Laser Cleaning for Aerospace Manufacturing
Submitting Institution
University of ManchesterUnit of Assessment
Aeronautical, Mechanical, Chemical and Manufacturing EngineeringSummary Impact Type
TechnologicalResearch Subject Area(s)
Physical Sciences: Other Physical Sciences
Chemical Sciences: Physical Chemistry (incl. Structural)
Summary of the impact
Research at the University of Manchester on laser cleaning of Ti alloys
has resulted in practical
implementation of the technology at Rolls-Royce for the automatic
preparation of surfaces prior to
electron beam welding. This has been applied to 24 different aero-engine
component types
including compressor drums across most current engine families. This has
resulted in close to
100% `first time right' aero-engine component welds. The technology is
also being adopted by BAE
Systems to replace chemical cleaning during airframe manufacture. The
elimination of manual and
chemical cleaning processes results in savings of several million pounds
per annum.
Underpinning research
The impacts are based on research that took place in the Laser Processing
Research Centre at
The University of Manchester from 2003-2013. The key researchers involved
in the research were:
- Professor Lin Li (2003-2013), PI and laser cleaning project leader.
- Dr Mark Turner (2003-2007), PhD student at The University of
Manchester.
- Dr. David Whitehead (2003 - 2013). Senior Experimental Officer — laser
processing.
- Dr Philip Crouse (2005-2007), Postdoctoral Research Associate, laser
cleaning and
modelling
- Dr. Wei Wuo (2010 - 2013, postdoctoral researcher, laser cleaning and
in-process
monitoring, instrumentation.
- Dr. Sundar Marimuthu (2009-2011), postdoctoral researcher, laser
cleaning process
development, and modelling.
- Dr. Zhu Liu (2003 - 2013), Senior Lecturer, Material Science.
As many contaminants, such as metal oxides, have vaporisation
temperatures much higher than
the substrate alloy and Ti-alloy is highly reactive to N2 and O2
at elevated temperatures (from
600oC upwards), it is critical to demonstrate the total removal
of contaminants without damaging
the substrate. Through our research, laser beam interactions with various
industrial contaminants
and specific aerospace alloys have been understood, and a new laser
cleaning process has been
demonstrated and subsequently adopted by the aerospace industry.
In this research, three different lasers: CO2, Nd:YAG and
excimer were investigated to identify the
basic process characteristics in laser removal of a variety of
contaminants including synthetic oil,
silicon grease and machining coolant, applied on Ti-6Al-4V,
Ti-6Al-2Sn-4Zr-6Mo and IMI834 alloys,
without damaging the substrates. Fundamental studies on how the lasers
interact with these
materials were carried out through both experimental investigations and
theoretical modelling. We
have shown that:
- The continuous wave CO2 laser at 10.64 µm wavelength and
nanosecond pulsed Nd:YAG
laser at 1.06 µm wavelength were not suitable for cleaning aerospace
components with the
specific type of contaminants, for E-beam welding or diffusion bonding
applications,
because of their specific beam absorption characteristics (e.g. Nd:YAG
laser is transparent
to silicon grease) and thermal history (leading to excessive heat input
to the substrate
material if the contaminants are to be removed) [1,2,4].
- The excimer laser at 248 nm wavelength at 8-20 nm pulse lengths was
the most suitable
tool for the cleaning the contaminants without damaging the substrate
alloys under specific
operating parameters [3].
- The excimer laser removes organic contaminants mainly by
photo-chemical ablation
mechanisms while oxide particle removal is by photo-thermal ablation
[3].
- Electron beam welded components following excimer laser cleaning were
shown to be
defect free after excimer laser cleaning [3].
- We found the emission spectroscopy and probe beam reflection
techniques can be applied
to monitoring the laser cleaning process [5]. This has been further
developed by the same
research team using an acoustic monitoring technique in collaboration
with Rolls-Royce
and BAE System.
References to the research
At least five publications (on laser cleaning for electron beam welding)
are in the leading journals,
e.g. Applied Surface Science, several invited/keynote international
conference presentations were
made and a patent was generated from the research.
