mike mcs repair
Registered User
chugiak AK
I think you can copy anything you want for own use.
Glenn
nope, and they can come take the tools you made it with too..
I think you can copy anything you want for own use.
Glenn
Your experimental and a clever guy. I would think it would not be that difficult to copy the geometry and get some CNC shop to make all the hangers, then build the flap sections?
Glenn
nope, and they can come take the tools you made it with too..
That is funny because Doug was measuring Paul's Otter flaps years ago.
With only a quick look at that seat I would be scared to to a 4G maneuver with that seat not to mention any hard landing.
Perhaps not: US application [FONT="]US20120280089[/FONT] (inventor Doug Keller) is abandoned for failure to respond to the PTO in 2015. Does anyone know of another application or patent that applies here?patented
Things I've observed about Performance STOL flaps. The STC'd ones on John Schwamm's Cub have better clearances/tolerances than my experimental version. To be fair my Backcountry's flaps use Backcountry's hangers and I can't say whether the flap bodies or the hangers are what's different. I have watched guys at Airframes working on the STC'd flaps and they were incredibly meticulous with details, but that's how Airframes rolls. John's flaps are painted and operate smoothly with consistent clearance throughout defection. Mine are painted and will require thin teflon tape to prevent the upper flap from scraping paint off the lower flap surfaces. That's common with the exp versions that I've seen on other planes, too.
Wait a few months before you try to re-invent split flaps on that Rans. Backcountry is about to fly a new flap design that may take flap performance up a notch, and by appearances it looks simpler than the split flaps.
Perhaps not: US application US20120280089 (inventor Doug Keller) is abandoned for failure to respond to the PTO in 2015.
Public PAIR: https://www.uspto.gov/patents-appli...s/check-filing-status-your-patent-applicationwhere do you find that?
Public PAIR: https://www.uspto.gov/patents-appli...s/check-filing-status-your-patent-application
Enter 20120280089 as the publication number.
Did the adverse affect of the large wing tip flat plates cause the plane to weather vane into the wind or did it cause increased drift in the direction of the wind? Thanks for your time.
Excellent review, Thank you.Here is a YouTube Pilot report on my newly installed PSTOL flaps. I like them a lot! Still learning how to use them effectivly - going to take some practice. The video is literally the first time I flew with them.
Which will further increase the pulling forces on the handle.I think I will however go to the Dakota spring in the future
Here is the full video to accompany the above picture. The PA18 A ratchet gives you approximately 16, 32 and 46 degrees of Performance STOL flaps in the PA18, pulling that last notch is quite easy below the max full flap speed of 70 .... at least that's what I figure by speculating not by actually changing to a ratchet that may be grey area for approval. I doubt that the difference between 50 and 46 degrees would be evident to all but the most experianced STOL pilot.