copyright Clearance Center, Inc., 222 Rosewood Drive, Danvers, MA 01923, (978) 750-8400, fax (978) 750-4470, or on the web at www.copyright.com. Requests to the Publisher for permission should be addressed to the Permissions Department, John Wiley & Sons, Inc., 111 River Street, Hoboken, NJ 07030, (201) 748-6011, fax (201) 748-6008, or online at http://www.wiley.com/go/permission.

Limit of Liability/Disclaimer of Warranty: While the publisher and author have used their best efforts in preparing this book, they make no representations or warranties with respect to the accuracy or completeness of the contents of this book and specifically disclaim any implied warranties of merchantability or fitness for a particular purpose. No warranty may be created or extended by sales representatives or written sales materials. The advice and strategies contained herein may not be suitable for your situation. You should consult with a professional where appropriate. Neither the publisher nor author shall be liable for any loss of profit or any other commercial damages, including but not limited to special, incidental, consequential, or other damages.

Wiley also publishes books in a variety of electronic formats. Some content that appears in print may not be available in electronic formats. For more information about Wiley products, visit the web site at www.wiley.com. For general information on other Wiley products and services or for technical support, please contact the Wiley Customer Care Department within the United States at. (800) 762-2974, outside the United States at (317) 572-3993 or fax (317) 572-4002.

Library of Congress Cataloging-in-Publication Data is available.

ISBN 978-1-118-99558-7

PREFACE

This book is a collection of articles describing the current state of research on gamma alloy technology. Many of the articles published here were presented at the Fourth International Symposium on Gamma Titanium Aluminide Alloys (ISGTA 2014) held at the TMS 2014 Annual Meeting & Exhibition, February 16–20, in San Diego, California, USA.

The symposium consisted of eight presentation sessions and one panel discussion session and provided a forum for leading scientists and engineers associated with the gamma-alloy technology to report on recent advances and experiences with introducing the alloys into commercial enterprises, to exchange findings about their limitations and barriers, and to offer insights into the future of gamma alloy technology.

The highlights of the symposium were demonstrations of significant progress made in the industrialization and application expansion of alloy Ti-4822 cast LPT blades. Those in attendance were excited to learn that the first wrought-alloy TNM (beta solidified) LPT blades are nearing implementation. These demonstrations ensured that the foundation of gamma materials–processes technologies have been firmly established along with remarkable advances in required peripheral technologies such as joining, machining, surface protection, and coating. The remaining challenges to produce lower-cost, sound components include casting near-net components, further innovation of processing technologies, and establishing a supply chain capable of mass-production.

Alloy design efforts in wrought-processed material forms were reported and discussed on high Nb-containing alloys, as well as beta-solidified alloys including gamma-modulated alloys, along with related processing such as forging and rolling. Novel processing methods, such as additive manufacturing and spark plasma sintering, and PM route processing were investigated for producing either complex shape and/or low-cost PM products. Unfortunately, these efforts have not shown strategies for achieving higher temperature (>750°C) performing material forms having improved balance in properties. A number of presentations reported familiar results from characterization and phase transformation study of these and other current alloy materials. Some efforts were reported in additional understanding of the influence of microstructures on properties, particularly including applied aspects of PST crystals.

One bright side of alloy design for high temperatures (>750°C) is a new class of gamma alloys called “beta-gamma” alloys that are beta solidified but distinguished from other “beta-solidified” alloys. Beta-gamma alloys are the first alloys that generate gamma-rich, fine-grained fully lamellar structures in both wrought-processed and cast forms with minimized beta volume. These significantly enhance the properties and prospects for improved balance of properties, especially for higher temperatures, potentially raising the gamma alloy-materials to their upper limit of performance.

