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Re: Europa-List: Re: Contact detail & Help

Subject: Re: Europa-List: Re: Contact detail & Help
From: Bud Yerly <budyerly@msn.com>
Date: Sat, 30 Jun 2012 12:03:42
To all,
>From testing with the Airmaster AP420 vs 332 a couple of notes on prop 
vibration/noise.
I do not intend to comment on the different brands, only the differences 
between a three and two blade prop both designed for and tested on the 
Europa..

A two blade AP420 with Sensenich Blades vs. three blade AP332 with Warp 
Drive Blades non tapered.  Engine 914, Aircraft Europa XS Trigear.

First, at cruise the Rotax only turns nominally 2050 RPM prop speed and 
the prop length is limited to 64 inches, so the tip compression or mach 
whack noises are minimized.  The limited cruise RPM really degrades the 
performance of a propeller.  The gear box limit of 2.43 reduction 
imposes a problem in cruise, but allows longer blades and the ability to 
deliver more torque to a prop.  In essence, the slow prop shaft RPM and 
limited length means the prop angle at cruise must be increased to 
absorb the torque of the engine.  The higher angle of attack of the 
blade makes for some interesting problems for the blade designer.  
Takeoff,  vs. climb performance vs. cruise performance will be 
significantly different conditions and design criteria for the blades 
and the downwash off the blades as they pass the cowl are different. 

The next thing is that the area of the blades must be near equal for 
proper comparisons.

Finally, the Europa thrust line has a near zero angle at cruise, but 
nearly 8 degrees during initial climb at max climb speeds of 65 and 75 
for angle and rate.

Comment:  Quality propeller blade manufacturers have very consistent 
mass balance and airfoil sections blade to blade, so vibrations due to 
balance are minimal.  Hand cut or custom props, or defective props (yes 
we had one Sensenich go out of balance due to an internal balloon 
failure) must be sorted out. The slightest profile difference makes a 
difference in both noise and vibration.

The two blade pulses, due to AOA during climb, does give a change in 
sound outside the aircraft as well as inside.  The power pulses of each 
blade passing through the windshield arc allows the two blade to make an 
audible (somewhat irritating) pulse across the windshield and cowl face.
The three blade prop increases the frequency of the power pulses and 
smooths out the pulses affects and although the decibels aren't terribly 
different, the noise (what is irritating to the ear) is less for the 
three blade.  Tapered tips are less noisy than square tips.  Cutoff tips 
give a sharp tip sound when compared to a swept tip.  Swept tips have 
lower initial inertia and lower tip drag at higher prop speeds.

At or near cruise, this pulsing noise is diminished significantly at the 
shorter blade lengths.  Long blade lengths tend to be noisier due to 
their effect on more of the aircraft, most noticeably is the windscreen 
pulsing noise transferred into the cockpit and to your ears.

On tests with the 76 inch long blades, the two blade is very loud in 
comparison, diminishing with a shortening of the blade length.  
The 76 inch long two blade requires ANR headsets for comfort, and the 
windscreen in the Rans and Kitfox actually moves like a drum as the 
blade passes.  The two blade at the long lengths is faster on top end as 
I approached the aircraft's VNE.  High altitude performance was a bit 
better with the two blade also.  This is, in my opinion, not not due to 
the differences in two vs three blade as much as the difference in blade 
areas, thickness and taper plus the slight advantage in efficiency of 
any two blade over a three blade (remembering the most efficient prop is 
a single blade).  The Sensenich blades are thicker and wider of chord on 
the longer blades.  The Warp Drive blades of that length were tapered 
tips because of the very long length and the difference in rotational 
inertia.  We went to the wide chord blade on the 332 at 76 inches (not 
good for the sprag clutch on the Rotax with its higher inertia on start) 
but it still was a bit slower at top end and had only a tiny decrease in 
static thrust than the 76 inch long Sensenich blades on the 420.

Tip design also has an effect.  A swept tip tends to be quieter on the 
very long props, but is less effective on the shorter props.  A number 
of designers have toyed with better blade designs but the problem is 
each experimental is different.  What works on a Vari Eze is not going 
to work for a Ran's or Europa even with the same engine...
I talked with Steve and Mike at Sensenich about the 64 inch two blade, 
but they had to admit, it isn't working as well as they would like.  The 
twist, area profile, taper and airfoil section have got to be tweaked to 
get the most out of the Europa/914 combo.  How many blades will we sell 
to pay for all the tweaking and testing that comes into the blade 
manufacture equation.  Yes, mass produced blades must operate 
efficiently but also sell.  Right now the Sensenich market is in the LSA 
market which doesn't need all that tweaking because they only go 120 
Knots.  We in the Europa commuity are looking for 150 Knots at 10,000, 
which is a totally different blade design.  Not that the casual observer 
would notice the difference, but to those of us flying efficient glass 
aircraft, we notice the difference.  Again, I am not getting into whose 
manufactured prop is better, because tests have to be done on the same 
aircraft, same CG, same conditions to be valid.  My Europa is 
significantly faster (15 knots) than another XS in the shop.  Same 
airplane, landing gear, engine, and prop, just different in oh so many 
little ways... CG, wheel pants, cowl seals, door fit, trim of the 
aircraft, flap droop, wing gap seals, engine isolation mount age, etc.

