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argoldman

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Posts posted by argoldman

  1.  

    But seriously - if you put too much of that crap in there you'd spend all your time messing with the gadgets.

     

    What these planes really need is a shaft brake and a BRS parachute system.

     

    True, with respect to redundancy, you only need one more of an indispensable item (or system) than the number you had before they all failed.:rolleyes:

  2. My best guess is that folks are using their NG-51's to locate the holes/hardpoints. All of the holes are not there, as numerous other builders have had the same question.

     

    When I searched the archives I found this from you, in reply to another builder:

     

    "My measurements show that the fourth hole (the lower one closer to F-22

    on the pilot's side of the fuselage) is approximately 4" forward of the

    rear surface of F-22 at a distance of 2-5/8" from the upper hole. It's

    NOT directly below the upper hole, but slightly in front of it. If you

    make a 2-5/8" circle around the upper hole and then intersect it with a

    line perpendicular to F-22 at 4" from the rear surface, you've got it."

     

    So that's what I used to approximate the location for that hardpoint. I'll drill the actual hole after the assembly is complete. With some luck it will be within the hardpoint.

     

    I'll look at M-19 - I haven't looked at that one yet - but M-10 and 11 do not show where the middle hole for Jack's mount needs to be.

    Phil, I may be talking totally out of my landing gear here, since it has been a couple of years since I mounted Jack's gear, but I think that using the original holes, for the manual gear, you locate the additional holes using the aluminum bracket that holds the motor assembly. Using this technique, you can locate the holes and do your hardpoints before assembling the box structure. Just make sure that when you do assemble the box that you first bolt, with spacers from one side to the other so that the holes on each side of the box are in proper relation to each other.

     

    I used this same technique, once I drilled my landing gear bulkheads using the wood 90 degree guides, before glassing them in. I made aluminum rods, tapped at each end, the exact length as I wanted the spacing to be, and glassing into the fuselage was a simple matter of taking both bulkheads (connected by these rods), leveling and squaring the whole mechanism and then bonding it in place See attached pictures (If I can get them to work). Makes life and alignment easy.

    post-825-141090173147_thumb.jpg

    post-825-141090173159_thumb.jpg

  3. Rich, you're right. Except the 'dump' door is only open when:

     

    1. I want outside air, w/ blower sitting at end of runway - no heat, canopy clsd,

    2. flow thru ventilation during no-heat conditions,

    3. heater in use in the summer and the hot air is intentionally dumped overboard.

    4. chewing gum or urine disposal....:)

     

     

    jerry

    If you can do #4 from the front seat, you are a better man than I:cool:

  4. the zinc chromated plate is a overboard air dump. I can close it to re-circulate warmed air or dump the air overboard.

     

    Jerry

     

     

    Perhaps I am looking at this the wrong way (which is not unusual for today). It seems, in the pictures that your heat exchanger is mounted to the seat front from which it draws air from the cabin, under one thigh or another. The seat top, itself, with the bulkheads and the fuselage bottom acts as a plenum. Your axial fan creates a negative pressure in the plenum, drawing air through the heater core and a positive pressure in the duct to heat the rest of the plane through the plans type plumbing.

     

    Here's my quandary. :confused: If the axial fan draws air through the core, there will be a negative pressure in the plenum with respect to the outside air, because of the resistance of the air going through the heater core. Opening your chromated plate will only allow outside non-heated air to be pulled into the plenum and be distributed. It will not dump heated air overboard unless the shape of your bottom creates some sort of venturi effect which creates more negative pressure than does the axial fan.

     

    That being said, Your workmanship puts me to shame. It looks beautiful. In the future, would you please send pictures that are slightly out of focus to make me feel better.:rolleyes:

  5. I'm about to start on the permanent firewall pieces and was wondering about the blind screw installs. I've read a lot of different solutions to the turning problem and was wondering how many folks went with Click-Bonds instead?

     

    They seem like a cleaner and easier solution than some of the Rube Goldberg ideas I've read about (no offense). If I decide to go with click bonds would I mount them on the outside or would I mount them through the firewall?

     

    Interesting question.

     

    If I were to use the click-bonds, I would put them on the inside of the firewall, through the firewall. One would hope that the adhesive that you use would counteract the torque of tightening the bolts. Perhaps if you modify the shape of the flange and flox/glass over them.