Organizing Committee

Young-Won Kim

Wilfried Smarsly

Junpin Lin

Dennis Dimiduk

Fritz Appel

EDITORS

Young-Won Kim

Young-Won Kim, Fellow of American Society for Materials (FASM) and graduate of Seoul National University, earned his Ph.D. in materials science from the University of Connecticut and worked on strengthening mechanisms and phase diagram construction at Carnegie Mellon University. In 1980, he joined Metcut Research Group (Wright-Patterson Air Force Base) to lead the research and development activities in processing high-strength and high-temperature aluminum alloys. He became well known worldwide and a frequent invited speaker in the areas. In 1989, Dr. Kim began to investigate titanium aluminides, and he joined UES as principal and chief scientist in 1992 to continue his R&D work on gamma titanium aluminide alloys. Since then, he has been involved in all types of projects and experiments and has become recognized worldwide in the areas of alloy design, processing, microstructure control, processing–microstructure–property relationships, environmental resistance, and integration of the data and knowledge toward the applications. After exhaustive R&D and through continuous relations with related industry and OEMs, he began to realize the serious limitations of conventional gamma alloys and their processes. For last several years, he has explored “beta-gamma” titanium aluminide alloys, a robust new class of TiAl-based alloys that exhibit improved balance of properties, especially for higher temperatures, potentially raising the gamma alloy-materials to their upper limit of performance. Other areas of his R&D activity included evaluating or developing Nb-silicides and Mo-silicide based alloys, high-entropy alloys, and dual superalloy disk materials. He is now leading a company, Gamteck, to more effectively contribute to the advances in gamma alloy materials-processes technology through targeted R&D work, consulting on technology details and education. Dr. Kim has published more than 170 articles and six patents; some of his publications on TiAl have been recognized by ISI among the most cited in the area of materials science. He has been actively involved in various technical activities, such as in delivering numerous invited talks and keynote lectures, organizing more than ten major international symposia and workshops, editing eight major proceedings, and serving as a panel member or a sole evaluator for several international and national gamma TiAl alloy programs. He was recognized as the Alumnus of 2003 by the University of Connecticut.

Wilfried Smarsly

Wilfried Smarsly is the Advanced Materials Representative at MTU Aero Engines in München, Germany. Dr. Smarsly earned a degree in Physics, Chemistry and Mathematics from the University of Münster and then completed his Ph.D. in Materials and Manufacturing Process Engineering from RWTH Aachen in 1985, His thesis described forging of Ti 64 powder to improve fatigue strength applied in helicopter engines. He worked as a research scientist at DLR e.V Köln, Institut for Materials Engineering until accepting a position at MTU Aero Engines München in 1987. At MTU, Dr. Smarsly is responsible for the development of advanced materials and raw part processes for aero engine applications. Dr. Smarsly is an expert on intermetallic materials (e.g., titanium aluminides) and has experience with alloys such as nickel superalloys, aluminum alloys, titanium alloys, niobium alloys, and intermetallics such as NiAl, and Mo-Si. He also works with processes such as melting and casting and forging processes and with pyrometallurgical processes, such as metal injection molding and spray forming.

Junpin Lin

Junpin Lin is the deputy director and professor of State Key Laboratory for Advanced Metals and Materials, University of Science and Technology Beijing. He has been honored with the “Cheung Kong Scholar” Professorship by the Ministry of Education of China. He received his bachelor’s degree at Harbin Institute of Technology in 1983 and Ph.D. degree in 1989. His major research fields include structural intermetallics (high-temperature TiAl alloys, Fe-Si alloys, etc.), severe deformation and structure controlling for hard-deformed materials, advanced porous materials, and new materials for extra-strong liquid zinc resistance. Dr. Lin is the chief scientist of the Major State Basic Research Development Program of China (973 program) and has already published more than 300 papers, applied 23 patents, and received high-level awards for scientific and technological achievements. He has made more than 30 invited presentations at regional, national, and international levels, including plenary and keynote lectures.

