Hi Paul,
hope you remember your visit in Wiener Neustadt some years ago?
Meanwhile I found my way via WankelSuperTec to AVL Schrick, as you can
see in the signature below. Unfortunately this means that I am
completely out of the Rotary business, but still more than enthusiastic
about it and working on my private Rotary projects, see attachment.
That's why I want to subscribe to your newsletter, just to stay in
touch
and to see what else is going on in the Rotary world - just in case!
And
to assist where ever possible from this end.
Looking forward to interesting discussions!
Mit freundlichen Grüßen/
Best regards
Martin Rühe
Motorenentwicklung Versuch
Engine development
AVL SCHRICK GmbH
Walter-Freitag-Straße 16
42899 Remscheid
DEUTSCHLAND/GERMANY
http://www.avl-schrick.com/
Yes I do. How are you Martin? Good to hear from you.
Here are some pictures from that time in addition to the three you
sent.
There is a guy and company called Rotamax in Ohio that really needed
your
services a couple of years ago. They failed to solve the charge
cooling problems
and stopped doing biz recently. If he ever starts up again he would
do well to
hire you at any salary.
I am working hard on getting turbo compound accepted and hopefully
that includes the rotary. If the piston engine community accepts
it so too Mazda hopefully. I was just in Oxford giving a presentation
on TC to the Formula 1 engine management engineers. Now that
Thielert stumbled
badly hopefully Chris Dries, owner of Diamond Aircraft, will
understand the
wonderful Wankel resource he is sitting on :)
Again good to hear from you.
Paul Lamar
thanks a lot for your quick reply! And for the pictures that bring
back some
very happy memories indeed!
I had spotted the Rotamax homepage a couple of months ago when I had
to spend
some time in the www due to lack of business here at AVL Schrick. I
wasn't aware
they went out of business though. Pity that. I wish I had known that
they could
have done with my support as I am now, working for AVL Schrick,
completely out
of the Rotary trade, as mentioned earlier.
Talking about Christian Dries: Check out
http://www.austroengine.at/, in
particular the news! Pity he made me leave some three years ago. But
admittedly
the two years with WankelSuperTec paid well for having to leave
Diamond!
Good to hear from you as well, we'll stay in touch!
Regards,
Martin
---------------------------
http://en.wikipedia.org/wiki/Cessna_172
172TD
On October 4, 2007 Cessna announced its plan to build a
diesel-powered Cessna 172 model starting in mid-2008. The planned
engine was to be a Thielert Centurion 2.0, liquid-cooled, two-litre
displacement, dual overhead cam, four-cylinder, in-line,
turbo-diesel with full authority digital engine control.[12] The
engine produced 155 hp (116 kW) and burns Jet-A fuel. The engines
were to be installed at the Cessna Skyhawk factory in Independence,
Kansas under an STC. The new model was designated the 172 Skyhawk
TD, indicating "Turbo Diesel".[1]
Cessna had taken special measures to ensure that the Skyhawk TD
would be only fueled with Jet-A and not misfueled with avgas. These
included placards, key-shaped tank fillers that only accept jet fuel
nozzles and a spring-loaded door activated with a jet-fuel nozzle.
The aircraft was planned to be certified for Jet-A only and not
automotive diesel.[13]
The TD was to be equipped with only one engine control, referred to
as a "power control", although it resembled the push-pull style
throttle used in previous 172 models. The prototype has no
carburetor heat or mixture control. The prototype is equipped with a
constant speed MT propeller, but this is controlled automatically
and there is no propeller rpm control.[13]
The TD was designed to have the same gross weight as the "S"
Skyhawk, 2,552 lb (1,158 kg), but at 155 hp (116 kW) was intended to
have 25 hp (19 kW) less than the "S" model. Because it is
turbonormalized the prototype's engine produces full power at all
altitudes and actually puts out more power than the "R" and "S"
models above 8,500 feet (2,600 m), where the normally aspirated
powerplant's output drops off.[13]
To account for the fact that Jet-A has a higher density than avgas
Cessna planned to reduce the tank capacity on the TD to 44.6 US
gallons, giving the aircraft a similar range to other models, due to
the better efficiency of the diesel engine. The Thielert 2.0 is
reported to burn 5.8 gal/hr at 5,000 feet (1,500 m) and 75% power.
