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facthunter

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Everything posted by facthunter

  1. That OHLSSEN is Actually a Brown Junior. The first model engine to be mass produced in the USA. About 50,000 were produced between 1935 and 1941. Nev
  2. On the suck side of a Water pump there is usually a coiled spring to Prevent the rubber hose collapsing. There's NOT ALWAYS Positive pressure and it's limited by the CAP at higher temps. The Pressure CAP raises the Boiling Point. Nev
  3. It's commonly used (very effectively) in cooling rubber Pipes and other ducting where Low pressure can exist and collapse the section. Pretty unlikely to fracture in those applications. Nev
  4. Put a coil spring in it. Nev
  5. They are probably a bit jittery about them. Nev
  6. Expecting such a low price for a complete wing is a Bit Insulting. You couldn't clean it Properly for that. Nev
  7. Carefully check it's rapid throttle response. That's what I'm concerned about Most. Nev
  8. Not really, The Ohlsson (spark ignition) Motor there was out of date Long before got a Motor. A FROG 150, about 1953. I can't recall what became of it. I only flew it control line, Once. It would have been free flight after that. Maybe it thermalled away? Nev
  9. Now I see, said the Blind Man. Nev
  10. 3 axis Planes DO fly when upside down. That's why I prefer them. Nev
  11. Just about doubled the DRAG. Nev
  12. Faux Pas. Foh Pah. "Make Not". Usually when a Comment is inappropriate.. NOT for errors of spelling or Fact. Nev
  13. FFS Fat Finger Syndrome. Nev
  14. it also covers being conned into being a NUN. Nev
  15. NEVER again Skip. Nev
  16. This "Constant power" thing is a misconstruction of the Issue. The first thing happening to an aero engine is FULL power from not fully warmed up for a max of 5 minutes, The time limit is because the engine is being used as a HEAT SINK. THEN IT climbs at METO to cruise level where it then drops Back to say 75% POWER till Top of descent. It doesn't get any rest. On one flight I did the time was 12 Hours. The four engines didn't miss a beat. (that time). Nev
  17. I personally think the chev Alloy V8 is a reasonable Motor for Aircraft, and said so BEFORE it was used in glider towing. It's NOT their High Performance engine though. It's a 2 valve Pushrod Motor. The Mercury V8 Motor is a very specialised Product. The Chev. alloy Block wouldn't like sea water. Even Cast iron doesn't. Nev
  18. Lycoming build a lot of different versions of any sized engine. Nev
  19. That's news. Are they very Popular?
  20. Yes they are mass Produced and FAR better than Older engines ever were and relatively Much cheaper trouble free (Till your battery goes flat and all the Management disappears and they have the vehicle for a week) and MORE SPECIFIC to the USE they were designed for. Not anything else Particularly, as time goes on. Nev
  21. Plenty of improvements since 1950. Materials and processes. Some heads are forged and then Milled Just because they Look the same doesn't mean they are. Nev
  22. Note. I didn't see Turbo's post before I Posted. Nev
  23. You should be talking of clearances, NOT tolerances and the clearances when the engine us Running. is what matters. 4 Valve heads are near impossible to cool effectively without liquid cooling as the 2 exhaust valves in each head are very close together. but are NOT needed. Good U/L engines shouldn't need to be complex. Liquid cooled engines run cooler than optimum for efficiency and Play up more in hot Ground temp environments. Ie Overheat on the ground if time is Prolonged. The also have the drag of radiators and vulnerability of Leaks and extra complexity, COST and weight and need to check Hoses, radiator Mounts water Pump seals etc and you don't want head gaskets and joins, IF they can be avoided. Nev
  24. Some Australian outlets for Chinese products MAY Choose to get a cheaper version. They will make what you want (as long as you keep a good eye on them). Their factories go for Miles. Chrysler/Jeep are no different .Some Indian stuff is real bad. Nev
  25. Some had 2 strokes. I can't recall one with a 912.. Nev
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