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Horse Power

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Old 01-24-2007, 07:01 PM
  #21  
Soaring
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Here's another piston driven engine.
>>>>
The largest internal combustion engine ever built is the Wärtsilä-Sulzer RTA96-C - a 14 cylinder, 2 stroke, turbocharged diesel engine that was designed to power the Emma Maersk, the largest container ship in the world. It weighs 2300 tonnes, and when running at 102rpm produces 109,000bhp, consuming some 13.7 tonnes of fuel each hour.<<<<
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Old 01-24-2007, 07:03 PM
  #22  
scott_m_mil
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I'm not sure that that bike made 50,000 it sounds like the dyno withstood lots of runs if i read it rights
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Old 01-24-2007, 07:05 PM
  #23  
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I like the turbine engine idea...

Didn't the SR-71 engine have no moving parts at supersonic speed? I remember something about that it utilized the airpressure to spontaneously combust once the fuel was applied...

If I find more info, I'll post (as long as we're off topic)
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Old 01-24-2007, 07:05 PM
  #24  
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ohhh did I read it wrong??? it's been a long day thanks scott
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Old 01-24-2007, 07:08 PM
  #25  
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http://www.sr-71.org/blackbird/sr-71/
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Old 01-24-2007, 07:09 PM
  #26  
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but isn't it supposed to be rope started??
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Old 01-24-2007, 07:09 PM
  #27  
scott_m_mil
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I thought turbine myself...but it doesn't technically have a stroke either?
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Old 01-24-2007, 07:21 PM
  #28  
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ORIGINAL: grruminator78

http://www.sr-71.org/blackbird/sr-71/
Nice find. Apparently the word I was looking for was "Ram Jet" technology. Thanks.

http://en.wikipedia.org/wiki/Ramjets
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Old 01-24-2007, 07:22 PM
  #29  
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NP google is my best friend!
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Old 01-24-2007, 07:26 PM
  #30  
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Default RE: Horse Power

ORIGINAL: crunchyskippy

I like the turbine engine idea...

Didn't the SR-71 engine have no moving parts at supersonic speed? I remember something about that it utilized the airpressure to spontaneously combust once the fuel was applied...

If I find more info, I'll post (as long as we're off topic)
The sr used a kerosene based fuel that was at something like -100*. It was used in part to help cool the plane at mach 8 (or however fsat it went).
-P.
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