Method for improving cracking and stable performance of jet fuel
A jet fuel, stable technology, applied in the direction of hydrocarbon oil cracking, petroleum industry, etc., can solve the problems of heat-absorbing fuel hypersonic aircraft heat management process is rare, carbon deposits, catalyst service life is short and so on, to improve fuel cracking rate, Effect of improving heat sink and prolonging service life
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Embodiment 1
[0016] Example 1: A supercritical endothermic fuel pyrolysis and coking evaluation platform was used to simulate the cracking and coking of fuel in the heat exchange system of a hypersonic aircraft, and n-dodecane was selected as the probe fuel. Using the method of Chinese patent CN200710058969.4, the ZSM-5 molecular sieve membrane is coated on the inner surface of the tubular reaction tube, the outer diameter of the tube is 3mm, the inner diameter is 2mm, and the coating amount of ZSM-5 molecular sieve is 2mg / cm 2 ; The hydrogen-donating agent is tetrahydronaphthalene, and its added concentration is 2wt.%.
[0017] The pyrolysis reactor is set to have a temperature of 600°C in the experimental section, a pressure of 4MPa, a reaction time of 2 hours, and a feed mass space velocity of 300h -1 .
[0018] Experimental conditions and operation are the same as in Example 1, and the hydrogen-donating agent tetrahydronaphthalene is replaced by: decahydronaphthalene, benzyl alcohol, ...
Embodiment 9
[0019] Embodiment 9: Experimental condition and operation are the same as embodiment 1. The difference is that the catalyst is ZSM-5 molecular sieve (purchased from Catalyst Factory of Nankai University) loaded with Pd and Pt (the loading amount is 1wt.%, the mass ratio of Pd and Pt is 1:1).
Embodiment 10
[0020] Embodiment 10: Experimental condition and operation are the same as embodiment 1. The difference is that the catalyst is coated with Y-type molecular sieve (purchased from Nankai University Catalyst Factory) in the tubular reaction tube, and the coating amount of molecular sieve is 3mg / cm 2 , choose n-dodecane with a sulfur content of 200ppm as the probe fuel. The hydrogen-donating agent is tetrahydronaphthalene, and its added concentration is 4wt.%.
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