
We have seen that the fuel for military aircraft both for civilian aircraft, take special additives, prepared ad hoc according to particular specifications (see the StadiS 450), but for any other elements to spread , the poisoning of the planet need of technical aerosols, on the one hand, degrade the items missing and the other did not reveal abnormalities in the viewer and / or photograph the aircraft used for clandestine operations of aerosols.
To understand what are the resources available to anyone who wants to modify an airplane in a simple, cheap and without such changes arouse suspicion, we must understand the principle of operation of a turbofan : the engine's most popular airplane in the world . For this reason we have got a model CMF-56 next-generation, whose scheme does not differ much from turbofan other manufacturers.
Let's see how a turbofan engine
For an airplane can move and fly, it is necessary that a pushing force is generated by accelerating the flow 'air between the front and back of the engine. This is achieved through a large ducted fan placed in front of the engine.
These are engine components :
the first fan (fan) of large diameter; compressors bassa ed alta pressione, con vari stadi che gradualmente aumentano la pressione dell'aria che scorre attraverso gli stadi; la camera di combustione, in cui il carburante del jet è mescolato all'aria combusta; le turbine ad alta e bassa pressione dove l'alta pressione dei gas è ridotta, non appena le turbine dirigono i gas nella ventola.
Dei cinque stadi della turbina, uno sviluppa alta pressione; gli altri quattro bassa pressione.
In conclusione questo è l'intero apparato
Il CMF56 è un "high by-pass ratio engine" ossia un motore ad alto rapporto di diluizione tra aria fredda ed aria calda.
Il carburante viene espulso ed iniettato. La miscela di door air and fuel temperature to 1700 degrees Celsius. Finally, the stored energy is extracted in the five-stage turbine, just out of the combustion chamber.
Ultimately, the outside air is sucked by the fan in the compressor and then forced into the combustion chamber and mixed with fuel creates a mix that switches determines the expansion of hot gases that drive the turbine and generate momentum for the plane.
The remaining air passes out. The
turbofan engine is a dual-flow: the air is compressed, is heated by fuel burned, after it has passed through the turbines, which are composed of the compressors and fans.

aviation experts with whom we have consulted in recent weeks have confirmed that, indeed, this type of change is unusual and has no reasonable justifications. In addition, although many schemes examined turbofan engines of the type , we have not found in any case, the presence of sensors in that part of the engine, at the project level.

a) Gli elementi da disperdere in atmosfera non entrerebbero nella camera di combustione. Ciò confuterebbe l'obiezione dei disinformatori, secondo i quali non si possono addizionare composti chimici in un motore, poiché essi brucerebbero con il carburante.
b) Il cono di uscita sarebbe vicinissimo a the exhaust gas and this would make it difficult, for a careful eye, the emergence of spraying. We observe, however, that in many movies and photos, exit cones produced by the wakes are often three, compared with two engines, or five, or six compared with four engines. In this regard it is useful to view this movie.

Un tecnico militare addetto alla manutenzione e revisione delle componenti dei motori per aerei civili e militari ci ha riferito circa l'anomala ed anticipata usura della prima ventola di grande diametro che, guarda caso, sarebbe l'unico elemento rotante a diretto contatto con eventuali composti chimici abrasivi o corrosivi.
Fonti:
Bologna-airport.it
CFM56.com
Enciclopedia delle scienze , Milano, 2005, s.v. turbofan

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