Monday, October 5, 2020

Engines / Powerplants

  • Engine will lose about 3% of its power for every 1,000’ of altitude
Carb Heat:
CHT (cylinder head temperature): see Temperature below.

EGT (exhaust gas temperature): see see Temperature below.

Fuel:
Exhaust valve recession: - what causes it? (GA News).

Jets / Turbofan / Turboprop:
Leaning: +
  • In General:
    • Before increasing power settings, return slowly towards full rich .
    • Whenever mixture is adjusted, rich or lean, it should be done slowly.
    • Use full rich mixture during take-off or climb below 5K density altitude (Lycoming).
    • Anytime power setting is 75% or less at any altitude.
    • Why do we do it? (Vid 3).
  • Airports (low altitude) < 5K density altitude:
    • Adjust mixture for descent, but only as required.  Keep the engine running smoothly.
  • Airports (high altitude) > 5K density altitude:
    • Lean for taxi, take-off, traffic pattern entry and landing.
    • How to (Rob Machado)
  • Ground ops:
  • Fuel economy - how to lean the mixture for it. (Flying).
  • Methods:
    • Fixed props: gradually lean mixture until either tachometer or airspeed peaks.
      • From a 1969 172 POH, “…the mixture should be leaded as follows:  pull mixture control out until engine RPM peaks and begins to fall off, then enrichen slightly back to peak RPM.
    • Controllable pitch props: lean until a slight increase of airspeed is noted.
      • Slowly lean mixture until engine becomes rough or until power rapidly diminishes as noted by undesirable decrease in airspeed.  When either occurs, enrich mixture to obtain an evenly firing engine or to regain most of the lost airspeed or engine RPM.
      • When leaned, roughness is caused by misfiring due to a mixture which can’t support combustion.  It’s eliminated by slightly enriching mixture.
    • With EGT: lean to 100°F on rich side of peak EGT for best operation.
    • At all times, caution must be taken not to shock cool the cylinders.  Maximum recommended temperature change should not exceed 50°F per minute.
    • FAA on leaning 
    • Lycoming on leaning
  • Traffic pattern: before entering, go full rich (as required).
  • Why does the engine run rough when it's lean? Vid 4 or Vid 109.
  • Reference / Articles:
  • See also Mixture below.
Lycoming:
Magnetos:
Mixture:
Oil:
Percent power (RPM):
  • We often see references to 75%, 65% or some other percent of max power setting.  It's easy if a pertinent chart/reference has the correlated RPM setting, but many do not.  When there isn't an RPM setting, it is completely frustrating.  For example, if your max RP is 2700 RPM, 75% power is NOT 2025 RPM.  It's actually 75% HP - which makes sense - but how do you calculate that?  It would seem if 2700 was 100% HP, 2025 would give you 75% HP...but it does not.  
  • In studying engines and this problem, I've come up with a possible equation to calculate your percentage RPM settings.  I underlined "possible" because I haven't correlated it to every engine.  It goes like this - and it's pretty simple:
    • Subtract the percentage from 100, multiply by 10, subtract from MAX
    • Example:  75% of 2700 and 65% of 2700
      • 100-75 = 25 x 10 = 250.  2700-250 = 2450 RPM (75% RPM)
      • 100-65 = 35 x 10 = 350.  2700-350 = 2350 RPM (65% RPM)
    • I hope this helps.  This question has bothered me for quite some time and it's a question students ask.
Power settings:
Starting engines:
Temperature(s):
  • Four different engine temps, and what they mean to you. (Vid 17).
  • CHT (cylinder head temperature)
    • How fuel flow affects CHT. (Vid 15).
    • If too high > Enrich mixture / decrease pitch attitude / reduce power / open cowl flaps
    • Shock cooling > avoid it by allowing CHT to drop slowly
    • Why are my cylinder head temperatures different? (Vid 7).
  • EGT (exhaust gas temperature):
    • Lean to 100°F on rich side of peak EGT for best operation (technique).
    • What's EGT used for? (Vid 6Vid 11 or Vid 80).
Thrust:
  • What happens to max available thrust as temperature increases? (Vid 11)
Turbochargers:
- FIG -

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