![]() |
If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below. |
|
|
Thread Tools | Display Modes |
#7
|
|||
|
|||
![]() "cavelamb himself" wrote in message hlink.net... Wayne Paul wrote: Bob, Your HP-18 side-stick to center-stick is an example of good design. http://www.hpaircraft.com/center_sti...22_january.htm (Complete story http://www.hpaircraft.com/center_stick/) Other designs that may be of interest to the group are Udo Rumpf's use of a PIK-20 sailplane stick http://www.soaridaho.com/Schreder/Co...ter_Stick.html and Brian Case's HP-16 modification. Brian need to lower the seatpan in his HP16 to allow more head/canopy clearance. So he removed the old cable system which ran under the seat and designed the following modification: http://www.soaridaho.com/Schreder/Co..._Stick_Mod.htm (Brian by his HP-16T http://www.soaridaho.com/Schreder/HP...Mackay_IDa.JPG) Wayne HP-14 "6F" http://www.soaridaho.com/Schreder The second picture from the top tells the tale. I'd assume (?) that there is something like a U joint behind the cockpit to let the push rod line up with the elevator horn? I'll have to think about this some more. You guys just could be right! Richard, Here are some pictures from behind the cockpit that may help understanding Brian's control system.. http://www.soaridaho.com/Schreder/Co...ick_Mod_11.jpg The above picture was take looking forward. It shows the bulkhead aft of the wheelwell. You can see the series of bell cranks that actuate the ailerons and the push the stick's push rod as it is routed through the right side of the bulkhead. The elevator push rod and direction reversal crank can be seen on the left side of the bulkhead. (More pictures http://www.soaridaho.com/Schreder/Co...tick_Mod_9.jpg http://www.soaridaho.com/Schreder/Co...ick_Mod_10.jpg) As you can see, there are no "U-joints". The linkage has almost no "slop" and give good control surface feed-back. It should also be noted that the ailerons droop and reflex with the flaps avoiding misalignment during normal cruise and thermaling flap configurations. Wayne HP-14 "6F http://www.soaridaho.com/Schreder Richard |
Thread Tools | |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
doodles damit... | Richard Lamb | Home Built | 8 | March 5th 06 08:17 AM |
Doodles... | Richard Lamb | Home Built | 39 | January 20th 06 08:34 PM |