Dennis M. Dimiduk

Dennis M. Dimiduk is a Laboratory Fellow and past technical director of the Structural Materials Division at the Air Force Research Laboratory, Materials and Manufacturing Directorate. Through the early 1980s he performed research on alloy development, phase transformations, and strengthening mechanisms in high-temperature superalloys. Dr. Dimiduk led the intermetallics research area for the Air Force, conducting in-house research and motivating research at other laboratories and universities. Throughout the 1990s, work by Dimiduk and his colleagues on titanium aluminides and refractory intermetallics opened an approach toward raising use temperatures and realizing weight reductions in advanced engines. Their research led to current introductions of titanium aluminides into commercial turbine engines. In 1989, Dr. Dimiduk contributed to and led research seeking to understand the influence of chemistry on microstructural evolution and deformation in alloys through computer simulation. The group’s involvement in materials simulations led directly to the community’s current and growing activities in Integrated Computational Materials Science & Engineering (ICMSE) and the Materials Genome Initiative (MGI). That research also led to advancements in the 3D characterization of materials, new techniques for mechanical property characterization at the micrometer scale and, to the discovery of a new regime of size-affected metal deformation behavior. Dr. Dimiduk continues to pursue and explore those advancements today. Dr. Dimiduk received his B.S. degree in Materials Science and Engineering in 1980 from Wright State University. He completed his M.S. and Ph.D. degrees in Metallurgical Engineering and Materials Science at Carnegie Mellon University in 1984 and 1989, respectively. He has authored or co-authored more than 190 technical papers, 13 patents, and 2 book chapters, and has co-edited 4 books. He is a member of the editorial board for Intermetallics and is an adjunct professor at The Ohio State University. In 1993–94 he was a Visiting Scholar at the University of Oxford, UK, conducting collaborative research and lecturing on structural intermetallics. Dr. Dimiduk received the 1991 AFSC Waterman Award for science, the 2004 Charles J. Cleary Award for scientific achievement and, and five “Star Team” awards from the Air Force Office of Scientific Research. He was elected Fellow of ASM International in 1997 and Fellow of the Air Force Research Laboratory in 1998. He was selected for a Carnegie-Mellon University Alumni Achievement Award in 2008. Dr. Dimiduk has been a member of TMS, ASM, and MRS throughout his career. Presently he is the Past Chair of the Structural Materials Division of TMS and served on the TMS Board of Directors.

Fritz Appel

Fritz Appel has continued to play an active role in TiAl research since his retirement in 2006 as group leader of physical metallurgy. He obtained a Ph.D. in 1973 and his habilitation in 1987 from the Martin-Luther University in Halle. He spent six months in Japan on a JSPS fellowship in 1987, joining the Institute of Materials Research in Geesthacht in 1990. He received the Tammann Award from the German Society for Materials Science in 1999 and the Charles Hatchett Award in 2002 from the Institute of Materials, London. He has authored or co-authored a number of publications and holds six patents in the field. Together with Jonathan Paul and Michael Oehring he wrote the book Gamma Titanium Aluminide Alloys, published by Wiley-VCH (2011).

GAMMA TITANIUM ALUMINIDE ALLOYS 2014

Alloy Design and Development

Gamma Titanium Aluminide Alloys 2014

Edited by: Young-Won Kim. Wilfried Smarsly, Junpin Lin, Dennis Dimiduk, and Fritz Appel

TMS (The Minerals, Metals & Materials Society), 2014

ALLOY DESIGN CONCEPTS FOR WROUGHT HIGH TEMPERATURE TiAl ALLOYS

Junpin Lin1, Xiangjun Xu2, Laiqi Zhang1, Yongfeng Liang1, Yong Xu3, Guojian Hao1

1State Key Laboratory for Advanced Metals and Materials, University of Science and Technology Beijing, Beijing 100083, China

2Materials and Chemistry School, Zhongyuan University of Technology, Zhengzhou 450007, China

3School of Materials Science and Engineering, Shandong Jianzhu University, Jinan, Shandong Province, 250101, China

Keywords: High Nb-TiAl alloys, Wrought TiAl alloy, Workability, Mechanical property

