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Presspley Crack Investigation

An official lab tested the smart turbo to determine why it cracked

Modification Details

In 2004, a disappointed smart customer sent their cracked turbo off to Presspley for analysis. was an Australian company who specialised in simulation and analysis.

The investigation was interesting but disappeared when Presspley went bust.
So here it is again in all its glory (with some of the poor English and grammar sorted).


Dated 24/10/04


Visual lnspection
Tensile Test
Chemical Analysis


The fuel economy of a Smart Pulse, was found to be dropping from a typical 66mpg
to around 40mpg, with no difference in vehicle use. 
Having reported this to his local
Smart Centre, and have them try to
 find the problem, no problems were found.

At a later date after the car had run out of warranty but with the same problem still
persisting, the vehicle was serviced at a
 Mercedes Benz dealer. The exhaust
manifold/turbocharger unit
 was found to be cracked in two places.


The Smart car manifold unit has had a considerable number of redesigns. The
unit being investigated is a Garrett GT12 turbo with
 part number: A 160 096 0599

Other numbers etched onto the in flange are: 000 T926 V001 

The manifold/turbo was received in the as removed condition. The unit appeared
to be in good condition except for the two large cracks in between the 3 cylinders.
The extent of the cracking can be seen in the photographs.


Cross-sectional specimens were cut from the sample and mounted in metallographic moulds.
These were then progressively ground before final polishing with 0.05mm colloidal silica
suspension, to give a scratch-free surface and reveal the true grain structure.

These were viewed in the as-polished condition first, then etched and viewed
again at magnifications up to x1000.
 Etching to a satisfactory level was carried
out by swabbing the polished surface with 5% Nital solution.

The microstructure was that of a Ni-Resist cast iron. Porosity was noticed
throughout the section of the casting, however it is not considered to be excessive.


A round tensile specimen was machined from the manifold and tested
using an lnstron 5582 tensile testing machlne. Results are shown below.

0.2% Proof stress (MPa) = 251
UTS (MPa) = 467
Elongation (%) = 16.5


A sample was tested using the Optical Emission Spectroscopy method.
Results can be seen in the table below.

Carbon, C = 2.10
Silicon, Si = 3.98
Manganese, Mn = 0.581
Nickel, Ni = 34.065
Copper, Cu = 0.086
Chromium, Cr = 1.852
Sulphur, S = 0.002
Molybdenum, Mo = 0.125

This is a typical composition of a Ni-Resist cast iron.


Mechanical properties appear typical of those expected for a cast Nickel-alloy.
The chemical composition is similar to that of a Ni-Resist cast iron.

Type 1 Ni-Resist should not be used in applications involving service above 1300° F (430° C).

Austenitic alloys may be softened and homogenized by heating to 1800-1900° F
(980-1040°C) for 3 to 5 hours and air-cooling. This 
breaks down some of the
carbides and most of those remaining will 
be spheroidised.

lf the car was driven under load for 3-5 hours causing exhaust temperatures to become
very hot, then the engine left to cool; heat
 treatment mechanisms could have taken place.

Thermal gradients across the manifold result in thermal shock, causing
internal residual stresses which could have lead to crack

Some inter-dendritic shrinkage is evident in the vicinity of the cracking.

Cracks always propagate through a material following the weakest path, which is through
the gaps between the shrinkage. 
Shrinkage is caused by poor casting design and technique.

On inspection of the vehicle, it is noted that the replacement manifold/turbo is part number A 160 096 0699, which is a redesign and features additional material around the areas which cracked.

This suggests the cracking was caused by poor design, which is most likely being addressed on a case by case basis by Smart (UK) rather than recalling all the vehicles sold due to the cost involved.


There are three factors that are generally causes for the problem, although no one is usually to blame alone - it is a combination of the three, in any percentage, that generates such cracks.

1) Mass of the turbo unit (and exhaust if hung off the turbocharger) with combined
shock loading from undulating road
 surface not being fully considered.

2) Insufficient allowance for expansion of the material due to the intended design, method or deviation of manufacturing from that of the design of the manifold/ cylinder head fixings.

3) Incorrect material thickness to accommodate the expansion and contraction of
the manifold based on the change of section
 of manifold, exhaust gas temperature
within the manifold, and
 method of attaching to cylinder head.

Other factors, such as the material not meeting the required specification, whether
at the design or manufacturing level, is yet
 another factor that cannot really be
commented on. Incorrect ignition
 advance is one such example.

This problem used to be quite common, but it is very surprising that it is occurring on a
modem vehicle. The use of modem
 computational analysis programmes such as Ansys
that can
 calculate combined thermal and mechanical stresses should (with suitable safety
factors) eliminate this - again assuming the 
turbocharger is manufactured correctly. from
the appropriate
 material, that it is fitted and used according the OEM’s specification.

The cross section, together with the mounting arrangement is at fault - i.e. it is a design
issue. Note that the cracks are propagating
 at the points around the manifold fixings.
It appears all bolt holes are
 the same size also. I would expect a greater hole size in the
 at either end of the manifold to allow the manifold and head to expand & contract
relative to each other, maintaining its position
 with the centre studs.

This is even more apparent when you consider the temperature of the manifold is not consistent
along its length. The end furthest from the turbine housing has one cylinders worth of exhaust
gasses (and heat). The second cylinder experiences two cylinders worth, whilst the third has one
cylinders worth but is closest to the compressor housing – the hottest part of any turbocharger.

Petrol engine manufacturers are faced with ever-tightening emissions regulations
imposed by American. Japanese. and
 European legislation. To meet future HC and CO
limits, and to
 improve fuel economy, automotive engine manufacturers are looking towards
running air to fuel ratios near lambda = 1 for full load engine

Traditionally full load air I fuel conditions have been in the region of lambda = 0.9 to
improve maximum engine power output and
 maintain engine durability. The excess fuel under
these conditions
 has a cooling effect on the exhaust temperature and has allowed engines
to be below 1000°C in exhaust temperature. The move
 towards lambda = 1 will remove
this fuel cooling effect and will yield
 exhaust temperatures up to 1050°C.

Today's turbochargers are designed and qualified for existing high temperature
gasoline applications. This has been a delicate balance
 of design, material technology,
and cost. The move to 1050°C
 exhaust temperatures has prompted the Garrett Turbocharging Group to redefine this balance for turbochargers.


Photograph 1: Overall shot of Manifold/turbo. as received, with arrows highlighting cracks.


Close up of cracking.

Close up shot of crack 1, as received.

Close up shot of crack 2, as received.

Showing complete penetration to inner face of manifold at crack 1.

Showing complete penetration to inner face of manifold at crack 2.

x100 magnification micro-section in the as polished condition.
Structure shows small graphite nodules with columnar cementite.

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