This compares to 8 gal/hr at the same power setting and altitude for
the "R" model and 10 gal/hr for the "S" model Skyhawks.[13]
Even with the reduced fuel tank capacity the full fuel payload of
the TD will be 445 lb (202 kg)[13] compared to 519 lb (235 kg) for
the Cessna 172S[14] and 440 lb (200 kg) for the 172R.[15]
Direct operating costs for the TD were forecast to be USD$96.39 per
hour versus USD$101.81 for the higher powered "S" model. While the
TD would burn less fuel per hour its engine replacement costs at
2400 hours, instead of overhaul, would almost make up for the
difference, although these numbers will change as the price of fuel
changes in future years.[13]
In early 2008 certification had been planned for the summer of 2008
and Cessna had forecast delivering about 125 TDs before the end of
2008.[13]
The TD was intended to sell for about USD$15,000 more than the top
of the line "SP" Skyhawk and $35,000 more than the "R".[13] Base
price was initially advertised as USD$269,500 versus USD$254,500 for
the "SP" or $234,500 for the "R".[16]
Early orders for the TD were strong with most of the demand from
flight schools and non-US operators.[13]
In April 2008 the 172TD's engine manufacturer, Thielert filed for
insolvency under German law, throwing the future of the aircraft
into doubt.[17][18][19][20]
On May 1, 2008 Cessna announced that they have cancelled all 2008
deliveries of the 172TD due to the insolvency of Thielert. The
company stated: "At this point we have decided that we will not
deliver 172TD aircraft during 2008, and we have informed our
customers accordingly."[21] Cessna has indicated, however, that they
will proceed with the certification of the 172TD.[22]
Cessna has indicated that they still wish to produce a diesel 172 as
market demand is strong for this aircraft with over 100 orders.[21]
--------------------------------------------------------------
Appears to me Chris Dries is going down the same Mercedes A class
engine
dead end road.
Twin Star Claims
50% power 7.2 gallons per hour 135 KTS 155 MPH
60% power 8.8 gallons per hour 138 KTS 159 MPH
90% power 14.4 gallons per hour 163 KTS 187 MPH
135 HP each or 270 HP total
90% 243 HP
14.4 gallons is 99 pounds of diesel fuel per hour. BSFC = .4 pounds
per HP hour. A regular leaned Continental is close to that BSFC and
a non-leaned Lycoming is .45 with out the extra weight of the
diesels. The rotary is lower weight and
.47 BSFC.
50% power is 135 HP
7.2 GPH or 50 pounds of diesel fuel per hour or BSFC .37 pounds per
HP hour.
Nobody is going to buy a $750,000 twin airplane and cruise it at 163
KTS let alone 135Kts except perhaps flight schools that need twins.
People are looking
for something that flies well over 200 Kts for that amount of money.
The hot tip is an engine that runs on car gas like the Mistral
Wankel rotary.
Car gas is over $1.50 cheaper per gallon right now than 100LL and
about 50 cents cheaper than Jet A. This is due to the fact there is
only 15% diesel fuel in a barrel of crude while there is 30% gasoline.
Paul Lamar
Hi Paul. That chart for 30% gas and 15% diesel is a bit out of date.
That was the approach taken in the past with simple distillate
refineries and shows what they got out of a barrel. Currently, fractal
distillation refineries get 40% gas from a barrel
http://science.howstuffworks.com/oil-refining4.htm while others refine
nearly the entire barrel into diesel fuel. It all depends on what you
want to make from the crude and what the content of the crude it ( how
many carbons are in what chains.) and the process of cracking long
chains into the diesel range and joining short ones up to the diesel
range. They can now taylor the output to what they want to sell using
full-range full-range, coker, Hydrotreater, and hydrocracker distillate
methods.
Stuart Petroleum is build a diesel refinery in Australia
http://uk.reuters.com/article/oilRpt/idUKSYD9796620070808
This Indiana refinery has retooled to get much more diesel out of a
barrel. They say in part "U.S. refining is not really set up for diesel
fuel?it?s always been driven by gasoline"
http://countrymark.com/node/320
But, it is a fact that with ULSD it costs more to make diesel than
gasoline http://www.eia.doe.gov/oiaf/servicerpt/ulsd/appendix_d.html
adding insult to injury that in the US we usually tax diesel at a higher
rate than gasoline.
-dave
The data is as of 2007.
They are going to make a lot of money as diesel fuel prices are going
up in the UK as well as on the continent. When I was in the UK last
week diesel
fuel was higher than gasoline. Here in CA it is 30 to 50 cents higher.
Of course all that special refining adds to the price.
The tax is as it should be as 80,000 pound trucks are a lot harder
on the roads and bridges.
Paul Lamar
Here in Michigan, diesel is about 50% higher in price than gas - $3.53
vs. $2.76, but this still is not the fair share for our trucking
industry. We allow 120,000 over the road and 10% of the trucks violate
this to 160,000 range because it is cost effective. As a result, our
roads disintegrate in short order costing us all. They do not have an
elastic demand for fuel like consumers do, so the price of diesel does
not swing as much as gas.
On the diesel side, all these heavy trucks spew out tons of NOx and
soot. They certainly produce more pollution that if all our cars were
suddenly 50 mpg diesels w/o the diesel particulate filters. But, its not
about what makes sense, but about money.
-dave
There is a mistake here. Gas really does typically cost $1.53 and diesel
really does cost $2.76 here in the Great Lake State of 10,000 lakes.
http://www.detroitgasprices.com/ Some places gas is as low as $1.43 and
diesel as low as $2.43
http://www.detroitgasprices.com/map_gas_prices.aspx
-dave
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