Another area of vibration is the wind angle during taxi, compression 
braking with the prop at high speed, resonance effects, Rotax gearbox 
(straight cut verses taped cut). There are certain aircraft where the 
vibration of the prop in one, or all of the above is quite irritating. 
The Warp Drive, does drive me nuts during taxi with a quartering tail 
wind as my engine /prop combo sounds terrible during taxi and if I dive 
into the pattern with the prop at cruise (5000) at 130 Knots and lower 
the power setting further, I can feel the prop and gearbox lash and 
rattling noise. Entering the pattern at "Takeoff" setting diminishes 
that as does entering the pattern at lower speed.

Pusher designs have noticeable differences from the tractor types due to 
air flow disturbance across the blades, especially if a tail boom is 
below the prop.  Even the addition of an augmenter exhaust to only one 
side of the aircraft makes a difference in feel.

In my summary to Airmaster, I saw no difference in performance between 
the AP332 vs the AP420 in the Europa (64 inch prop length) but a 
noticeable difference in the longer 76 inch blades on the Kitfox / Rans 
S6 aircraft.  The two blade was lighter, easier to get the cowl off and 
on, and a bit noisier on the Europa.  Longevity of the blades depends on 
how much grass you intend to mow.


Have a great weekend,
I'm off to the shop.

Bud Yerly


  ----- Original Message ----- 
  From: GRAHAM SINGLETON<mailto:grahamsingleton@btinternet.com> 
  To: europa-list@matronics.com<mailto:europa-list@matronics.com> 
  Sent: Tuesday, June 26, 2012 2:27 PM
  Subject: Re: Europa-List: Re: Contact detail & Help


  Hi David
  Yes it probably is, but it's at low speeds and high power on climb out 
that the vibration is worst. 
  With multi blade props the problem isn't as bad. I'm not good enough 
at maths to explain why
  but I am just reiterating what Bruno Guimbal said years ago. He 
designed a very attractive looking helicopter I once saw at 
  the RSA Rally years ago. He seems to have moved on, haven't heard 
anything for years. Very experienced aerospace engineer
  who built a Vari Eze around 1978 which he flew to Leicester when our 
rally was there in 1979 I think.
  Graham


-------------------------------------------------------------------------
-----
  From: David Joyce <davidjoyce@doctors.org.uk>
  To: europa-list@matronics.com 
  Sent: Tuesday, 26 June 2012, 18:35
  Subject: Re: Europa-List: Re: Contact detail & Help


<davidjoyce@doctors.org.uk<mailto:davidjoyce@doctors.org.uk>>

  Graham, In my innocence I thought that the plane was designed so that 
in normal cruise attitude the engine axis was horizontal and the blades 
at equal AOA
  Regards, David Joyce, G-XSDJ


