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2-blade props

 
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kheindl(at)msn.com
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PostPosted: Thu Apr 15, 2010 4:43 pm    Post subject: 2-blade props Reply with quote

Graham,
 
I am shure you are correct, but in my experience I have not noticed more vibration, once the carbs ar well balanced.
Advantages are  -  less weight, less money, less maintenance, easier to balance, easier to ship in one piece, better visibility when feathered on MG, less drag, and bottom cowling comes off easily, without having to remove tailpipe etc.
Why do most GA aircraft have 2-blade props  ?
 
Karl
 


 


 
Date: Thu, 15 Apr 2010 22:54:04 +0000
From: grahamsingleton(at)btinternet.com
Subject: Re: Weight reduction - Brake Discs
To: europa-list(at)matronics.com

.ExternalClass DIV {;} Frans
in theory only is a 2 blade more efficient, you get more vibration that can't be balanced out. More vibration gives more disruption to laminar flow so more drag.
This is also why 2 blade windmills are more likely to throw blades. 2 blades don't cope with non axial air flow, multi blades do
Graham


From: Frans Veldman <frans(at)privatepilots.nl>
To: europa-list(at)matronics.com
Sent: Thursday, 15 April, 2010 23:14:32
Subject: Re: Weight reduction - Brake Discs

Get a two blade prop. One blade of a CS prop is 4Kg's worth. Apart from
that, it cruises more efficiently, cutting down on fuel (read: weight).

Frans

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grahamsingleton(at)btinte
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PostPosted: Thu Apr 15, 2010 11:50 pm    Post subject: 2-blade props Reply with quote

Karl
Cost I suspect. Most things are a compromise

Graham,

Why do most GA aircraft have 2-blade props ?

Karl







Date: Thu, 15 Apr 2010 22:54:04 +0000
From: grahamsingleton(at)btinternet.com
Subject: Re: Weight reduction - Brake Discs
To: europa-list(at)matronics.com

.ExternalClass DIV {} Frans
in theory only is a 2 blade more efficient, you get more vibration that can't be balanced out. More vibration gives more disruption to laminar flow so more drag.
This is also why 2 blade windmills are more likely to throw blades. 2 blades don't cope with non axial air flow, multi blades do
Graham


From: Frans Veldman <frans(at)privatepilots.nl>
To: europa-list(at)matronics.com
Sent: Thursday, 15 April, 2010 23:14:32
Subject: Re: Weight reduction - Brake Discs

Get a two blade prop. One blade of a CS prop is 4Kg's worth. Apart from
that, it cruises more efficiently, cutting down on fuel (read: weight).

Frans

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rampil



Joined: 04 May 2007
Posts: 870

PostPosted: Fri Apr 16, 2010 3:26 am    Post subject: Re: 2-blade props Reply with quote

....most commercial GA aircraft have two blade props...
Actually as can be seen convincingly in a stroll about Sun and Fun
today, any new, high performance aircraft , i.e., Cirrus, Cessna,
Mooney, Lancair, etc., etc., has 3 blades.

Just because most aircraft designed 30 years ago or earlier had
two blades doesn't mean that it was best for aerodynamics, just
best for the marketplace at the time.

In the end I think Graham is correct, it was just about money.

Reporting from under the old Oak tree with the Europa Team!
Regards,

Ira


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Gilles.Thesee(at)ac-greno
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PostPosted: Fri Apr 16, 2010 3:42 am    Post subject: 2-blade props Reply with quote

Ira and all,
Quote:
Actually as can be seen convincingly in a stroll about Sun and Fun
today, any new, high performance aircraft , i.e., Cirrus, Cessna,
Mooney, Lancair, etc., etc., has 3 blades.

Apart from what Karl said, the number of blades has something to do with

the prop *solidity* necessary to transfer power. The aircraft you cite
have powerful engines, hence the tendancy to increase the number of blades.
Quote:
Just because most aircraft designed 30 years ago or earlier had
two blades doesn't mean that it was best for aerodynamics,

Our airplane and two-blade prop were designed just a few years ago, and

they are quite efficient aerdynamically.
Remember that more blades means more drag (I also owned an unlimited
aerobatics airplane with a 3 blade, and we performed comparative tests
with a 2 blade).
In some cases, 3 blades are needed with low power (100 hp) in order to
reduce prop diameter for clearance reasons.

Quote:
In the end I think Graham is correct, it was just about money.

Weight, parts count and efficiency also play a role.


Best regards,
--
Gilles
http://contrails.free.fr


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kheindl(at)msn.com
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PostPosted: Fri Apr 16, 2010 5:08 am    Post subject: 2-blade props Reply with quote

Graham,
 
Yes, every choice has its pros and cons. If it hadn't been for my MG project, I would have been quite happy to carry on with the Warp Drive. It performed well, and you can't beat the exterior carbon finish, as opposed to painted or varnished propellers.
But I also had to have feathering, and the Airmaster hub had become very expensive. I am not really wild about automatic pitch control; I would prefer just manual, with an accurate display in percent or degrees of pitch. I don't think there is such an animal.
 
