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Engine configuration



 
 
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  #31  
Old December 16th 07, 03:00 AM posted to rec.aviation.homebuilt
Steve Hix
external usenet poster
 
Posts: 340
Default Engine configuration

In article ,
Richard Riley wrote:

On Fri, 14 Dec 2007 22:32:42 -0800, Steve Hix
wrote:


I spoke about an Indian motorcycle (in reply to the comment "that
ought to bring out the Harley guys"). Guess those bikes were before
most of the times for many in this group )

Big John


Until a year or two ago, they were making them new down the road in
Gilroy, CA.

Too bad they couldn't make a go of it.


They are reincarnating again

http://www.indianmotorcycle.com/Port...dian%20Motorcy
cle%20Revised%20Press%20Release%20-%20Revised%20Sept.pdf

Factory in North Carolina, major stockholder is Stellican Limited,
which brought back ChrisCraft.


I wish them luck this go 'round.
  #32  
Old December 19th 07, 02:36 AM posted to rec.aviation.homebuilt
Charlie[_2_]
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Posts: 56
Default Engine configuration

Ron Wanttaja wrote:
On Thu, 13 Dec 2007 21:53:23 +1000, Michael Henry
wrote:

The Wikipedia article on "V Engine" is quite short but it includes this:

"Certain types of V engine have been built as inverted engines,
most commonly for aircraft. Advantages include better visibility
in a single-engined airplane, and lower centre of gravity."

OK, these are two pretty good advantages! There are no disadvantages
listed. So why isn't the Lycoming O-540 or the Continental O-520 an
inverted V?


The practical difference in visibility between an inverted-V and a horizontally
opposed engine is minor, especially when the airplane they're used on has
tricycle gear vs. a taildragger. An inverted-V engine has a significant
visibility advantage over a radial, but they're no longer common in light
aircraft.

Same holds true for the lower CG: The inverted-V is much better than a radial,
but not that much better than the horizontally opposed engine. If you're
speaking of an air-cooled engine, much of the mass is in the crankcase, anyway,
irrespective of which way the cylinders poke.

And as you say: There are no disadvantages *listed* in a short Wikipedia
article. That does not mean there are no disadvantages. Access to the carb and
other elements that mount below the crankcase is probably more awkward; the
spark plugs may be more susceptible to oil fouling. For that matter, the
inverted-V may have the same problems with hydro lock as a radial...probably in
itself enough of a reason to favor horizontally opposed.

Ron Wanttaja

Is this thread dead yet?

Actually, there is a real structural advantage to the flat engine over
the V. The block can be lighter in the opposed configuration, for the
same strength.

Charlie
  #33  
Old December 19th 07, 05:08 PM posted to rec.aviation.homebuilt
[email protected]
external usenet poster
 
Posts: 1,130
Default Engine configuration

On Dec 18, 7:36 pm, Charlie wrote:
Ron Wanttaja wrote:
On Thu, 13 Dec 2007 21:53:23 +1000, Michael Henry
wrote:


The Wikipedia article on "V Engine" is quite short but it includes this:


"Certain types of V engine have been built as inverted engines,
most commonly for aircraft. Advantages include better visibility
in a single-engined airplane, and lower centre of gravity."


OK, these are two pretty good advantages! There are no disadvantages
listed. So why isn't the Lycoming O-540 or the Continental O-520 an
inverted V?


The practical difference in visibility between an inverted-V and a horizontally
opposed engine is minor, especially when the airplane they're used on has
tricycle gear vs. a taildragger. An inverted-V engine has a significant
visibility advantage over a radial, but they're no longer common in light
aircraft.


Same holds true for the lower CG: The inverted-V is much better than a radial,
but not that much better than the horizontally opposed engine. If you're
speaking of an air-cooled engine, much of the mass is in the crankcase, anyway,
irrespective of which way the cylinders poke.


And as you say: There are no disadvantages *listed* in a short Wikipedia
article. That does not mean there are no disadvantages. Access to the carb and
other elements that mount below the crankcase is probably more awkward; the
spark plugs may be more susceptible to oil fouling. For that matter, the
inverted-V may have the same problems with hydro lock as a radial...probably in
itself enough of a reason to favor horizontally opposed.


Ron Wanttaja


Is this thread dead yet?

Actually, there is a real structural advantage to the flat engine over
the V. The block can be lighter in the opposed configuration, for the
same strength.

Charlie


Opposed engines have less drag than a radial or vee. Opposed
engines are easier to see over.

Buy they sure look funny in a warbird replica.

Dan
  #34  
Old December 20th 07, 02:50 AM posted to rec.aviation.homebuilt
Ron Webb
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Posts: 39
Default Engine configuration



"Certain types of V engine have been built as inverted engines,
most commonly for aircraft. Advantages include better visibility
in a single-engined airplane, and lower centre of gravity."


An aluminum V8 was adapted in the 1960s to power ---I want to say the
Whittman Tailwind, but I could be wrong --- it was run direct drive and
inverted. Ran fine for many years. One problem was that the oiling system
had to be redesigned. It was originally designed to pump oil up into the
valve covers, then let it drain back down. Obviously that won't work if the
whole engine is upside down. Also the carb had to be replaced (float bowls
don't work upside down either.) Neither change is trivial, both are do-able.

You can see why it would result in a lower center of gravity - the crank
(directly connected to the prop) becomes the highest point on the engine
instead of the lowest. Same for visibility - the whole engine is lower and
out of the way.

But that all assumes you are going to use it direct drive - which almost
nobody does. If you use a gearbox, belt PSRU, or HiVo chain PSRU, they will
all give you an offset of several inches, making for the same center of
gravity without the other changes, and allowing for much greater power,
because engine RPM's can be run much higher for the same prop RPM.