  GRAHAM SINGLETON 
<grahamsingleton@btinternet.com<mailto:grahamsingleton@btinternet.com>> 
wrote:
  > Karl
  > 3 blades will always be smoother because when the 2 blades are 
horizontal each blade sees a 
  > different AoA, especially with high angles of attack. This causes 
different thrist on the blades resulting 
  > in yawing oscillation of the airplane.
  > Graham
  > 
  > 
  > ________________________________
  > From: Karl Heindl <kheindl@msn.com<mailto:kheindl@msn.com>>
  > To: europa-list@matronics.com<mailto:europa-list@matronics.com> 
Sent: Tuesday, 26 June 2012, 14:57
  > Subject: RE: Europa-List: Re: Contact detail & Help
  > 
  > 
  > 
  > Hi Frans,
  > 
  > Thank you for the additional information. I will follow your advice, 
but probably not until next year.
  > If you are going to publish in the flyer, then some good pictures 
please of the radiator installations.
  > Also, a source for the rads.
  > 
  > You mentioned that the prop is not as smooth at lower rpm's. I have 
the same prop and I discovered a long time ago that the carbs need to be 
in sync 100% for a two-bladed prop. With three blades the carbs would 
need to be out of sync quite a bit before you would notice. I know, 
because I tried it by putting my original Warp Drive back on.
  > 
  > Karl
  > 
  > 
  > 
  > 
  > 
  > 
  > 
  >> Date: Mon, 25 Jun 2012 23:09:34 +0200
  >> From: frans@privatepilots.nl<mailto:frans@privatepilots.nl>
  >> To: europa-list@matronics.com<mailto:europa-list@matronics.com>
  >> Subject: Re: Europa-List: Re: Contact detail & Help
  >> 
  >> Hi Karl,
  >> 
  >> > I have been following your developments with great interest and I 
think
  >> > that the end result is just plain amazing.
  >> 
  >> Thanks!
  >> 
  >> > Now, top speed is very useful for testing drag improvements, but 
you
  >> > don't cruise at those speeds, do you ? When you are touring, what 
are
  >> > your preferred settings regarding speed, MP, rpm etc., and 
exactly what
  >> > is your fuel consumption then.
  >> 
  >> I found the sweet spot of the aircraft is with 27 inch MAP, where 
it
  >> usually cruises with a speed somewhere between 120 and 130 KIAS,
  >> depending on C of G and some other obscure factors. Fuel 
consumption
  >> used to be 16 to 17 liters per hour, but I have observed this year 
that
  >> the fuel consumption has increased to 18 liters per hour. Maybe the
  >> carbs need an overhaul or so.
  >> RPM is usually between 4800 and 5000 RPM, this feels best for the
  >> engine. I have a two blade prop and at lower RPM's it feels less 
smooth.
  >> Of course actual settings depend on various circumstances. With a 
strong
  >> head wind we usually advance the throttle a bit, with a tail wind 
we
  >> enjoy the lower fuel consumption of a lower power setting. We fly 
90% of
  >> our cruising with power between 26 and 28 inch.
  >> With higher power settings the fuel consumption goes up faster than 
the
  >> gain in speed. Other than in a car, a higher speed doesn't give any
  >> other feeling than a lower speed, it just gives the same sensation. 
One
  >> hour flying is still one hour flying. On a 3-hour trip I rather 
enjoy an
  >> additional 10 minutes flying and have a free meal than just 
cranking up
  >> the fuel consumption, paying more for less fun. AVGAS can be close 
to 3
  >> Euro's per liter over here, so saving 10 liters on a trip can save
  >> enough money to have a dinner for two! ;-) I love telling friends 
that
  >> flying there isn't more expensive than getting there by car.
  >> 
  >> > If the rest of us mortals wanted to implement some of your 
changes
  >> > without too much expense, what would you recommend ?
  >> 
  >> There isn't much money involved actually. The radiator costs about 
300
  >> Euro's, the heat exchanger a bit less. You can do without the heat
  >> exchanger, I have been flying one summer with the stock oil 
radiator fed
  >> by a 2" Scat tube via a wedge diffuser. Apart from the long warm up 
time
  >> it was quite an improvement over the tandem setup. Best thing to do 
is
  >> to scrap the stock coolant radiator, dog house, duct and associated
  >> hardware and just install a thin radiator in a 45 degree angle in 
front
  >> of the exhaust and turbo.
  >> 
  >> The main hurdle here is to shape a new underside of the cowling. 
You
  >> have to be brave enough to cut the dog house away, and then insert 
a
  >> block of blue foam and start cutting, rasping, sanding until you 
have
  >> the shape you desire. Anyone who wants to make a mold out of my 
cowling
  >> is welcome to do so, provided I'm allowed to use that mold to make 
a new
  >> light weight carbon cowling for myself. ;-)
  >> 
  >> BTW I'm not the only one who devised something like this. See the
  >> attached picture. This is another configuration with a thin 
radiator in
  >> a 45 degree angle, although it lacks a cowl flap and heat exchanger 
for
  >> the oil. (Oil is cooled by a radiator, fed by a NASA duct on the 
port
  >> side, you can see it on the picture). Also this owner claims very 
good
  >> results with his setup on his 914 engine. The key really is to use 
a
  >> thin radiator and mount it at the belly so the "used" air can take 
the
  >> heat of the exhaust with it, and enjoy the benefits of a very sleek
  >> cowlng, excellent cooling, low pressure losses, and minimal cooling 
drag.
  >> 
  >> Anyway, my cooling design is not an exclusive invention of me but 
the
  >> combination of ideas and experiments of multiple Europa owners who
  >> believed that the cooling of the Europa could be improved other 
than by
  >> using draggy brute force solutions.
  >> 
  >> > What is the part number for the
  >> > heat exchanger and exactly where did you install it ?
  >> 
  >> See picture, taken from under the engine. The heat exchanger is 
mounted
  >> behind the engine. This was the first setup, with the stock coolant
  >> radiator, hence the configuration of the coolant hoses pointing
  >> downwards. In the current design the hose routing has been changed 
to
  >> accomodate for the thin belly radiator.
  >> If you really want to go this way, contact me privately for more 
info.
  >> One caveat though: this heat exchanger has very thin canals and is 
not
  >> compatible with Evans coolant due to its viscosity. I use it with 
50/50
  >> without problems.
  >> 
  >> > It also had a very
  >> > small (8AH?) battery.
  >> 
  >> I also have a small 8Ah battery, never needed anything more than 
that.
  >> But I have a second alternator (mounted on the vaccuum pad) so I 
don't
  >> ne//www.matronics.com/Navigator?Europa-List" 
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