Karl


 
Date: Fri, 16 Apr 2010 07:32:26 +0000
From: grahamsingleton(at)btinternet.com
Subject: Re: 2-blade props
To: europa-list(at)matronics.com

.ExternalClass DIV {;} Karl
Cost I suspect. Most things are a compromise

Graham,
 
Why do most GA aircraft have 2-blade props  ?
 
Karl
 
 


 
Date: Thu, 15 Apr 2010 22:54:04 +0000
From: grahamsingleton(at)btinternet.com
Subject: Re: Weight reduction - Brake Discs
To: europa-list(at)matronics.com

.ExternalClass DIV {;} Frans
in theory only is a 2 blade more efficient, you get more vibration that can't be balanced out. More vibration gives more disruption to laminar flow so more drag.
This is also why 2 blade windmills are more likely to throw blades. 2 blades don't cope with non axial air flow, multi blades do
Graham


From: Frans Veldman <frans(at)privatepilots.nl>
To: europa-list(at)matronics.com
Sent: Thursday, 15 April, 2010 23:14:32
Subject: Re: Weight reduction - Brake Discs

Get a two blade prop. One blade of a CS prop is 4Kg's worth. Apart from
that, it cruises more efficiently, cutting down on fuel (read: weight).

Frans

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frans(at)privatepilots.nl
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PostPosted: Fri Apr 16, 2010 7:00 am    Post subject: 2-blade props Reply with quote

On 04/16/2010 01:26 PM, rampil wrote:
Quote:
....most commercial GA aircraft have two blade props...

Quote:
Actually as can be seen convincingly in a stroll about Sun and Fun
today, any new, high performance aircraft , i.e., Cirrus, Cessna,
Mooney, Lancair, etc., etc., has 3 blades.

It has a lot to do with sound. A 3-blader produces less sound.
Furthermore it has less vibrations, and to some folks looks sexier.

Performance is another subject.

A 2-blade prop IS more efficient. The tips of the prop slice through the
air with almost the speed of sound, if you have two tips instead of
three, you reduce drag quite a lot.
If is the same question versus a two wing airplane or a bi-plane. A
bi-plane has more drag because it has more frontal wing surface. More
wings is not more efficient, just like more propeller blades is not more
efficient.

My propeller still converts the same amount of engine power to thrust,
but it has less frontal surface slicing through the air. Once I' flying,
I will be happy to share performance data.
And no, no first flight today. Sad The whole airspace has been shut-down
because of the volcanic ash.

Quote:
Just because most aircraft designed 30 years ago or earlier had
two blades doesn't mean that it was best for aerodynamics, just
best for the marketplace at the time.

Well, then this must have been the reason the bi- and three-plane
airplanes vanished from the market as well? Just because two wings was
cheaper?

Frans


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PostPosted: Fri Apr 16, 2010 7:00 am    Post subject: 2-blade props Reply with quote

On 04/16/2010 01:41 PM, Gilles Thesee wrote:

Quote:
Apart from what Karl said, the number of blades has something to do with
the prop *solidity* necessary to transfer power. The aircraft you cite
have powerful engines, hence the tendancy to increase the number of blades.

Right. If you increase the amount of power, at some point you have to
increase the diameter of the prop. If you can't do this (for clearance
reasons), you will have to revert to adding some more blades. More
blades is a compromise.

Quote:
Our airplane and two-blade prop were designed just a few years ago, and
they are quite efficient aerdynamically.

I can't think of ANY reason why more blades would be more efficient. I
can however think of reasons why less blades is more efficient.

Frans


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rampil



Joined: 04 May 2007
Posts: 870

PostPosted: Fri Apr 16, 2010 11:36 am    Post subject: Re: 2-blade props Reply with quote

Actually 2 blades being longer radii get less efficient as the length
blade in the transonic or faster regime grows. More blades keeps the tips
out of the transonic regime by keeping the radius down.
Of course we will discuss this in detail at the "Engineering" meeting
this evening for the Europa group at SnF

Cheers,

Ira


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kheindl(at)msn.com
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PostPosted: Fri Apr 16, 2010 4:26 pm    Post subject: 2-blade props Reply with quote

Quote:

Frans wrote :

Quote:

It has a lot to do with sound. A 3-blader produces less sound.
Furthermore it has less vibrations, and to some folks looks sexier.




