posted 02-03-2003 02:40 PM
When one is afraid to expose the truth it's easy to debunk any theory. It's that fear of the possibilities that really inhibits one's 'desire to learn'."""A CFM-56 is a CFM-56""" (It's good to see statements like this. It gives me a chance to review turbines for beginners again)
I must again refer you to the work being done by General Electric, John Ackermann, Randy Lewis, William Stowell and others.
The invention describes the use of turbine engines for the chemical reaction process.
It provides documentation that a CFM56 can be utilizied to compliment the theories of this board.
Anyone that states that you can't cram anything other than fuel through a turbine....... is wrong........
Further research on the Lewis's, Ackermann's, Rosnethal's and Stowell's of the world will support the chemtrail theory. It is understood that a patent does not a chemplane make but a rose by any other name would smell as sweet.
http://patft.uspto.g ov/netacgi/nph-Parser?Sect1=PTO2&Sect2=HITOFF&p=1&u=/netahtml/search-bool.html&r=13&f=G&l=50&co1=AND&d=ptxt&s1=CFM56&OS=CFM56&RS=CFM56
>>>As a non-limiting, general guideline, chemical reactions with a heat output up to the maximum output of a typical commercial aircraft engine are very suitable for this invention. An example of such an engine is General Electric's CFM56 model, which consumes approximately 4,500 kg of jet fuel per hour under take-off conditions, with an average heat output of about 43,000 kJ/kg. Thus, the total energy output would be about 195,000 kJ/hr, which generates approximately 11,500 newtons of thrust. A reaction size which more closely parallels heat output of the engine under cruise conditions would be more common for this invention. Such reactions consume less than about 1,400 kg of fuel per hour, with a corresponding heat output of less than about 5.8 million J/hr.<<<
>>>A wide variety of turbine engines may be modified and used in carrying out the present invention. They are all well-known in the art and described in a variety of references. Exemplary sources include U.S. Pat. Nos. 5,476,224; 5,475,979; 5,474,258; 5,472,313; 5,460,002; 5,435,126; 5,419,112; 5,404,709; 5,396,760; 5,323,604; 4,419,044; 4,414,815; 3,484,847; 3,484,144; and 3,448,582.<<<
Further information to establish the possibilities.
>>>Method and apparatus for protecting crops from frost by jet-dispersed, microencapsulated aerosols.<<<
[URL=http://patft.uspto.gov/netacgi/nph-Parser?Sect1=PTO2&Sect2=HITOFF&u=/netahtml/search-adv.htm&r=157&f=G&l=50&d=PTXT&s1=%27jet+turbine%27&p=4&OS=%22jet+turbine%22&RS=%22jet+turb ine%2]http://patft.uspto.gov/netacgi/nph-Parser?Sect1=PTO2&Sect2=HITOFF&u=/netahtml/search-adv.htm&r=157&f=G&l=50&d=PTXT&s1=%27jet+turbine%27&p=4&OS=%22jet+turbine%22&RS=%22jet+tur bine%2[/URL] 2
"""Assuming Boeing was being paid enough to do this secretly (although god knows why, as they don't make much money out of military contracts, commercial is the cashcow"""
This is no secret, it's just a little covert.
Again, the money spent upgrading KC135's to pacer-crag, cfm56 and 'other' modifications does not a chemplane make. I do find the large dollar value and the timing most interesting.
BOEING SITE search for ?KC-135 engine modification? http://www.boeing.com/news/releases/1997/news.release.970120a.html http://www.boeing.com/news/releases/1995/news.release.951010.html http://www.boeing.com/news/releases/1998/news_release_980922n.htm http://www.boeing.com/news/releases/1997/news_release_971111o.html http://www.boeing.com/news/releases/1997/news.release.970326a.html http://www.boeing.com/news/releases/2001/q2/news_release_010504n.htm
http://www.boeing.com/news/releases/1997/news.release.970106c.html
Yes the ability and capability exists, but who wants to disclose it?
Keyword search: Aerial Spray System http://w3.afrc.af.mil/units/910aw/spray/dod.af.htm
"""PS. I know you probably won't, but anyone with an ounce of common sense (linked to my name, getit? With the average IQ of this board you probably won't...) can see how incrediably stupid this theory is."""
My IQ must be on the average low side. If I had any common sense i'd have givin' up on the theory long ago.
No common sense here, just balls.
[Edited 1 times, lastly by ICU812 on 02-04-2003]