     

    I chose to use stainless steel thingies, from the ACE or True Value aircraft store that are designed to go through wood and provide a metal threaded recepticle. They have a flange with a female thread (kind of like a "T") and the flange has 3 tines which are driven into the firewall (from the inside).

     

    These have no locking ability so that I will have to use Locktite (and safety wire).

     

    One of the reasons that I chose to do this (mounted from the inside) is that your SS firewall material (or what ever metal you decide to use) will be primarily held to the firewall, sandwiching the Fiberfax, by the through the firewall bolts of the engine mount, the pulleys, and all of the other things that you bolt onto the firewall.

  6. Thanks Rick! I got the bolts and put the wheel, inner tube and tire together with a few pounds of pressure in it. Seems to be OK - good enough for me to continue working on the nose section, anyway! :cool:

    Phil, I may be talking out of my innertube here, but I seem to remember that there were two types of nosewheels available. One from Ken brock, that I think was in more than two parts (I have never seen one) and the Gerdies wheel that was available from ACS. Why don't you send a picture to us so that we can identify it.

     

    The bolts on a wheel are somewhat important as you will be blowing about 70# of pressure into that little bladder.

     

    I think that in the railroad business they use much less pressure than that to lift railroad cars back onto the track.

     

    You don't want a failure here as it will probably happen on landing.

     

    The bolts are probably AN3 or 4s but make sure. If it is the Gerdies, the Cozy Girlllllllllllls have a lot of experience as they take the sow's ear that was provided by the Gerdies factory and with a little machining, create a silk purse.

  7. Sanding is sanding. Either "waste time" sanding filler or waste time sanding high-build primer.

     

    Sanding the filled surface from 40G to 320G also requires less high-build primer and results in a lighter airplane.

     

    What's the logic in purposely leaving deep scratches in a surface so you have to use high-build primer to fill them?

    It boils down to time spent sanding:mad: . Shaping and sanding with 40G is very rapid and takes relatively little effort. After the 40 is done, a coat of aeropoxy light, using the high points of the prior sanding merely the areas on each side of the "scratch left by the 40 grit, just filling in the scratches requires very little post application sanding with 8o then finer.

     

    Don't know how much added weight that adds, --probably none-- since if you build up, sand down then sand finer and finer, you end up with the same surface, It's just a matter of building it from the inside rather than sanding it away from the outside. For what it's worth, this technique served me well on my dragonfly and the wings of my cozy (still waiting for the final coat and sanding). "you say either and I say Ether":cool:

  8. thats a waste of time to sand the filler more than 60 grit. The epoxy is to fill the pinholes and then use high build primer to fill everything else. actually the epoxy is also a waste of time the new epoxy high build primers are the way to go. fills the 36 grit and you end up with no pinholes. we did a Lancair IV with a carbon fuselage this way and did not have any pinholes

    Agreed, I've been doing 40 grit and then a top and/or fill layer of Aeropoxy light, down to finer.

     

    What high build epoxy primer are you recommending???

  9. Steve Bennett (Great Plains Aviation) has been doing VW Engine conversions for years and knows them backwards and forwards. He's a member of my EAA Chapter (80). I had an occasion some tme back to ask him this same question and his comment was that it was not a suitable powerplant for a Vari or Long.

     

    In reference to the Corvair, he said that the crank was not strong enough and usually broke. I forget what journal they fail at but could get that information for you if you are interested.

    Steve is a great guy and sells great products and ideas, but remember that he is a VW seller and may have a prejudice against competitors. This is not specific to Steve but is rampant in the aircraft (and many other) business. There is probably a Corvair website where the information is more reliable (or possibly slanted the other way.)

     

    I know that there are a few dragonflies that are switching from the VW to Corvair. Perhaps listening in on the D-fly list would give you more info.

  10. I like the idea of Fred

     

    Going VFR but having the IFR capability just in case of an emergency

     

    What would you incorporate in the ideal panel?

     

    Just trying to get as many ideas and opinions.

    Started saving pics from all the EZ panels I can find on the web, there is a wide variety to be seen

     

    Thanks for the help

     

    Ronny

    :D :D :D :D

    REDUNDANCY!!!!!!REDUNDANCY!!!!!!REDUNDANCY!!!!!!REDUNDANCY!!!!!! with no single point failure spot.