Key Publications
[1] M.Turner, M.J.J.Schmidt and L.Li, "Preliminary study into the effects
of YAG laser processing
of Titanium 6Al-4V alloy for potential aerospace component cleaning
application", Applied
Surface Science, 247, (2005), 623-630.. DOI
10.1016/j.apsusc.2005.01.097
[2] M.W.Turner, P.L.Crouse, L.Li and A.J.E.Smith, "Investigation into CO2
laser cleaning of
titanium alloys for gas-turbine component manufacture", Applied
Surface Science, 252,
(2006), 4798-4802. DOI
10.1016/j.apsusc.2005.06.061
[3] M.W. Turner, P.L.Crouse and L.Li, "Comparative interaction mechanisms
for different laser
systems with selected materials on titanium alloys", Applied
Surface Science, 253, No.19,
(2007), 7992-7997. DOI
10.1016/j.apsusc.2007.02.173
Other relevant publications
[4] M.W.Turner, P.L.Crouse and L.Li, "Comparison of mechanisms and
effects of Nd:YAG and
CO2 laser cleaning of titanium alloys", Applied Surface
Science, 252,No.13, (2006), 4792-
4797. DOI
10.1016/j.apsusc.2005.06.050
[5] D.Whitehead, P.Crouse, M.Schmidt, L.Li, MW.Turner, A.J.E.Smith
"Monitoring laser cleaning
of titanium alloys by probe beam reflection and emission spectroscopy", Applied
Physics A-Material Science & Processing, 93, Issue 1, (2008),123-127. DOI
10.1007/s00339-008-4643-7
Details of the impact
Context
Electron beam welding and diffusion bonding are typical joining processes
(in the final stages of
aero-engine assembly) used in the aerospace industries for a variety of
components and
structures. Insufficient bonding and defects such as porosity can occur if
the surfaces are not
perfectly clean from dirt, particles, oil/grease and machine coolants. The
resultant cracking and
porosity leads to quality assurance failure of these very expensive parts
in this final stage of aero-
engine manufacture.
Prior to our research, the practice in use for E-beam welding of
aero-engine components was
either manual cleaning (up to 10 different steps) using chemicals and
abrasives or dipping the
components into a bath of concentrated HF (hydrofluoric acid) that is
highly corrosive and
hazardous, with chemical residuals sometimes becoming trapped (e.g. HF) in
the material [A].
Our research has shown that laser cleaning offers great advantages
eliminating the use of
chemicals and allowing the process to be fully automated and over 20 times
faster [A]. The new
technology allows precise control of the process, so that all contaminants
are removed, without
damage to the substrate surface.
Pathways to Impact
The research work was carried out in collaboration with Rolls-Royce
(since 2003) and later (since
2009) with BAE Systems. The companies participated in all stages of the
R&D (monthly review
meetings), provided the test materials, process requirements, welding and
diffusion bonding of
laser cleaned components, and testing of laser cleaned specimens and
components to industrial
standards [A,B]. Rolls-Royce subsequently certified and implemented the
technology. BAE
Systems is also taking up the technology for diffusion bonding surface
preparation.
This work was originally funded by Rolls-Royce (CASE studentship) and the
Northwest Science
Council (N0003200) with over £1m. Following the successful application of
the technique at Rolls-
Royce since 2008, major funding from industry (Rolls-Royce, BAE Systems)
and EPSRC and TSB
of around £2m was granted (SAMULET project) to further develop the laser
cleaning process for
diffusion bonding applications (2009-2013).
Reach and Significance of the Impact
The impact of our research is demonstrated by its adoption and use by the
leading UK aerospace
company Rolls-Royce — globally the second largest manufacturer of
aero-engines. In addition BAE
Systems is also now adopting the technology.
Rolls-Royce began introducing the laser cleaning technology, developed
through our research, for
E-beam welding of aero engine components in 2008. By May 2013, Rolls-Royce
had approved 24
different aero-engine components such as compressor drums in almost all
the current engine
families such as Trent 700, using the laser cleaning technology in the
manufacture of commercial
aero-engines [A]. The technology has shown improved productivity and
reduced failure rate. The
first time right rate using chemical methods was 82-90% and has improved
significantly utilising our
new laser cleaning method. In his statement [A] the global process owner
for laser processes at
Rolls-Royce confirms "This automatic laser cleaning process has
replaced previous manual
chemical cleaning of parts for electron beam welding with significant
improvements in productivity
and first time right."
The economic impacts are multiple including cost savings in reducing
scraps at this final stage of
the aero engine assembly, estimated at several millions of £ per year and
elimination of the use of
harmful chemicals and their disposal, estimated at a few £ million per
year. In 2013, a new in-process
monitoring system, developed at the University of Manchester, was
installed at Rolls-Royce
for the monitoring of the laser cleaning process [A].
Following the successful use of laser cleaning of Ti alloys in welding,
the research has been further
developed (2009-2013) for diffusion bonding of a wide variety of aerospace
products. The diffusion
bonding of Trent 900 fan blades at Rolls-Royce, after laser cleaning, has
passed the quality
criteria. A modelling tool has been delivered to Rolls-Royce and BAE
Systems for laser cleaning
process evaluations. This tool has been successfully utilised by BAE
Systems to aid their decision-making
with regards to the installation of a laser cleaning system in the company
[B]. As a result
the laser cleaning technology is now being commissioned by BAE Systems for
military aircraft
manufacture, with the diffusion process replacing chemical cleaning [B].
Sources to corroborate the impact
[A] Letter from Global Process Owner — Laser Processes, Rolls-Royce plc
corroborating
deployment of laser cleaning process by Rolls Royce, replacing previous
manual cleaning
process, and procurement of patented monitoring techniques.
[B] Letter from SAMULET Project Manager, BAE Systems corroborating
transitioning of laser
cleaning process by BAE Systems and use of modelling tool for evaluation
of performance.