A kind of manufacturing method of low-cost dual-element carbon matrix aircraft carbon brake disc
A manufacturing method and technology of dual carbon, applied in the direction of brake discs, mechanical equipment, gear transmission mechanisms, etc., can solve the problems that are not conducive to mass industrial production, unstable product quality consistency, poor structure uniformity, etc., to achieve Improve wet braking performance, improve structural uniformity and quality consistency, and reduce the effect of opening ratio
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Embodiment 1
[0036] This embodiment includes the following steps:
[0037] Step 1. Set the density to 0.50g / cm 3 The needle-punched non-weft carbon cloth integral carbon disc preform is loaded into a high-temperature heat treatment furnace, and subjected to high-temperature pretreatment at a temperature of 1800 ° C; the needle-punched non-weft carbon cloth integral carbon disc preform is composed of carbon fiber plain cloth and carbon The fiber mesh tires are alternately layered and made by radial needle punching;
[0038] Step 2, the needle-punched non-weft carbon cloth integral carbon disc preform after high temperature pretreatment in step 1 is loaded into a vapor deposition furnace with a diameter of 600 mm, and the furnace loading structure is as follows: figure 1 As shown, the needle-punched non-weft carbon cloth integral carbon disc preform 4 after high temperature pretreatment is loaded into the furnace chamber surrounded by the heating element 2 of the vapor deposition furnace to...
Embodiment 2
[0043] This embodiment includes the following steps:
[0044] Step 1. Set the density to 0.70g / cm 3 The needle-punched non-weft carbon cloth integral carbon disc preform is loaded into a high-temperature heat treatment furnace and subjected to high-temperature pretreatment at a temperature of 2400 ° C; the needle-punched non-weft carbon cloth integral carbon disc preform is composed of carbon fiber twill cloth and carbon fiber The mesh tires are alternately layered and made by radial needle punching;
[0045] Step 2: Put the needle-punched non-weft carbon cloth integral carbon disc preform after high temperature pretreatment in step 1 into a vapor deposition furnace with a diameter of 650 mm, and put the needle-punched non-weft carbon cloth as a whole after high temperature pretreatment. The carbon disc preform 4 is loaded into the furnace chamber surrounded by the heating element 2 of the vapor deposition furnace to form a single material column. The top of the single materi...
Embodiment 3
[0050] This embodiment includes the following steps:
[0051] Step 1. Set the density to 0.65g / cm 3 The needle-punched non-weft carbon cloth integral carbon disc preform is loaded into a high-temperature heat treatment furnace, and subjected to high-temperature pretreatment at a temperature of 2000 ° C; the needle-punched non-weft carbon cloth integral carbon disc preform is composed of carbon fiber plain cloth and carbon The fiber mesh tires are alternately layered and made by radial needle punching;
[0052] Step 2: Load the needle-punched non-weft carbon cloth integral carbon disc preform after high temperature pretreatment in step 1 into a vapor deposition furnace with a diameter of φ of 1400 mm. The furnace loading structure is as follows: figure 2 and image 3 As shown, the needle-punched non-weft carbon cloth integral carbon disc preform 4 after high temperature pretreatment is loaded into the furnace chamber surrounded by the heating element 2 of the vapor depositio...
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