Loughborough University Institutional Repository Developments in platinum electroplating for aero-engine applications ThisitemwassubmittedtoLoughboroughUniversity’sInstitutionalRepository by the/an author. Additional Information: • A Doctoral Thesis. Submitted in partial fulfilment of the requirements for the award of Doctor of Philosophy at Loughborough University. Metadata Record: https://dspace.lboro.ac.uk/2134/28176 Publisher: (cid:13)c S.E. Hadian Rights: ThisworkismadeavailableaccordingtotheconditionsoftheCreative CommonsAttribution-NonCommercial-NoDerivatives2.5Generic(CCBY-NC- ND2.5)licence. Fulldetailsofthislicenceareavailableat: http://creativecommons.org/licenses/by- nc-nd/2.5/ Please cite the published version. This item was submitted to Loughborough University as a PhD thesis by the author and is made available in the Institutional Repository (https://dspace.lboro.ac.uk/) under the following Creative Commons Licence conditions. For the full text of this licence, please go to: http://creativecommons.org/licenses/by-nc-nd/2.5/ LOUGHBOROUGH UNIVERSITY OF TECHNOLOGY LIBRARY " AUTHOR/FILING TITLE j ______________ J~'~~l -'~~-7-?:~f~------______ _ 1-------------------------------- --------------- -~- 1_;:;~N~:~~;~~J.~.2"------------ ", i i 1111111111111 11111 ' DEVELOPMENTS IN PLATINUM ELECTROPLATING FOR AERO-ENGINE APPLICATIONS BY SEYED. ESMAIL. HADIAN, P.G.Dipl.(Brunel), MSc, MPhil(CNAA) Sheffield City Polytechnic A thesis submitted in fulfilment of the regulations for the degree of Doctor of Philosophy of Loughborough University of Technology October 1993 Supervisor: Dr.D.R.Gabe IPTME Loughborough University Of Technology Industrial Supervisor: Mr.M.Dean C.U.K Ltd, Hatfield, Herts G) S.E.HADIAN,1993 ,od < Loughborough University ofT~': <:-1 Ubrary -- .. .'., . <. Date 'J.4:0~ Class .. --.,- Ace. -.~- -r No. IN O<:>'?J 10 0 ABSTRACT The electro-deposition of platinum on mild-steel and nimonic alloys substrates using more than twenty baths have been investigated. It has been shown that the cell efficiency can be improved markedly with lower current density, pH value and plating temperature. Distinct differences between direct and pulsed processes revealed themselves in the cathode current efficiency data. Implications of using pulse plating to control the quality of electrodeposits have been considered. The experimental work reported in this thesis is to a large extent based on cell efficiency and potentiodynamic polarisation which is considered to be a powerful tool for evaluating potential coating solutions. The cathodic polarisation characteristics of platinum solutions has been studied quantitatively. An excellent technique (electroless) has been developed in an attempt to successfully apply platinum deposit on commonly used mild steel or_nimonic alloys using 'Q'salt manufactured by Johnson Matthey. A series of different designed experiments were used to evaluate the high value ranges of throwing power{localised plating) capabilities and opportunities for extending that capability to replace the Brush plating. Throwing power is currently used for those blades which require the plati num/rhodium plating for RB211 Blades at concave aerofoil sections manufactured by Rolls Royce situated at Derby in U.K. The investigation employed different size and shape of anodes/cathodes to explore the effects of various factors in the Ni-plating and then as this technique has been established using nickel rather than noble metals, it was used to implement this feature in platinum and rhodium plating. PREFACE The work presented in this thesis was carried out at the C.U.K Ltd's laboratory in Hatfield, Herts and Loughborough University of Technology during the period from July 1989 to October 1993. During this period the candidate has not been registered for any other university degree. The research reported here is, as far as can be ascer tained, original except where due reference has been to previous work. I would like to thank Dr D.R.Gabe, my supervisor, for his considerable help and guidance during this project. I would also like to express my grateful thanks to Mr M.Dean, my industrial supervisor at C.U.K Ltd, to whom I am greatly indebted for his patient supervision and en couragement. Similarly I would like to thank Mr D.Maxwell-Lyte, laboratory supervisor,Mr D.Clark, Labora tory Chemist, and all technical staff in the C.U.K Engi- neering company for their invaluable help, advice and constant support. TABLE OF CONTENTS Page No Abstract Preface Table of Contents CHAPTER 1: INTRODUCTION 1 1.0 Developments in Platinum Electroplating for Aero-Engine Applications 1.1 Summary 1.2 History of Platinum 2 1.2.1 Occurrence 1.2.2 Extraction 1.3 Physical and Chemical Properties 4 1. 3.1 Uses 4 1.4 Characteristics of the Platinum Metals 7 1.5 General Considerations 10 (a) Molten Cyanide Electrolytes 13 (b) Electroless Plating 14 1.6 Anodes and Plating Salts 15 1.7 Protective Coatings for gas turbines 15 1.7.1 Summary 1.7.2 Introduction 16 1.7.3 Environmental Degradation of High Temperature Alloys 17 1.7.4 Surface Coatings 18 1.7.5 Property Requirements of Turbine Aerofoil Coating System 18 1.7.6 Classification of Current Coating 19 1.7.7 Concluding Remarks 20 1.8 Coatings for Corrosion control 21 CHAPTER 2: 2.0 Principles of Electrodeposition 24 2.1 Basic Electroplating Theory 2.2 Mechanism of general Electrodeposition 25 2.3 Electrode Potentials 29 2.4 Electrolytic Crystallization 32 2.5 Electrolytes for the Deposition of Platinum 33 2.5.1 Platinum Plating 34 2.5.2 Powell and Scott Bath 36 2.5.3 Platinum Plating from Alkaline solutions 38 2.5.4 Sulphato-Dinitrio-Platinate Solution 39 2.5.1.1 Plating Conditions 41 2.5.5 Platinum 209 43 2.5.5.1 Bath Maintenance 43 2.5.5.1.1 Platinum Metal 2.5.6 Platinum Solution 3745 44 2.5.6.1 Bath Maintenance 45
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