     

    Even if you don't plan to do much IFR, if a failure happens there, it is 100% and your survival might depend on either redundant instruments or your ability to use partial information to ascertain that the oily side is down. If you don't do much instrument work, the probability of this is slim. This, of course does not imply that you need 2 of everything.

  11. It appears to me, based on the photo that it would have been for a Corvair.

    What is the N number on the EZ so we can look up on the regristry.

    I have been looking into the possibility of put a Corvair on my EZ.

    Any body out there in Canard Land have any data on a Corvair installation?

    Contact William Wynne, the Corvair/aviation expert. (although not specifically for EZs

  12. Hi all. My name is Mike and I'm a grad student in Indiana. I'm starting the planning process for building my own COZY. I've gotten the official approval from the wife and plan on buying plans soon. I'd love to come see a project if there's anyone building a canard in Indiana. Thanks for all of the future support that I'm sure I'll need!

     

    -Mike

     

    Great, and Wecome

     

    Getting the spousal permission is a great step forward, keeping it will require a little work.

     

    If you have access to a bird, or ever find yourself in the Chicago area, I am building an Aerocanard in Kenosha Wi (just over the IL/Wis Border, at the airport. I would love to show you, or any others my project.

     

    Good luck with your venture-- uh-- Cozy

  13.  

    I mean - 75 cents for a 2.5" grade 8 bolt? Come on.

     

    As said before, the aircraft bolt is not a grade 8. Specific stats can be found in the ASS catalog or just google An-??

     

    The metal in these bolts is tested and certified to specific strength numbers. Grade 8 is a somewhat brittle metal and may vary bolt to bolt. The aircraft bolt will stretch before it separates, not so with the more brittle grade 8. Additionally, the threads are rolled, not cut which adds more strength to the bolt. The length of the thread and grip is also specified. The quality, size and metallurgy is constant and they are Cad plated.

  14. Steve said:

     

     

    Well If you are really a Canard a holic you will build one of your own to be a true canard a holic. There is way more satisfaction to build than to buy. Ps. Longezes have way more leg room than a cozy at least that is my exsperience. Build on STeve

     

    There is room for all canardaholics, be they strictly imbibers or imbibers and distillers.

     

    Yes, you are right, your legs are somewhat stretched out. What you don't understand is that in the EZs, the whole seating configuration is different. It is not standard seating with legs stretched. That would be torture. In the EZs, your back is actually reclining about 45 degrees, your hips are slightly bent and your legs are somewhat stretched out. Sounds horrible!!!!

     

    However, it is a VERY comfortable position, almost like sitting in an recliner chair. a couple of minutes is all it takes to accomodate to it.

     

    In addition to being very comfortable, since you are somewhat reclining, the physiological effects of G-forces are felt much less. You don't notice this at first, but as you do "zoom ups" and steep turns, you have the feeling that something is missing--- that is a reduction in the increased G awareness.

     

    With the EZ seating, and high Gs, instead of your stomach descending to your feet, it stays around your family jewels.

     

    An additional factor in the seating is that in vertical impacts, the force is distributed through your ribs to the seat back, rather than vertically to your spine, decreasing the possibility of making you shorter.

     

    After crashing my dragonfly (similar seating) and surviving spinally, despite prior existing rods in my spine, I chose to build the Aerocanard because of this seating arrangement.

     

    I recline to comment further:bad:

  15. some of us do it with templets and a router, so all the over-spill is cut off

    a fast clean way to do all the bulk heads. no cutting, no sanding,

    you do all your fussing with masinit 1/4".

     

    Clean????

     

    Been there, done that

     

    I'm still pulling the resultant airborne fiber and epoxy dust out of my personal glass.:irked: (I even used a vacuum system directly over the router)

     

    a better way is to layup as you would for routing, however use a sharpie to mark actual size and shape or cut out template and glue on cured glass and cut out with metal cutting band saw.

     

    The band will last for quite a while, however after the first cut, the blade will be unable to cut metal well.

  16. I've been really picking up steam on chapter 4 and only have the front side of the IP, the landing gear bulkheads and firewall to do.

