DuPont™ Vespel® CP parts offer an array of fiber or fabric reinforced composites for a range of unique design needs when wear and strength are key. Composite parts can be found as replacements for aluminum or titanium in tube clamps. Wear strips are “self-lubricating”. Typically CP parts are used in aircraft bushings, wear pads, washers, bumpers and seals.
Vespel® CP-8000 series composite parts are made from fibers braided into hollow tubes held in a matrix of resins. This produces bushings that offer the best combination of properties for applications that require the benefits that a composite structure offers. Toughness, thermal resistance, self-lubricity, and wear resistance are the most common requirements for the Vespel® CP-8000 series products.
Gross Weight | Net Weight | Carton Each | Carton Length | Carton Weight | Carton Height |
---|---|---|---|---|---|
0 | 0 | 0 | |||
0 | 0 | 0 | |||
0 | 0 | 0 |
Property | Value | Unit | Method |
---|---|---|---|
Glass Transition Temperature, Tg | Thermal Mechanical Analysis | °C (°F) | 360 (680) |
Thermal Expansion Coefficient | — | m/m/°C (in/in/°F) | 8.3 x 10–6 (4.6 x 10–6 ) |
Oxidative Stability | See notea | % weight loss | 3 |
TEST CONDITION – TDS-M202P (ULVAC) | — | — | 250(482) 10˚,10˚ 1.0(0.0022) 10-5/1.45 x 10-8 |
DEFLECTION | — | — | 330 /44 x 106 230(446) |
Property | Value | Unit | Method |
---|---|---|---|
DENSITY | — | — | 1.70 106 |
FINGER THICKNESS | — | — | 3 0.12 |
TEST CONDITION – ASTM E595-93 | — | — | 0.329 0.002 |
FLEXURAL MODULUS | — | — | 300 44 x 106 |
FINGER WEIGHT | — | — | 0.50 1.10 |
Fabric/material |
CP-8000 PARTS |
---|---|
Design |
BUSHING |
Seam |
NR-150 (PI) |
Packaging |
BUSHING,ROUND FLANGE |
Hazard |
|
Coated Material |
NR-150 |
Features |
BRAID |