GMW GMW17047-2013 Polyamide High Heat Resistant - Glass Fiber Reinforced Heat Stabilized Issue 1 English.pdf
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1、 WORLDWIDE ENGINEERING STANDARDS Material Specification GMW17047 Polyamide High Heat Resistant - Glass Fiber Reinforced, Heat Stabilized Copyright 2013 General Motors Company All Rights Reserved December 2013 Page 1 of 4 1 Scope 1.1 Material Description. This standard covers the properties of a glas
2、s fiber reinforced, heat stabilized, high temperature capable polyamide which is used in injected form for molded components. 1.2 Symbols. The material abbreviations according to ISO 11469 are shown in Table 1. 1.3 Typical Applications. Typical applications include the following: Engine covers, turb
3、o system components, and other underhood application where temperature resistance is desired. 1.4 Remarks. The classification into groups is according to the different ranges of glass fiber content. Additional glass ranges will be added as they become necessary. 2 References Note: Only the latest ap
4、proved standards are applicable unless otherwise specified. 2.1 External Standards/Specifications. ASTM D6869 ISO 188 ISO 527-1/2 ISO 3451 ISO 75 ISO 294 ISO 1183 ISO 11469 ISO 179/1eA ISO 527 ISO 1874-2 ISO 15512 2.2 GM Standards/Specifications. GMW3013 GMW3059 GMW3221 GMW14335 2.3 Additional Refer
5、ences. TMC003 Material Safety Data Sheet guidance documents (available at ). 3 Requirements 3.1 Requirements on Test Specimens. Reference GMW3221. 3.2 Requirements on Delivery. Important physical, mechanical and thermal properties that characterize the material are summarized in charts. The color sh
6、all be specified on drawings, in material specifications and otherwise. Unless otherwise specified, injection molding of test specimens shall be accomplished per ISO 294 with the conditions for injection molding from ISO 1874-2. All values indicated herein are based on material considered to be in t
7、he dry-as-molded state with moisture content of 0.2% maximum (ASTM D6869, ISO 15512, Method A or B, or GMW14335). Immediately after molding, specimens shall be sealed in moisture-proof containers and stored at 22 C 3 C for at least 24 h prior to test as specified in ISO 1874-2. All tests shall be pe
8、rformed on unannealed specimens immediately after their removal from the containers in a controlled atmosphere per GMW3221, Code A, unless otherwise specified. In addition, tests specified at temperatures below or above 22 C 3 C shall be conducted at the specified temperature using specimens conditi
9、oned at the specified temperature for 4 h minimum. The minimum values specified in the property tables must be met by test specimens in natural, black, or in a standard sampled color if natural or black are not available. 3.2.1 Compound Properties (Natural, Black and Integrally Colored). See Table 1
10、. The following are also required for full standard approval. The minimum number of lots per test required is one in natural: Poissons Ratio, Coefficient of Linear Thermal Expansion (CLTE), Mold Shrinkage, Stress Strain Curve at multiple temperatures (for example -30 C, 23 C, 85 C), Shear Modulus Cu
11、rve. See GMW3013 for the test procedures. Copyright General Motors Company Provided by IHS under license with General Motors CompanyNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-GM WORLDWIDE ENGINEERING STANDARDS GMW17047 Copyright 2013 General Motors Company All
12、 Rights Reserved December 2013 Page 2 of 4 Table 1: Compound Properties (Natural and Black) Glass Fiber Reinforcement Percentage 15% 35% Property Standard Units Value Value ISO Symbol ISO 11469 PA-GF15PA-GF35 Ash ISO 3451 % 13 to 17 33 to 38 Density ISO 1183 g/cm3 Target Range 1.15 to 1.30 Target Ra
13、nge 1.35 to 1.50 Moisture Content ISO 15512, Method A or B or GMW14335 % 0.2 0.2 Tensile Modulus ISO 527-1/2 MPa 5000 to 8500 10 000 to 12 500 Tensile Stress at Break ISO 527-1/2 MPa 85 120 Tensile Stress at Break after Heat Aging Note 1 ISO 188 ISO 527 % Retention 75 75 Tensile Strain at Break ISO
14、527-1/2 % 2.0 2.0 Notched Charpy Impact Strength At +23 C At -30 C ISO 179/1eA kJ/m2 6.0 3.0 9.0 5.0 Notched Charpy Impact after Heat Aging Note 2 ISO 188 ISO 179/1eA % Retention 75 75 Heat Deflection Temperature under Load 1.8 MPa ISO 75 C 200 230 Note 1: Specimens tested for Tensile Stress at Brea
15、k to ISO 527 after heat aging 1000 h 5 h at +180 C 5 C according to ISO 188, Method A (air oven method) shall have a minimum of 75% retention relative to unaged specimens tested concurrently. Note 2: Specimens tested for Notched Charpy Impact per ISO 179/1eA after heat aging 1000 h 5 h at +180 C 5 C
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