Abstract

Wrought TiAl alloys provide more possibility to control the microstructure and give a balanced mechanical properties than cast alloy. Titanium aluminides based on the general composition Ti-45Al-(6-9)Nb (in at.%) exhibit several desired properties for higher temperature applications. Nb addition changes the Ti-Al phase diagram and the segregations of Nb and other elements are easy to form, which induces formation of B2 phase. B2 phase worsens the mechanical properties at both room temperature and elevated temperatures. The new idea is that the β phase is can be used to improve the hot-workability, and the segregations can be lightened during the deformation and finally disappeared, so stable B2 phase is avoided at room temperature. Otherwise, high Nb addition significantly reduces the stalking fault energy (SFE), resulting in abundant twinning and twin intersections, which plays an important role for accommodating heterogeneous deformation and avoiding formation of microcrack at boundaries. The basic compositional characteristics of the high temperature TiAl alloys are high Nb and low Al content, typically 6/9 Nb and 44-46Al. Carefully microalloying using the elements B, W, Y, C may further optimize the properties of the alloys. These wrought alloys have excellent oxidation resistance, balanced mechanical properties and good workability.

Introduction

Gamma TiAl alloys display attractive properties for high temperature applications. They have attracted significant attention in the last 30 years for their attractive properties that have the potential to enable high temperature automobile, aerospace and other industry applications. Due to low density and high strength, TiAl alloys have become front-runners in replacing nickel-based superalloys in gas turbine engines. Replacement of Ni-based superalloy components with TiAl alloys is expected to reduce the structural weight of high performance gas turbine engines by 20–30% [1]. TiAl alloys have been used in General Electric’s GEnx gas turbine engine designed for the Boeing’s 787 Dreamliner [2]. Cast 4822 TiAl alloys are being used in low pressure turbine blades. It is well established that the properties of TiAl alloys are highly dependent on composition and microstructure. An inhomogeneous microstructure resulting from chemical inhomogeneity can lead to a large scatter in mechanical properties. This is undesirable and can result in components being over-designed so that minimum properties can be guaranteed. For the components produced by ingot metallurgy, any chemical segregation during ingot solidification is very difficult to remove, requiring subsequent heat-treatment at temperatures within theαphase field or even higher. Defects such as cracks, inclusions, or even porosity may be present within ingots. The extent of such defects and elemental macrosegregation is magnified as ingot size increases. These inherent problems make the production of large parts, with guaranteed properties and homogeneous microstructures, much more challenging. Wu [3] recently reported that the low ductility is the biggest problem in the application of TiAl based alloys as structural components since 1% is generally accepted as the minimum acceptable level and cast samples in particular seldom reach even this level. The other major problem with TiAl alloys is the difficulty in processing them to form a component. This great issue limits the application in many areas of TiAl alloys.

Hot working, such as extrusion, forging and rolling, either singlely or combined, are often used to refine the cast microstructures and improve the mechanical properties of ingot material. There is the thermo-mechanical processing to adjust specific microstructures by means of forging and/or ensuing heat treatments. So, the wrought TiAl alloys provide more possibility to control the microstructure and give a balanced mechanical properties than cast alloy. High temperature TiAl alloys (high Nb-TiAl alloys) developed by Chen et al. [4-6] were suggested to be the first example for the development of high performance TiAl alloy for high temperature application by Young-Won Kim [7].Titanium aluminides based on the general composition Ti-45Al-(6-9)Nb exhibit several desired properties for higher temperature applications. Nb addition changes the Ti-Al phase diagram and the segregations of Nb and other elements are easy to form, which induces formation of B2 phase. B2 phase worsens the mechanical properties at both room temperature and elevated temperatures. The new idea is that the β phase is can be used to improve the hot-workability, and the micro-segregations can be lightened during the deformation and finally disappeared, so stable B2 phase is avoided at room temperature. Otherwise, high Nb addition significantly reduces the stalking fault energy, resulting in abundant twinning and twin intersections, which plays an important role for accommodating heterogeneous deformation and avoiding formation of micro-crack at boundaries. The intention of the present paper are:

(1) to identify the effect of Nb addition in the phase transformation of TiAl alloy;
(2) to figure out the strengthening mechanism in high temperature TiAl alloy;
(3) to discuss the deformation behaviors and workability;
(4) to evaluate the oxidation resistance and mechanical properties.