I am not sure about the sound difference. My 2-blader makes a very attractive low-frequency sound. To me it appears quieter than the Warp Drive. You have the same prop, so maybe you can sometime compare it to another Europa


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raimo.toivio(at)rwm.fi
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PostPosted: Sat Apr 17, 2010 10:45 am    Post subject: 2-blade props Reply with quote

Frans,

you are absolutely right:

More
Quote:
blades is a compromise.

Just one is best = most efficient.

They (Germans) have done that, with a counterbalance of course.
More blades compromise an efficiensy because of ground clearance, noise, tip speed, how it look and so,.

Raimo OH-XRT

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rparigoris



Joined: 24 Nov 2009
Posts: 805

PostPosted: Sat Apr 17, 2010 11:54 am    Post subject: 2-blade props Reply with quote

Hi Raimo"More blades is a compromise. Just one is best = most efficient. They (Germans) have done that, with a counterbalance of course."I made a 1 bladed prop for a hot Cox 020 model motor. Worked for hours and hours trying to get it to be reasonably balanced with a die grinder spinning it up. Not too much joy when approaching the 20K plus RPMs the engine is capaible of. Less RPMs not too bad, but I think the differential thrust caused harmonics that I was unableto get rid of.Ron Parigoris [quote][b]

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PostPosted: Sun Apr 18, 2010 3:40 am    Post subject: 2-blade props Reply with quote

From: Raimo Toivio <raimo.toivio(at)rwm.fi>
To: europa-list(at)matronics.com
Sent: Saturday, 17 April, 2010 19:28:44
Subject: Re: Re: 2-blade props

--> Europa-List message posted by: "Raimo Toivio" <raimo.toivio(at)rwm.fi (raimo.toivio(at)rwm.fi)>

Frans,

you are absolutely right:
More blades is a compromise.
Just one is best = most efficient.

Raimo OH-XRT

Not true Raimo, it is impossible to balance out the assymetric thrust. Vibration will be awful, so no laminar flow.
Graham

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Fergus Kyle



Joined: 03 Jun 2007
Posts: 291
Location: Burlington ON Canada

PostPosted: Sun Apr 18, 2010 9:10 am    Post subject: 2-blade props Reply with quote

I think the number of blades in our types of machines is mainly ethereal because the power range is so small.
The Spit began with 700horse had two wood blades, the -5 had 3, the -6 had 4 and eventually a copy came out with 10 (two contra-rotating 5’s) – al to accommodate larger more powerful engines. I think later models had 3 times the prototype’s poop.
That’s why I opted for 3 – I liked the look.
Ferg
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PostPosted: Mon Apr 19, 2010 6:24 am    Post subject: 2-blade props Reply with quote

Not true Raimo, it is impossible to balance out the assymetric thrust. Vibration will be awful, so no laminar flow.
Graham

Well Graham - Germans have done many "impossible" things during centuries...
I have seen a film about this construction (but maybe it was shit who knows!).
Please remember, they built also the first ever diesel aircraft (Junkers Jumo?) during -30s.
That should have been also "impossible"...

Raimo





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PostPosted: Mon Apr 19, 2010 2:27 pm    Post subject: 2-blade props Reply with quote

Think about the one blade for a moment. It produces thrust one side of the airplane only, left, top, right then bottom. And that doesn't include the asymmetric effect of angle of attack.The airframe will oscillate in a corkscrew fashion, what a horrible prospect I can almost feel my teeth rattling at the thought of it!
2 stroke diesel? Now that is a good idea, most efficient form of piston engine.
Graham
From: Raimo Toivio <raimo.toivio(at)rwm.fi>
To: europa-list(at)matronics.com
Sent: Monday, 19 April, 2010 15:23:55
Subject: Re: Re: 2-blade props

 DIV { MARGIN:0px;}
Not true Raimo, it is impossible to balance out the assymetric thrust. Vibration will be awful, so no laminar flow.
Graham

Well Graham - Germans have done many "impossible" things during centuries...
I have seen a film about this construction (but maybe it was shit who knows!).
Please remember, they built also the first ever diesel aircraft (Junkers Jumo?) during -30s.
That should have been also "impossible"...

Raimo

 



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peterz(at)zutrasoft.com
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PostPosted: Mon Apr 19, 2010 3:35 pm    Post subject: 2-blade props Reply with quote

"2 stroke diesel? Now that is a good idea, most efficient form of piston engine."

reborn as the Gemini - Oh how I hope it makes a comeback from the 'new engine development' graveyard.


Cheers,
Pete
A239


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PostPosted: Mon Apr 19, 2010 4:21 pm    Post subject: 2-blade props Reply with quote

 
Just to throw another spanner in the works: what about steam engines ? The Besseler brothers were flying around in one in California in the 30's. It performed very well, engine is almost silent, and performance does not degrade with altitude. The steam kettle would be part of the fuselage. 
 