     

    I have a new question. On some of the layups, specifically f-22, 28 and the IP, I had a helluva time keeping excess expoxy from running off and then under the foam. For F-22 and 28 there was only a bit and I easily sanded it off but on the IP I've got a spot that's about 9 sq. in. Do I really need to get that off or can I just rough it properly with 30grit and glass over it?

     

    as usual, thanks for any input.

    Just get out your FEIN with a sanding head (40 grit), knock off the extra epoxy in a heartbeat. and the resulting surface will be great for further bonding.

     

    What you don't have a Fein???????-- Shame on you!!!!!:mad::confused:

  17. Ok that seems to have worked,Not sure what was going on last night, maybe not enough sleep to operate lap top. Thanks for the help,I have just started this project and I am having a lot of fun working on it, Hope it turns out to be a usable airplane. I still have lots to learn and I hope by talking with some experienced builders I will get a good idea of progressing this project. Right now my imediete concern is let a seasoned builder look at it and give me there opinion. No point in building an unsafe airplane. Second I would like to find a set of plans, I have already downloaded the POH and found it very interesting. It seems sourcing parts is going to be a chalenge however not imposible. So far I do not see any reason the I should not be able to build this thing to completion given the skills I already have.

    H4,

     

    Looks like a great project. Welcome to the backward flyers.

     

    Looking at the way that you have your nosewheel retracted (part way), unless you have an electric nose retraction system, I would advise against putting any weight in the cockpit.

     

    The crank type retraction mechanism puts a huge load, in the incomplete retraction or extension mode, on the teeth of a rather weakish gear. This gear is subject to stripping with load. When the nose gear is retracted, the gear has little load on it (in fact negative), when it is extended, there is an over-center mechanism which again takes the load off of that wimpy gear.

     

    DISCLAIMER:::::::::

     

    I am not a veri-EZ bulder/flyer (Aerocanard with electric nose builder) however I am somewhat familiar with the mechanism that the veri and the long use.-- Perhaps I am being overcautious, but reading all of the requests for new gears, or information on how to rotate the existing stripped gear, I felt that I had to write this.

  18. Tyson, agree, I should have listed the caveats in smallprint. Happy for you to go through that data an multiply by the efficiency factors you see for e.g. an MT and a silver bullet for each of the flight profiles. No question. I will be interested to see the resultant deltas between the designs, and compare them to published test data. I believe they will be smaller than you think, and hence I deemed them relatively inconsequential. Given CS prop are essentially a fixed blade design that twists at the hub, they too are set for an optimum flight profile. Is blade design, independant of hub more efficient for a CS prop?

     

    Published tests in the CSA newsletter, might be Jack Fehling's 200hp Velocity from memory, were quite telling when comparing the MT to the silver bullet, and I think they included environmental data.

     

    I too am interested in the data. Having had a total of 9 aircraft (including the one that I am building) one fixed pitch prop and 7 constant speed ones, and having flown most other light singles and twins, of both persuasions, I am partial to the constant speed variety.

     

    If we remove the twins from consideration since they need the C/S for feathering reasons, in store bought craft I have had, and my dragonfly (airmaster C/S with warp blades) the C/S-CP props give a better climb and shorter t/o distance. There is probably a slight cost in high cruise.

     

    Imagine starting your car off from a start in second or third gear.

     

    I hope to be proven wrong so I don't have to consider the choice for my aerocanard.

     

    There is another advantage to a C/S (constant speed) prop or C/P (cockpit controllable pitch) and that is on landing, when you go to full fine on the approach, the prop acts as a speed brake and makes landing a lot easier. Kinda like an additional belly board (on the ground it doesn't make any difference).

     

    There must be a reason why all high performance store bought aircraft come from the factory with expensive, higher maintainence, C/S props with similar downsides to the governors which control them.

     

    For low performance aircraft such as 150/2s or 170/2s or smaller pipers and the like, Fixed props are used for simplicity and cost.

     

    This is not to say that C/S- C/P props are necessary on our craft. If you always fly out of long enough runways and are satisfied with the rate of climb that can be gotten with a f/P prop, that's great.

     

    In store bought Planes that have f/P as standard, there are usually two varieties that are certified. One is the cruise prop, with a certain pitch, the other is a climb prop with a finer pitch. The climb prop being a finer pitch will climb better at the expense of top end. The cruise prop has a better top end, at the expense of climb performance. A C/S -C/P prop allows you to have both of these, cockpit selectable. (I won't go into the mechanism and difference between C/S and C/P here suffice it to say they have similar effects).

