Low-cost high-temperature pultruded epoxy resin for smart energy carbon fiber resin-based composite core
A carbon fiber resin-based, epoxy resin technology, applied in the field of low-cost high-temperature pultrusion epoxy resin, can solve the problems of difficulty in meeting the use requirements, prone to cracking, fracture, poor toughness of epoxy resin, etc., to promote rapid curing, Improve the heat and humidity aging resistance and the effect of not easy to absorb
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment 1
[0017] The composition, proportioning number and model of this embodiment are shown in Table 1:
[0018] Table I
[0019]
[0020]
[0021] The epoxy resin cost that present embodiment makes and performance are as follows:
[0022] The price of the epoxy resin system is 80-90 yuan / Kg, which is significantly lower than the existing 200 yuan / Kg.
[0023] Epoxy resin has a viscosity of 500-1000cps at 25°C.
[0024] It takes 10 hours for the viscosity of epoxy resin to double at 25°C.
[0025] The composite mandrel formed by the epoxy resin pultrusion made by the present embodiment can pass through the 50D winding cylinder body for 2min at a speed of 3r / min without peeling or cracking on the surface; / min speed to reverse 360 °, keep 2min, and then straighten, the mandrel does not crack. The pultruded composite mandrel is steadily applied with radial pressure at a speed of 2mm / min, and can withstand a pressure of more than 40kN. The Tg of the pultruded composite mandr...
Embodiment 2
[0027] On the basis of Example 1, adding 10-20 parts of polyethersulfone will further improve Tg and toughness, wherein Tg can be increased to 200-210°C, and the composite core passes through the surface of the 45D winding cylinder at a speed of 3r / min for 2min No peeling, no cracking.
PUM
| Property | Measurement | Unit |
|---|---|---|
| epoxy value | aaaaa | aaaaa |
| particle diameter | aaaaa | aaaaa |
| tensile strength | aaaaa | aaaaa |
Abstract
Description
Claims
Application Information
Login to View More 

