Increased efficiency in turbomachinery design, manufacturing and performance using 3D inverse design software
Submitting Institution
University College LondonUnit of Assessment
Aeronautical, Mechanical, Chemical and Manufacturing EngineeringSummary Impact Type
TechnologicalResearch Subject Area(s)
Engineering: Interdisciplinary Engineering
Summary of the impact
The development of a novel 3D inverse design method for turbomachinery
aerodynamic design at UCL has led to important design breakthroughs for
pump and compressor applications. The resulting IP and software has been
commercialised by a UCL spinout company Advanced Design Technology Ltd
(ADT), which is now considered a global leader in advanced turbomachinery
design software. Since 2008, the 3D inverse design codes embedded within
ADT's TURBOdesign™ suite of software have been adopted by many of the
leading turbomachinery equipment manufacturers in Europe, Japan and the
US. These companies are using the TURBOdesign suite to achieve significant
improvements in the time taken to design their turbomachinery components.
It has also helped them unlock major efficiency gains and hence achieve a
reduction in CO2 emissions. [text removed for publication]
Underpinning research
There are two different approaches to aerodynamic design of
turbomachinery components such as turbines, compressors, fans, pumps and
torque converters. The direct design approach is based on trial and error
iteration of the blade or vane geometry by the designer, using feedback
from a Computational Fluid Dynamics (CFD) code. This approach inherently
results in a reduction of the design space as designers tend to operate
within their comfort zone. Using this approach makes it more difficult to
achieve designs beyond the designer's previous experience and is also
time-consuming. The result is significant constraints on the ability of
companies to achieve further improvements in the performance of their
turbomachinery. By contrast, in the inverse design approach, the blade or
vane geometry is designed for a given specified distribution of pressure
or blade loading. The 3D pressure distribution controls the viscous
behaviour of the flow; by controlling the 3D pressure field it is possible
to directly use the detailed information provided by CFD solutions to
arrive at a choice of optimum loading to control particular sources of
loss in turbomachines. By removing the need for empiricism in the design
process, the inverse design approach allows designers to directly use
their knowledge of detailed fluid dynamics, as provided by CFD and
detailed measurements, to arrive at a breakthrough solutions that solve
particular adverse flow phenomena.
The inverse design approach had previously been used extensively in two
dimensions by the aeroengine industry but no robust design methods existed
in three dimensions. To address this gap, the research group headed by
Professor Mehrdad Zangeneh (Professor of Thermofluids, at UCL since 1989)
in UCL's Department of Mechanical Engineering started working on the
development of novel 3D inverse design methods in the early 1990s. One of
the key aspects of previous inverse design methods was that they mainly
relied on the specification of blade surface pressure on suction and
pressure surfaces. This removed the designer's control of blade thickness,
which is a very important parameter for high-speed applications.
Furthermore, the compatibility conditions in three dimensions make it
difficult to know the correct feasible spanwise static pressure
distribution on the blade a priori, as spanwise variations in
pressure are influenced by the streamwise flow distribution. This meant
that development or extension of any inverse method in 3D had limited
success. A key innovation arising from the UCL research was the use of
blade loading within the design methodology. When coupled with pressure
jump across the blade and blade thickness, it was possible to achieve a
significantly more robust 3D inverse design method and this allowed some
of the important outstanding problems in turbomachinery aerodynamics to be
solved [1][2]. The design code was subsequently extended to marine ducted
propulsors as a result of a $700k research grant from the US Office of
Naval Research [3] and extended to include coupling with automatic
optimisation for multi-point/multi-objective design [4]. UCL's application
of 3D inverse design methods to various applications, especially in radial
turbomachinery, resulted in important breakthroughs in design and led to
the university filing a number of international patents [8].
One of the first applications of the 3D inverse design method was in
centrifugal compressors and pumps. The main aim was to reduce or eliminate
secondary flows in the impeller, which result in significant flow
non-uniformity (jet/wake flow) and hence are a major cause of loss in
impellers. The nature of secondary flows and what causes them was quite
well understood, but with conventional (or direct) design based on
iterative changes to geometry it was rather difficult to arrive at a
design that helped to reduce or minimise secondary flows. By using the 3D
inverse design method, UCL researchers could establish a systematic
approach for minimising secondary flows in centrifugal impellers. The
control of secondary flows actually led to significant improvements to
compressor/pump stage efficiency [5 and patents i and iii]. Other
breakthroughs were related to control of 3D corner separation in pump
diffusers [6 and patents iv, v and vi]. Further important breakthroughs
were obtained in cavitation in pumps [7] and shockwave losses in transonic
axial fans [2].