     

    There are some props which claim to be "Semi constant speed" These props, I believe are designed to actually flex and change their pitch slightly automatically. I have no idea if they actually are better-- anybody out there have one or two??

     

    Disclaimer::::::::: I don't know if the above holds true for pushers, however I think that it does.

     

    One more thing, for those considering Turbo or other chargers.

     

    A C/S C/P is required to achieve maximum use of your setup.

     

    As the aircraft ascends, the air, as we all know gets thinner. The charger makes the engine think that it is lower than it is and it is able to produce more power at the thin air altitudes.

     

    Not so the prop. Fewer molecules of air are being quesenarted by the prop than at a lower level, and unless you increase the pitch of the prop, it will over-speed as you fly in the rarefied air with more power. To stop your Lyconental parts from flying hither and yon because of this over-speed, you have two choices: 1) reduce throttle setting (in which case you waste the advantage of the turbo) or 2) increase the pitch of the prop-- which you can't do with a F/P

     

    Why don't F/P props typically over-speed with Normally aspirated engines at altitude????? The engine is producing less power and because of this the decreased density of the air isn't usually a factor.

  19. If you trim the next day when the glass seems to be to hard you can use a heat gun and it will soften it enough to knife trim.

    After what seems like miles and miles of knife trimming at just the right time, waking up at 3:00 in the AM so that I can get the trim exactly at the right time, the Fein tool was a godsend (or whatever "send" prefix you prefer to use).

     

    When caught at the right time, knife trimming is, as Garrisson Keillor says, "Tasty and Expeditious", however getting it at the right time can be difficult as it depends on the thickness of the layup many times.

     

    Although heating and trimming works, it is a great deal more work than simple knife trimming. I have no idea of what the reheat, cutting (and pulling the fibers) has on the final layup--probably none.

     

    Best to get the sleep and use your Fein. One blade, possibly 2 will last for the entire build and make your life so much easier. Easier and in a time frame that fits your schedule is more bettttter.

  20. That was Neiman-Marcus' price, and included training for two. Pretty pricey training! LOL! I guess N-M needs to make a hefty profit! Can't imagine many takers...

    NM has one of these things in every X-mas catalog. The question is do they sell any at all or is it just a gimmick to get people looking.

     

    One year it was a his-n-her set of mini submarines.

     

    Of course there are those to whom a mere 1/4 mil is insignificant and a gift like this is a novelty (not exactly your x-box).

     

    The question that I have is does this gift come in a NM gift box?

  21. I typically use large ziploc bags filled with sand for wieght when I need it. Easy to adjust the weight etc.

     

    When I did this bulkhead, I used a vacuum bag process and let the atmosphere provide the required pressure to the part.

    If you get some sink cutouts (formica type)from kitchen counters (ie from Hme depot-- very cheap), lay it on top of your structure, you can use whatever type of weights that you want to, including buckets of water.

     

    I have found these mini-countertops to be of invaluable help in many of the construction tasks. If you contaminate them with epoxy and don't want to clean them up, discard them.

  22. I have to take a pause in my building to move. I have removed the resin and hardener from the pump reservoirs, and I was wondering what to use to pump through the pump to cleanse it? Do I have to take the pump apart to clean it properly? I did notice as I pumped the last of the fluids out that the handle is slow to return to top position and worry that the metering is affected. It is a Michaels Engineering pump with MGS 335.

     

    Thanks.

     

    Check with others, but I think that I used denatured alcohol. (it's been a while). While you are at it, replace the reservoirs with new ones. So much easier to do when empty and non-sticky.

     

    If you call yourself the canardologist, can I be the proptologist??

  23. Wanted to let folks know. Thanks for all the comments. I got some dual with another cozybuilding in New England and it was a HUGE help.

     

    My basic problem boiled down to my wet out procedure and going to fast.

     

    After the dual, I went home and tackled F-28 and that went great. The part came out looking really good. I am moving on....

     

    Who turneda offa thea bubble machine? :rolleyes: (for those old enough to remember LW)

     

    Congratulations. The skill you learned will keep you in good stead throughout.

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