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Author Topic: A weighty situation  (Read 11968 times)

Offline Jason Greer

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Re: A weighty situation
« Reply #100 on: May 05, 2018, 10:41:27 PM »
This post is in reply to several comments regarding the actual weights of a full size/competitive electric model.  I thought I’d add a few real world examples of my last few completed electric model weights. These models were built per the plans with no extreme measures to save weight.  For example, the engine bearers were left out of the fuselage construction, but no other structural changes were made. All of the wood used to construct these models was purchased from Tom Morris. These weights include the battery and are ready to fly.

Geo-XL built in 2011: 53 ounces (5 cell battery)
Impact built in 2013: 53 -54 ounces (5 cell battery)
Impact built in 2016: 57 ounces (6 cell battery)

All of these models were finished with monokote except for the 2016 model. It has a silkspan/doped fuselage and monokote covered flying surfaces.

I shared the component weights of a typical 6 cell 60 size electric power system in an earlier post. These are actual numbers weighed on a trustworthy scale. 

Please note that I don’t personally have any issue with how we are currently weighing/pull testing electric models. The purpose of this post is to simply inform the guys who have no experience with electric power systems of the true weights of a typical ready to fly electric model.

Jason
« Last Edit: May 06, 2018, 12:22:51 AM by Jason Greer »
El Dorado, AR
AMA 518858

Offline Randy Cuberly

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Re: A weighty situation
« Reply #101 on: May 05, 2018, 11:13:04 PM »
This post in reply to several comments regarding the actual weights of a full size/competitive electric model.  I thought I’d add a few real world examples of my last few completed electric model weights. These models were built per the plans with no extreme measures to save weight.  For example, the engine bearers were left out of the fuselage construction, but no other structural changes were made. All of the wood used to construct these models was purchased from Tom Morris. These weights include the battery and are ready to fly.

Geo-XL built in 2011: 53 ounces (5 cell battery)
Impact built in 2013: 53 -54 ounces (5 cell battery)
Impact built in 2016: 57 ounces (6 cell battery)

All of these models were finished with monokote except for the 2016 model. It has a silkspan/doped fuselage and monokote covered flying surfaces.

I shared the component weights of a typical 6 cell 60 size electric power system in an earlier post. These are actual numbers weighed on a trustworthy scale. 

Please note that I don’t personally have any issue with how we are currently weighing/pull testing electric models. The purpose of this post is to simply inform the guys who have no experience with electric power systems of the true weights of a typical ready to fly electric model.

Jason

Hi Jason,
Thanks for the post!  It confirms what I basically have believed to be fact.

My Geo XL built in 2006 weighed 54 ounces with no fuel in the 4.5 ounce tank (no nitro fuel) and the wood was very carefully selected to be as light as possible.  It used a Belko long shaft .56 which is a fairly light engine at 11.5 ounces with the rear exhaust muffler.  It was finished in the traditional silkspan Dope finish on the entire airframe with considerable fiberglass reinforcement on the fuselage and internal areas of the engine compartment.
Had it used a typical tuned pipe arrangement on a PA65 it would have weighed significantly more.  Probably as much as 6-7 ounces more plus the weight of the fuel!

It was a terrific flying airplane at that weight and perfectly matched to the power!  I still miss it!  It was unfortunately stolen from the flying field!

Randy Cuberly
Randy Cuberly
Tucson, AZ

Offline Dave Hull

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Re: A weighty situation
« Reply #102 on: May 06, 2018, 01:19:49 AM »

Offline Jim Svitko
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Re: A weighty situation

« Reply #105 on: May 03, 2018, 01:11:20 PM »


Quote

 

"I have also been curious about measuring the line pull in the air.  With the proper equipment (instrumentation?) I suppose it could be done if someone wanted to go thru the steps.  But, is it worth the time spent?   Maybe, for some, but for me, it is easier to do the math.  I know the weight (mass) of the plane, the radius of the circle, and with a standard lap time (5 seconds, give or take a few tenths?), I plug the numbers into the formula."

Yes, there was at least one in-situ measurement of line tension. The results were published back in probably the early 1960's. As I recall, it was done by the racing guys. They probably used load cells at the handle, or less likely, strain gages on the lines. (I remember looking at the photos and trying to decide what type of transducer was being used. I couldn't tell, other than there were electrical lead wires to some electronics strapped the pilot's belt.) They plotted the loads and compared them to the straight "centrifugal force" calculation. Their conclusion was that the actual loads were higher than the simple mass/centrifugal force calculation. I would have to find the article to see if they characterized the uncertainty of the test results. The biggest question I would have is whether they grabbed random instantaneous values or were able to collect max/max value.

A few other cautions:  pilots often whip at times, which increases the line load temporarily beyond the simple centrifugal force calculation. Also, I suspect that trim can cause a significant offset in the straight and level line tension. Lots of line rake, rudder offset, engine offset, etc. These cause aerodynamic loads that are not accounted for in the simple centrifugal force calculations. Bob mentioned in one of his posts that he could show us how to reduce the excessive line tension--I liked his oil painter metaphor. I used a different one when I tried to describe motor skills and strength to guys at work: try holding a suitcase in one hand and then try to take the cap off a tube of Chapstick and apply to lips. The extra weight demolishes your fine control. Go ahead, no one is looking, try it!

Also note that increased line tension in the wind--which everyone can relate to--occurs from two sources: so-called wind-up where the plane speeds up, and also from the "crosswind drag" on the plane. Planes are not very streamlined along the lateral axis, and you can feel it. So the first one is mass related and the second is aero related.

The team race (F2C) guys experimented years ago with engine in-thrust and banana fuselages to try to reduce the in-flight drag. Not sure how much that achieved--but it made the planes a real #$@%?! to take off. Not sure anyone is still building/trimming that way. However, I know that racers trim for least out-thrust of any of the events that I have participated in. Zero everything and then push the leadouts forward until you have trouble on takeoff. Not sure how the old B-TRs in the study were trimmed, but I would start by assuming a stunter would have more aerodynamically generated line tension.

One of the other posts implied that a centrifugal force calculation wasn't valid during maneuvers. I disagree: the component of force that is solely due to the accelerating mass is always valid--if you put in the correct velocity and other inputs. However, as I tried to list above, it is only one of the vector components.

Dave

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