Karl


 
Date: Mon, 19 Apr 2010 22:23:34 +0000
From: grahamsingleton(at)btinternet.com
Subject: Re: Europa-List: Re: 2-blade props
To: europa-list(at)matronics.com

.ExternalClass DIV {;} Think about the one blade for a moment. It produces thrust one side of the airplane only, left, top, right then bottom. And that doesn't include the asymmetric effect of angle of attack.The airframe will oscillate in a corkscrew fashion, what a horrible prospect I can almost feel my teeth rattling at the thought of it!
2 stroke diesel? Now that is a good idea, most efficient form of piston engine.
Graham


From: Raimo Toivio <raimo.toivio(at)rwm.fi>
To: europa-list(at)matronics.com
Sent: Monday, 19 April, 2010 15:23:55
Subject: Re: Europa-List: Re: 2-blade props

 .ExternalClass DIV {;}
Not true Raimo, it is impossible to balance out the assymetric thrust. Vibration will be awful, so no laminar flow.
Graham
 
Well Graham - Germans have done many "impossible" things during centuries...
I have seen a film about this construction (but maybe it was shit who knows!).
Please remember, they built also the first ever diesel aircraft (Junkers Jumo?) during -30s.
That should have been also "impossible"...
 
Raimo
 
 
 

 
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PostPosted: Mon Apr 19, 2010 4:34 pm    Post subject: 2-blade props Reply with quote

Paul Lipps had this to say about single blade props:
Quote:

Single-Blade Myth
One of the myths that has been propagated in the aviation community, to the point that it’s almost become gospel, is that the most efficient prop is a single-blade and that all props with higher numbers of blades fall further and further short of this paragon. Did you ever consider that a single-blade prop, developing thrust on only one side of the plane as it revolves, would cause the engine to cone violently in its mounts as it is twisted by the prop?
Airbus Military’s latest turboprop transport, the A400M, has eight-blade props! The Boeing MD-900 helicopter has a five-blade rotor. A popular regional turboprop airliner has a five-blade prop. Hasn’t anybody filled these aircraft manufacturers in on the errors of their ways? In a past issue of a popular aviation magazine, the author of an article on props uttered the same fallacy. He maintained that multiple blades interfere with each other.
When I pointed out to him that at 200 mph and 2800 rpm the blades on my three-blade prop follow three distinct helical paths through the air, and each blade is 25 inches ahead of the previous blade at the same point of rotation, he rather lamely explained that in static conditions interference occurs. Static? Who uses static thrust? Airplanes are meant to fly, not pull tree stumps!

http://www.eaa.org/experimenter/articles/2009-02_elippse.asp
Fred

On Apr 19, 2010, at 3:23 PM, GRAHAM SINGLETON wrote:
Quote:
Think about the one blade for a moment. It produces thrust one side of the airplane only, left, top, right then bottom. And that doesn't include the asymmetric effect of angle of attack.The airframe will oscillate in a corkscrew fashion, what a horrible prospect I can almost feel my teeth rattling at the thought of it!

From: Raimo Toivio <raimo.toivio(at)rwm.fi (raimo.toivio(at)rwm.fi)>

Well Graham - Germans have done many "impossible" things during centuries...





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PostPosted: Mon Apr 19, 2010 5:09 pm    Post subject: 2-blade props Reply with quote

Good one Graham!
JR 327
do not archive
[quote] ---


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PostPosted: Tue Apr 20, 2010 7:07 am    Post subject: 2-blade props Reply with quote

OK Graham,

I got it and lift my hands. I feel I am a poor victim of "One Blade Awesome Myth Aspect (OBAMA)".

Raimo


From: GRAHAM SINGLETON (grahamsingleton(at)btinternet.com)
Sent: Tuesday, April 20, 2010 1:23 AM
To: europa-list(at)matronics.com (europa-list(at)matronics.com)
Subject: Re: Re: 2-blade props


Think about the one blade for a moment. It produces thrust one side of the airplane only, left, top, right then bottom. And that doesn't include the asymmetric effect of angle of attack.The airframe will oscillate in a corkscrew fashion, what a horrible prospect I can almost feel my teeth rattling at the thought of it!
2 stroke diesel? Now that is a good idea, most efficient form of piston engine.
Graham


From: Raimo Toivio <raimo.toivio(at)rwm.fi>
To: europa-list(at)matronics.com
Sent: Monday, 19 April, 2010 15:23:55
Subject: Re: Re: 2-blade props

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Not true Raimo, it is impossible to balance out the assymetric thrust. Vibration will be awful, so no laminar flow.
Graham

Well Graham - Germans have done many "impossible" things during centuries...
I have seen a film about this construction (but maybe it was shit who knows!).
Please remember, they built also the first ever diesel aircraft (Junkers Jumo?) during -30s.
That should have been also "impossible"...

Raimo





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