
Posted on July 14th, 2008 at 10:29am —
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Posted on June 16th, 2008 at 10:00am —
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Along with a couple of Tri-Turbofan toy blimps, one of the purchases for my early blimp experiments was a Plantraco MicroBlimp, which is the company's current offering. After ordering, I found out that it was too small to carry any useful paylo… Continue
I attached some additional sensors today - a pair of Maxbotics EZ0 ultrasonic ranging modules and a Honeywell HMC6532 I2C compass. Also, I added an extender to the camera module to point downward about 30-degrees and I finally adjusted the focus. I think the camera angle is pretty g… Continue
Posted on March 16th, 2008 at 5:01pm —
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Here's a video clip from YARB 1.0's first untethered flight. I captured the video while sitting in my office while the blimp explored the hallway and front room (the dogs completely ignored it). The camera is a bit out of focus, and the afternoon light washed out the picture somewha… Continue
Posted on March 13th, 2008 at 4:26pm —
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Chris Anderson
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What CAD Software did you use for your board? I'm using Eagle and it doesn't have the Sayno or the Fairchild and that's really annoying :(
I searched through the ~1,900 presolved powertrains generated by the FlightSolver program. These powertrains are generated by the FlightSolver program according to minimum performance criteria and battery and motor current and voltage limits for use with airplanes.
The APC 12x8P and APC 12 x 6E are not in the database, but I have the APC 12 x 8E (tractor) propeller in the database.
I found a presolved powertrain with a APC 12x8E that reached about 4.7 grams/Watt at zero airspeed (ie in a hover). The thrust in a hover is 17 N and the powertrain mass is 0.37 kg (3.7N), so the powetrain can lift its own weight.
The current drawn by the motor in a hover is about 31 Amp which slightly exceeds the battery pack current limit of 30 Amp. Flight time is thus quite low, about 2 minutes.
The complete powertrain is as follows:
propeller: APC 12 x 8E
motor: AXI 2826/12
battery: FlightPower (UK) EVO20 1500 4S1P
I have the complete report generated by FlightSolver in pdf form. I can't figure out how to attach it to this email, however, I will figure it out and send it along in a separate email.
James
I found the name of the paper on the coaxial propellers, unfortunately, I did not keep a copy of the document itself.
Here are the details:
'An Experimental Investigation of Low Speed Single and Dual Rotating Propellers', Ronald Helmut Lorenz, University of Toronto, MSc Thesis, Department of Aerospace Science and Engineering.
I believe that it can be obtained through the library at the following URL: http://cisti-icist.nrc-cnrc.gc.ca/main_e.html
If you would like me to prepare a report for any specific combinations of propeller, motor, cells, please go to my website www.flightsolver.com and select the link for 'database summary' which is grouped with two other links near the top of the page.
I believe your comment that the second propeller should have a higher pitch is correct. The difficulty is determining how much. Another question arises, ie, is it better to have a space between two coaxial propellers.
James
I think that I have a paper on coaxial propellers, I will try to dig it out today.
I'd be interested to compare results with you. I'll be travelling today so I will see if I can find the paper on coaxial propellers tonight.
James
It looks like you are using a couple of APC propellers. How it your machine performing. I have measured some propeller performance data for APC props for electrics up to 16" I also have some software to match props, gearboxes, motors and battery packs.
James
James
I should have guessed I would find you here.... !8-D