Effect of Nb addition in the phase transformation of TiAl alloy

The high Nb addition greatly changes the phase diagram of binary TiAl alloy. The quasi-phase diagrams of Ti-Al with 8Nb and 10Nb addition are shown in Fig. 1 [8], for comparison the binary Ti-Al phase diagram is presented as dotted lines [9]. It can be seen that 8-10 Nb addition has pronounced effect on the phase relationship of TiAl alloys. The effects are summarized as follows [9].

Fig. 1 Quasi-phase diagrams showing the effect of 8Nb and 10 Nb additions on the phase relationship of near γ-TiAl alloys (solid lines) [8]. The binary Ti-Al diagram is drawn in dotted lines for reference.

(1) The melting point increases by about 60-100 °C, for example, from ~1500 of Ti-45Al alloy to 1610 °C of Ti-45Al-10Nb alloy.

(2) The β transus (β/α+β boundary) decreases by 50-80 °C, and the β phase region is extended to higher Al concentration.

(3) The α transus decreases by about 30 °C. The α/α+β transus decreases by 50-100 °C. The α phase region beccomes narrowed and moves to higher Al concentration.

(4)The low temperature phase region (α2+γ) is replaced by the α2+γ+B2 ternary phase region if Nb content exceeds 10%.

Nb element is strong stabilizer of β phase, so the area of β phase enlarges remarkably; the β phase solidification occurs at Al content of about 44-46%, avoiding the peritectic transformation, which results in the grain refining and reduces the micro-segregation of Al and Nb. Another important result is that the B2 phase is equilibrium phase if the Nb content reaches 10%, and this means that micro-segregation of Nb can celebrate the occurrence of B2 phase. It is can be concluded that the high Nb addition can enhance the workability of TiAl alloys at high temperature because of existence of β phase; Nb content cannot exceed the 10%, avoiding stable B2 phase at room temperature, which worsen the mechanical properties at both ambient and high temperatures.

Strengthening Mechanism in high temperature TiAl alloy

Fig. 2 Hall-Petch relations for both FL binary alloys and 10 Nb containing ternary alloy

Nb addition can significantly enhance the strength of TiAl, and the room temperature ductility is same as that for binary TiAl, which is resulting from reducing the SFE of TiAl alloys by Nb addition [15-16].

It is interesting that the lower SFE leads to the twinning intersections even in the cast high Nb-TiAl alloys, as shown in Fig. 3 (index as the arrows). During the deformation at high temperature, a lot of intersections of twins and platelets, resulting formation of new twins and dislocations, as shown in Fig. 4, that significantly reduces stress concentration, avoiding formation of microcrack at boundaries. So the high Nb addition remarkably increases the strength at room temperature, maintaining enough ductility.

Fig. 3 The twinning intersections in the cast high-Nb TiAl alloys

Fig. 4 Microstructures of deformed at 900 °C for high Nb-TiAl alloys: (a) formation of new twins in the adjacent γ platelet by the twin intersections, (b) formation of the dislocations in the adjacent γ platelet by the twin intersections with α2, (c) relaxing stress concentrations by formation of abundant dislocations in the γ platelet by the twin intersections with fine α2 platelets, (d) and (e) high magnifications for Fig.4 (c)

Deformation behavior and workability

It is very hard to produce industrially required large and complex parts from TiAl alloys by hot-forging, due to limited equipment capability, cracking, etc. For the application of wrought TiAl alloys, the reduction of high temperature flow stress and improvement of deformability is essential. In the case of TiAl alloys, the most effective way to accomplish this is the introduction of β phase during the deformation [13]. Fig.5 shows the microstructures of cast ingot with a weight of 1000kg of high Nb-TiAl alloy by plasma arc melting. It can be seen that this is refine NF microstructure with B2 phase and the high magnification image shows dark ω phase in the light B2 phase.