The research was subsequently commercialised through the formation of a
UCL spinout company, Advanced Design Technology (ADT), which was
established as a joint venture with the major Japanese turbomachinery
manufacturer, Ebara Corporation, in 1998.
References to the research
[1] M. Zangeneh, "Invisicid-viscous interaction method for
three-dimensional inverse design of centrifugal impellers", Journal of
Turbomachinery, vol. 116, pp. 280-290, 1994. DOI: doi.org/bgcp5h
[2] W. T. Tiow and M. Zangeneh, "Application of a three-dimensional
viscous transonic inverse method to NASA rotor 67", J of Power and
Energy, Proc of IMeche, vol. 216, pp. 243-255, 2002. DOI: doi.org/bq7z94
[3] K. Yiu and M. Zangeneh, "On the simultaneous design of blade and duct
geometry of marine ducted propulsors", Journal of Ship Research,
vol. 42, pp. 274-296, 1998. Available on request.
[4] D. Bonaiuti and M. Zangeneh, "On the Coupling of Inverse Design and
Optimization Techniques for the Multiobjective, Multipoint Design of
Turbomachinery Blades", Journal of Turbomachinery, 2009. DOI: doi.org/fvzncz
[5] M. Zangeneh, A. Goto, and H. Harada, "On the design criteria for
suppression of secondary flows in centrifugal and mixed flow impellers", ASME
J of Turbomachinery, vol. 120, pp. 1-15, 1998. DOI: doi.org/dmr3xr
[6] A. Goto and M. Zangeneh, "Hydrodynamic Design of Pump Diffuser Using
Inverse Design Method and CFD", Journal of Fluids Engineering,
vol. 124, pp. 319-328, May 2002. DOI: doi.org/bnds24
[7] D. Bonaiuti, M. Zangeneh, R. Aartojarvi, and J. Eriksson, "Parametric
Design of a Waterjet Pump by Means of Inverse Design, CFD Calculations and
Experimental Analyses", Journal of Fluids Engineering, vol. 132,
pp. 1-15, Apr. 2010. DOI: doi.org/ckh5ds
[8] Selected related patents: i) US5685696 A — (1997-11-11), ii)
EP0775248 B1 — (1999-09-15), iii) JP3693121B2 B2 — (2005-09-07), iv)
US6595746 B1 — (2003-07-22), v) DE69812722T T2 (2004-01- 29), vi)
JP2002513117T T — (2002-05-05), vii) US6062819 A (16-05-2000), viii) EP
1082545 B1 (03-03-2004), ix) US6508626 B1, x) DE69915283D D, xi) JP4405966
(B2) (2010-01-27). Available on request.
Patent xi won the commendation of the Japan Institute of Invention and
Innovation in November 2010. References [1], [4] and [5] best demonstrate
the quality of the research.
This work was supported by two major international research grants. One
of £800k from Ebara Corporation of Japan (1995-2003) and a €1.2M Eureka
project with sponsorship from ABB Turbo, Sulzer Turbo (now MAN Turbo) and
HV-Turbo (now part of Siemens) and collaboration with ETH Zurich
(1999-2002).
Details of the impact
Since 2008, major turbomachinery manufacturers have adopted ADT's
TURBOdesign™ software suite in ever increasing numbers, as they sought to
achieve improvements in their design processes and manufacturing methods,
and thus unlock benefits such as increased efficiency of their
turbo-machinery and reductions in CO2 emissions. Some of the
key impacts arising from the UCL research are summarised below.
Delivering more efficient design methods for the turbomachinery
industry:
A number of the leading turbomachinery manufacturers have changed their
design systems to access the benefits that arise from the use of ADT's 3D
inverse design approach. For example, in pumps manufacturing, four of the
top ten global manufacturers, including Ebara Corporation, use
TURBOdesign™ in their design workflow [a]. Also the world's leading fan
manufacturer, ebm-papst, uses TURBOdesign™ in most of its divisions; one
of the company's engineers noted: "Our experience shows that
TURBOdesign™ can reduce development / design time, improve efficiency
and reduce noise of fan blades" [b]. Other leading companies in
turbomachinery application areas such as aeroengines, automotive cooling,
Central Processing Unit (CPU) cooling, cryogenic and air-conditioning
applications and power generation have switched to using TURBOdesign™ in
their design systems [c].
Many of these manufacturers are finding that using the code reduces the
development and design time for their new designs and improves
performance. For example, the Director of R&D at Andritz Group said in
a March 2013 article in Pumps and Systems magazine that the "the [ADT]
software considerably supported the pump manufacturers to accelerate the
hydraulic design process" [d]. In another article in Machine Design,
Mr Toru Iwata of Daikin Industries said: "The software helped us reduce
development time and slash material use, as well as develop new models
of high-efficiency fans" [e].