  #35  
Old December 20th 07, 04:11 AM posted to rec.aviation.homebuilt
Bill Daniels
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Posts: 687
Default Engine configuration


"Charlie" wrote in message
. ..
Actually, there is a real structural advantage to the flat engine over the
V. The block can be lighter in the opposed configuration, for the same
strength.

Charlie


That's both true and, now that you point it out, relatively obvious. The
through-bolts take most of the loads so the case itself can be quite thin
and light. Something not possible with other configurations.

I wonder why I didn't think of it. Thanks for pointing it out.

Bill Daniels


  #36  
Old December 20th 07, 04:50 AM posted to rec.aviation.homebuilt
Peter Dohm
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Posts: 1,754
Default Engine configuration


"Ron Webb" wrote in message
...


"Certain types of V engine have been built as inverted engines,
most commonly for aircraft. Advantages include better visibility
in a single-engined airplane, and lower centre of gravity."


An aluminum V8 was adapted in the 1960s to power ---I want to say the
Whittman Tailwind, but I could be wrong --- it was run direct drive and
inverted. Ran fine for many years. One problem was that the oiling system
had to be redesigned. It was originally designed to pump oil up into the
valve covers, then let it drain back down. Obviously that won't work if
the whole engine is upside down. Also the carb had to be replaced (float
bowls don't work upside down either.) Neither change is trivial, both are
do-able.

Steve Wittman's plans for the conversion are still available, or were a year
or so ago, from Aircraft Spruce. Several of the V6 engines which have been
produced much more recently have similar torque and displacement--so they
may also be possiblilities in the 200 to 260 CID range.

You can see why it would result in a lower center of gravity - the crank
(directly connected to the prop) becomes the highest point on the engine
instead of the lowest. Same for visibility - the whole engine is lower and
out of the way.

But that all assumes you are going to use it direct drive - which almost
nobody does. If you use a gearbox, belt PSRU, or HiVo chain PSRU, they
will all give you an offset of several inches, making for the same center
of gravity without the other changes, and allowing for much greater power,
because engine RPM's can be run much higher for the same prop RPM.

I agree in principle. It's really the builder's choice of compromises--just
as it is for the designers of certified engines and certified airframes.




  #37  
Old December 20th 07, 05:03 AM posted to rec.aviation.homebuilt
cavelamb himself[_4_]
external usenet poster
 
Posts: 474
Default Engine configuration

Ron Webb wrote:
"Certain types of V engine have been built as inverted engines,
most commonly for aircraft. Advantages include better visibility
in a single-engined airplane, and lower centre of gravity."



An aluminum V8 was adapted in the 1960s to power ---I want to say the
Whittman Tailwind, but I could be wrong --- it was run direct drive and
inverted. Ran fine for many years. One problem was that the oiling system
had to be redesigned. It was originally designed to pump oil up into the
valve covers, then let it drain back down. Obviously that won't work if the
whole engine is upside down. Also the carb had to be replaced (float bowls
don't work upside down either.) Neither change is trivial, both are do-able.



As I recall, Wittman said big problem was that the engine ate plugs in
the inverted position. Barely get 20 hours on a set...



You can see why it would result in a lower center of gravity - the crank
(directly connected to the prop) becomes the highest point on the engine
instead of the lowest. Same for visibility - the whole engine is lower and
out of the way.

But that all assumes you are going to use it direct drive - which almost
nobody does. If you use a gearbox, belt PSRU, or HiVo chain PSRU, they will
all give you an offset of several inches, making for the same center of
gravity without the other changes, and allowing for much greater power,
because engine RPM's can be run much higher for the same prop RPM.



And what does all that do to 1) weight and 2) CG ???
  #39  
Old December 20th 07, 05:52 PM posted to rec.aviation.homebuilt
John Halpenny
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Posts: 22
Default Engine configuration

On Dec 20, 12:03 am, cavelamb himself wrote:
snip
But that all assumes you are going to use it direct drive - which almost
nobody does. If you use a gearbox, belt PSRU, or HiVo chain PSRU, they will
all give you an offset of several inches, making for the same center of
gravity without the other changes, and allowing for much greater power,
because engine RPM's can be run much higher for the same prop RPM.


And what does all that do to 1) weight and 2) CG ???


1) A PSRU gives a smaller faster engine, which is usually lighter even
with the weight of the reduction gear.
2) Raising the output shaft several inches is the same as lowering the
CG, and the bulk of the engine that spoils your view, the same amount.

John halpenny

  #40  
Old December 20th 07, 07:08 PM posted to rec.aviation.homebuilt
cavelamb himself[_4_]
external usenet poster
 
Posts: 474
Default Engine configuration

John Halpenny wrote:
On Dec 20, 12:03 am, cavelamb himself wrote:
snip

But that all assumes you are going to use it direct drive - which almost
nobody does. If you use a gearbox, belt PSRU, or HiVo chain PSRU, they will
all give you an offset of several inches, making for the same center of
gravity without the other changes, and allowing for much greater power,
because engine RPM's can be run much higher for the same prop RPM.


And what does all that do to 1) weight and 2) CG ???



1) A PSRU gives a smaller faster engine, which is usually lighter even
with the weight of the reduction gear.
2) Raising the output shaft several inches is the same as lowering the
CG, and the bulk of the engine that spoils your view, the same amount.

John halpenny



Not necessarily.

Starting with a V8 (or any other given engine) doesnt make the engine
smaller...


This only works for an engine "designer"...
 




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