Fig. 5 Microstructures of cast, ingot of high Nb-TiAl alloy by plasma arc melting: (a) NF microstructure with B2 phase, (b) high magnification image showing darkωphase in the light B2 phase

In general, the route for rolling sheet for TiAl alloys is that multi-step canned forging is first, in order to refine the coarse cast microstructures, then hot rolling. Fig.6 shows the sheet with the size of 310×80x4.68 mm3 by hot rolling directly from cast ingot, and deformation is ~70%. This reveals that the cast ingot of high Nb-TiAl alloy has an excellent workability, which results from the fine microstructure and some volume of B2 phase.

Fig. 6 Sheet with the size of 310×80x4.68mm by hot rolling from cast ingot for high Nb-TiAl alloy: (a) canned sample, (b) rolling sheet

Oxidation resistance and mechanical properties

The actual service of TiAl alloy has been hindered by their poor oxidation resistance above about 750 °C. A great deal of research work has been undertaken to improve the oxidation behavior of these alloys by adding ternary and quaternary elements. In view of third element addition, niobium and several other elements have been reported to be effective in the oxidation resistance of TiAl [17-21]. High Nb addition greatly improves the oxidation resistance of TiAl alloys. Alloys with higher Nb contents (up to 10 %) show much smaller mass gain in the isothermal oxidation at 900 °C [21]. Nb is firstly supposed to function as a dopant element with a higher valence than titanium, which is expected to decrease the oxygen vacancy concentration owing to the electroneutrality in the oxide, and thus to suppress rutile growth [22]. The addition of Nb also has other effect on the oxidation behaviors, such as increasing the activity of Al, lowering the solubility of oxygen in the alloy and promoting the formation of TiN at the oxide scale/substrate interface, which impede the diffusion of titanium and oxygen ions [23-25]. Our recent work reveals that an appropriate amount of Y addition (depend on Nb) is effective in improving the oxidation resistance, especially high temperature long term oxidation resistance (1000hrs and 1000 cycles) by refining the oxide particles, promoting formation of a protective continuous Al2O3 scale and improving the adherence of the oxide scale and matrix the interlayer adhesion [26-27].

The high Nb-TiAl alloys have good workability, so high-quality pancake can be produced by multi-step canned forging of the ingot. Microstructure in the major part of the pancake is homogenous with a DP microstructure containing equiaxedγand fine α2/γ lamellae with a grain size of about 20-30 μm, while in the near surface zone is a fine-grained DP and retained lamellar colony. The metastable β phase is eliminated, and the long boride ribbons are broken off. Both microstructures of the alloy had excellent strength at room and high temperatures. Fig. 7 shows the typical engineering tensile stress-strain curve for wrought high Nb-TiAl alloys at room temperature, The yield stress and ultimate stress are 782 MPa and 912 MPa, respectively. The most important is that the elongation is 2.3%.

Fig. 7 The engineering tensile stress-strain curve for wrought high Nb-TiAl alloys at room temperature

The as-forged material was stronger and much more ductile than the as-cast material, exhibiting a brittle-ductile transition with an elongation 2.3% at room temperature increasing to 59.1% at 815 °C [28]. The YS and UTS of the as-forged material are 537 and 648MPa at 815 °C, respectively.

For the high temperature application, the creep behaviors are very vital. The creep properties for the wrought high Nb-TiAl alloys are better than that of the conventional TiAl alloys with both DP and FL microstructures. The creep temperatures of high temperature TiAl alloy are 60-100 °C higher than that of conventional TiAl alloys [29]. The higher creep strength can be attributed to higher friction stress, lower recrystallization rate, higher microstructure stability and lower SFE and diffusion-assisted transport processes [29].