Enabling improvements in manufacturing methods in the
turbomachinery industry: In the turbomachinery industry
various methods are used for manufacturing the vanes and blades. For low
volume vane and blade manufacture within aerospace applications, it is
usual that CNC machines are utilised. For high-volume applications, such
as turbochargers, it is customary to use casting or in some cases a flank
milling process for blades with straight filaments, as these approaches
result in lower manufacturing costs.
In 2011, Cummins Turbo Technology, one of the leading manufacturers of
heavy-duty diesel turbochargers globally, decided to take into high-volume
production a turbocharger compressor with 3D blades. This was designed
using the 3D inverse design method TURBOdesign™ and machined by using a
5-axis point milling process. The point milling process can add between
15-20 per cent to manufacturing costs compared to flank milling or
casting. The main impetus for the company to make such a substantial
change in its manufacturing process was the fact that for 10 years they
had not been able to make any improvement in the performance of a baseline
turbocharger compressor, which had straight filaments, with direct design
methods. By using the inverse design approach an impeller could be
designed that was up to 3 points more efficient through most of the
compressor map. However, this impeller had a 3D geometry and required a
significant change in manufacturing process. The significant improvement
in performance of the new compressor, in the eyes of Cummins Turbo and its
major engine manufacturers, more than justified the additional costs
associated with the changes to manufacturing method [f].
The TURBODesign™ software makes it easier to design 3D blade and vane
geometries with high efficiency, and with the current rate of reduction in
the cost of the point milling process it can create important
possibilities for further improvement in turbomachinery component
efficiencies.
Increased turbomachinery efficiency and reduction of CO2
emissions: One of the major impacts of industry's adoption of
ADT's inverse design method is a significant improvement in the efficiency
of turbomachinery. Earlier research had shown that breakthrough designs
made possible by this approach can lead to significant improvements in
pump stage efficiency of up to 6 points (see outputs [5] and [6], above).
Similar levels of performance improvement are being achieved by industrial
use of the inverse design method. For example, in 2013, Daikin Industries
confirmed that they had improved the efficiency of an air-conditioning fan
by 10% by using the inverse design method [e].
Likewise, performance improvements have been achieved in other industries
such as pumps, automotive and power generation through the adoption of
this technology. For example in 2008, RR Marine, a major manufacturer of
large-scale marine waterjets, was able to improve the propulsive
efficiency of their marine waterjets by 3-5% by using ADT's software
TURBOdesign™ [g]. Furthermore, they obtained a significant reduction in
manufacturing cost of their waterjets, which came on the market in 2013
[g].
These efficiency savings have consequent environmental benefits by
reducing CO2 emissions. ebm papst has been using the inverse
design method since 2006, and claimed in a 2008 advert in The Economist
magazine that "If for ventilation, refrigeration and airconditioning,
European industry switches to the latest generation of fans (designed by
ebm-papst), 16 Million tons of CO2 emission
will be cut and 4 coal fired power stations will be made redundant"
[h].
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Sources to corroborate the impact
[a] Case study on Ebara (http://www.adtechnology.co.uk/case-studies/ebara-manufacturing-system-hydraulic-parts)
corroborates the company's use of the software. Available on request.
[b] ADT case studies on epm pabst confirm that TURBODesign™ is the
standard design tool in use at the company and the quote from the
engineer. Available on request.
[c] For a range of ADT's customers, see:
http://www.adtechnology.co.uk/adtsearch/node/_/cas_/_/cas_/_
[d] Quote from Andritz Group in "Design Software Increases Hydraulic
Efficiency", Pumps & Systems, March 2013, p 44, http://pump-zone.imirus.com/Mpowered/book/vps13/i3/p44
[e] Quote from Daikin Industries, in "Inverse design code boosts HVAC fan
efficiencies", Machine Design, January 2013, http://machinedesign.com/news/inverse-design-code-boosts-hvac-fan-efficiencies
[f] Pages 9 and 10 of Cummins Turbo Technologies' HTi magazine confirms
Cummins' use of ADT software and the 3 percentage points efficiency
improvements. http://bit.ly/15W2vnK
[g] A letter from the Senior Hydrodynamicist at Rolls Royce Marine
confirms the 3-5% improvement in propulsive efficiency of the company's
next generation of marine waterjet pumps using the ADT system. Available
on request.
[h] The epm-pabst advert is in The Economist, 10 October 2008. Available
on request.
[text removed for publication]