High-temperature-resistant solid propellant for deep oil-gas well and preparation method thereof
A solid propellant and high-temperature-resistant technology, which is applied in the direction of offensive equipment, inorganic oxyhalide salt explosive composition, explosives, etc., can solve the problems of inability to use, and achieve the effect of good temperature resistance and excellent hydrolysis resistance
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[0037] The preparation method of the above-mentioned high temperature resistant solid propellant for deep oil and gas wells, the method is carried out according to the following steps:
[0038] Step 1, according to the formula ratio, in weight percentage, the high temperature resistant epoxy resin is 10.00% to 32.37%, the bisphenol A epoxy resin is 0 to 11.79%, and the epoxy resin reactive diluent is 0 to 12.77%. Add 0.03% foaming agent to the mixing pot and premix for 10 minutes;
[0039] In step 2, in percentage by weight, potassium perchlorate is added to the system in step 1 in an amount of 41.00% to 56.00%, and 1-oxo-2,6-diamino-3,5-dinitropyrazine is added in an amount of 10.00% to 25.00% , after 50 minutes of mixing, add 2-ethyl-4-methylimidazole to 0.98% to 1.60%, and stop mixing after 15 minutes of mixing to obtain medicinal slurry;
[0040] In step 3, the slurry obtained in step 2 is poured into a mold, put into an oven at 70° C. for curing for 24 hours, and demolde...
Embodiment 1
[0043] The high temperature resistant solid propellant for deep oil and gas wells of this embodiment is composed of the following raw materials in weight percentage: 41.00% of potassium perchlorate, 25.00% of LLM-105, 14.40% of TGDDM, and 5.40% of epoxy resin E-51 , o-tolyl glycidyl ether is 12.77%, silicone resin is 0.03%, 2-ethyl-4-methylimidazole is 1.40%.
[0044] Performance Testing:
[0045] Detonation heat is determined according to GJB770B-2005 method 701.2 explosion heat and combustion heat constant temperature method.
[0046] The specific volume is determined by the GJB770B-2005 method 702.1 specific volume pressure sensor method.
[0047] The test method of high temperature resistance is: Ф20mm×20mm grain column (1) 3℃ / min rise to 180℃, keep warm for 48h; (2) Temperature control point: The thermocouple is suspended directly above the sample and is not in contact with the sample. The thermal weight loss of the sample is not more than 3%, and the test is passed if it...
Embodiment 2
[0054] The high temperature resistant solid propellant for oil and gas deep wells of the present embodiment, in terms of weight percentage, is composed of the following raw materials: potassium perchlorate is 52.70%, LLM-105 is 13.30%, TGDDM is 43.37%, silicone resin is 0.03%, 2- Ethyl-4-methylimidazole was 1.60%.
[0055] The performance test method of the high temperature resistant solid propellant for oil and gas deep wells of this embodiment is the same as that of embodiment 1, and the performance test results are shown in Table 2.
[0056] Table 2 embodiment 2 performance test results
[0057]
[0058] It can be concluded from Table 2 that the explosion heat (ie energy) of the propellant is slightly higher, the specific volume is moderate, and the high temperature resistance, water resistance and salt water resistance all meet the performance requirements. It is suitable for the use of heat-resistant fracturing ammunition in deep oil and gas wells.
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