Challenge for wrought high Nb-TiAl alloy is how to get the homogenous fine FL microstructure by ensuing heat treatment, in order to further enhance the high temperature capability.

Conclusion

(1) High Nb addition changes the TiAl phase relationships and the segregations of Nb and other elements are easy to form, which induces formation of B2 phase;
(2) The new idea is that the β phase is can be used to improve the hot-workability, and the segregations can be lightened during the deformation and finally disappeared, so stable B2 phase is avoided at room temperature.
(3) High Nb addition significantly reduces the stalking fault energy, resulting in abundant twinning and twin intersections, which plays an important role for accommodating heterogeneous deformation and avoiding formation of micro-crack at boundaries.
(4) The basic compositional characteristics of the high temperature TiAl alloys are high Nb and low Al content, typically 6/9 Nb and 44-46Al.
(5) These wrought alloys have excellent oxidation resistance, balanced mechanical properties and good workability.

Acknowledgement

The authors thank the National Basic Research Program of China (973 Program) for financial support under contract No. 2011CB605501 and The National Natural Science Foundation of China for financial support under contract Nos. 51271016 and State Key Laboratory for Advanced Metals and Materials, University of Science and Technology Beijing, under contract No. 2012Z-06.

References

[1] W. Voice, M. Henderson, E. Shelton, X. Wu, Intermetallics, 13(2005)959–64.

[2] GE Aviation. GE—Aviation: GEnx. GE. [Online], 2007. /http://www.geae.com/engines/commercial/genx/S.

[3] X.H. Wu, Intermetallics, 14(2006)1114.

[4] G.L. Chen, Z.Q. Sun, and X. Zhou, Corrosion, 11(1992), 939.

[5] W.J. Zhang, G.L. Chen, and Z.Q. Sun, Scripta Metall. Mater., 28(1993), 563.

[6] G. Chen., W. Zhang, Y. Wang, J. Wang and Z. Sun, Structural intermetallics, eds. R. Darolia, J.J. Lewandowski, C.T. Liu, P.L. Martin, M. V.Nathal, TMS Warrendale, PA, 1993, 319.

[7] Y-W Kim, Gamma Titanium Aluminides, eds. Y-W Kim, R. Wagner and M. Yamaguchi, TMS, PA. 1995, 637.

[8] G.L. Chen, W.J. Zhang, Z.C. Liu, S.J. Li, Y-W, Kim, Gamma Titanium Aluminizes 1999, ed. Y-W Kim, D.M. Dimiduk, N.H. Lerotto, TMS, 1999, 371.

[9] H. Okamoto, J. Phase Equilibria, 14(1993)120.

[10] G.L. Chen, Z.C. Liu, J.P. Lin and W.J. Zhang, 3rd International Symposium on Structural Intermetallics, USA, 2001, 475.

[11] Z.C. Liu, J.P. Lin, S.J. Li and G.L. Chen, Intermetallics, 10(2002)653.

[12] W.J. Zhang, G.L. Chen, F. Appel, T.G. Nieh, S.C. Deevi, Materials Science and Engineering, A, 315(2001) 250–253.

[13] G.L. Chen, L.L Zhao, J. P. Lin, X.J. Xu, Proceeding for Materials Fabrications, Properties, Characterization and Modeling, TMS, 2007, 547–554.

[14] C.T. Liu and P.J. Maziasz, Intermetallics, 6(1998) 653-.

[15] X.P. Song and G.L. Chen, Journal of Materials Science Letters, 20(2001)659–661.

[16] X.P. Song and G.L. Chen, Materials Letters, 48(2001)273–280.

[17] G.L. Chen, Z.Q. Sun, X. Zhou, Corrosion Science, 48(1992)939–946.

[18] Y.G. Zhang, X.Y. Li, C.Q. Chen, W. Wang, V. Ji., Surf Coat Technol, 100-101(1998)214–218.

[19] M.F. Stroosnijder, N. Zheng, W.J. Quadakkers, R. Hofman, A. Gil, F. Lanza, Oxid Met, 46(1996)19–35.

[20] M. Yoshihara, K. Miura, Intermetallics, 3(1995)357–363.

[21] J.P. Lin, L.L. Zhao, G.Y. Li, L.Q. Zhang, X.P. Song, F. Ye, G.L. Chen, Intermetallics, 19(2011)131–136.

[22] G.L. Chen, Z.Q. Sun, X. Zhou, Corrosion, 48(1992)939–946.

[23] V.A.C. Haanappel, J.D. Sunderkotter, M.F. Stroosnijder, Intermetallics, 7(1999)529–541.

[24] M. Schmiedgen, P.C. Graat, B. Baretzky, E.J. Mitterneijer, Thin Solid Films, 415(2002)114–122.

[25] V. Maurice, G. Despert, S. Zanna, P. Josso, M.P. Bacos, P. Marcus, Acta Materialia, 55(2007)3315–3325.

[26] L.L. Zhao, G.Y. Li, L.Q. Zhang, J.P. Lin, X.P. Song, F. Ye, G.L. Chen, Intermetallics, 18(2010) 1586–1596.

[27] L.L. Xiang, L.L. Zhao, Y.L. Wang, L.Q. Zhang, J.P. Lin, Intermetallics, 27 (2012) 6–13.

[28] X.J. Xu, J.P. Lin, Y.L. Wang, J.F. Gao, Z. Lin, G.L. Chen, Journal of Alloys and Compounds, 414 (2006) 175–180.

[29] S.J Li, Ph.D thesis, The University of Science and Technology Beijing, 1998.

Gamma Titanium Aluminide Alloys 2014

Edited by: Young-Won Kim. Wilfried Smarsly, Junpin Lin, Dennis Dimiduk, and Fritz Appel

TMS (The Minerals, Metals & Materials Society), 2014

Lesen Sie weiter in der vollständigen Ausgabe!

Lesen Sie weiter in der vollständigen Ausgabe!

Lesen Sie weiter in der vollständigen Ausgabe!

Lesen Sie weiter in der vollständigen Ausgabe!

Lesen Sie weiter in der vollständigen Ausgabe!

Lesen Sie weiter in der vollständigen Ausgabe!

Lesen Sie weiter in der vollständigen Ausgabe!

Lesen Sie weiter in der vollständigen Ausgabe!

Lesen Sie weiter in der vollständigen Ausgabe!

Lesen Sie weiter in der vollständigen Ausgabe!

Lesen Sie weiter in der vollständigen Ausgabe!

Lesen Sie weiter in der vollständigen Ausgabe!

Lesen Sie weiter in der vollständigen Ausgabe!

Lesen Sie weiter in der vollständigen Ausgabe!

Lesen Sie weiter in der vollständigen Ausgabe!

Lesen Sie weiter in der vollständigen Ausgabe!

Lesen Sie weiter in der vollständigen Ausgabe!

Lesen Sie weiter in der vollständigen Ausgabe!

Lesen Sie weiter in der vollständigen Ausgabe!

Lesen Sie weiter in der vollständigen Ausgabe!

Lesen Sie weiter in der vollständigen Ausgabe!

Lesen Sie weiter in der vollständigen Ausgabe!

Lesen Sie weiter in der vollständigen Ausgabe!

Lesen Sie weiter in der vollständigen Ausgabe!

Lesen Sie weiter in der vollständigen Ausgabe!

Lesen Sie weiter in der vollständigen Ausgabe!

Lesen Sie weiter in der vollständigen Ausgabe!

Lesen Sie weiter in der vollständigen Ausgabe!

Lesen Sie weiter in der vollständigen Ausgabe!

Lesen Sie weiter in der vollständigen Ausgabe!

Lesen Sie weiter in der vollständigen Ausgabe!

Lesen Sie weiter in der vollständigen Ausgabe!