FORD WSS-M2D486-A-2016 TUBING SILICONE (VMQ) HIGH TEMPERATURE HOT AIR RESISTANT TO BE USED WITH FORD WSS-M99P1111-A .pdf
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1、 ENGINEERING MATERIAL SPECIFICATION Date Action Revisions Rev 03 2016 07 05 Revised See Summary of revision J. Souza, SA 2006 04 05 Revised Corrected test methods in para 4.5.4 and 4.5.5 T. Covert 1996 06 13 Activated T. Covert Controlled document at www.MATS.com Copyright 2016, Ford Global Technolo
2、gies, LLC Page 1 of 6 TUBING, SILICONE (VMQ), HIGH TEMPERATURE, HOT WSS-M2D486-A AIR RESISTANT 1. SCOPE The material defined by this specification is a long life, high temperature oil resistant, ozone resistant, moderate to low pressure silicone rubber hose with ability to service low temperature do
3、wn to -40 C. 2. APPLICATION This specification was released originally for material used in connectors for the engine charge air and or Turbo Charged connections. The tubing is not recommended for engine coolant or engine oil. The hose construction shall consist of silicone rubber coated on woven ar
4、amid (Nomex) cloth. 3. REQUIREMENTS Material specification requirements are to be used for initial qualification of materials. 3.1 APPROVED SOURCES This specification requires the use of approved sources. Only the sources identified on the Ford Approved Source List (ASL) can be used when this specif
5、ication is listed on the drawing, CAD file, or other documents. The list of approved sources is located within Ford at or available externally through a Ford Materials Engineer. 3.2 CONDITIONING AND TEST CONDITIONS All test values are based on material conditioned for not less than 24 h prior to te
6、sting in a controlled environment of 23 +/- 2 C and 50 +/- 5% relative humidity. Testing of the material should occur in the conditioning environment or soon after removal. 3.3 INFRARED SPECTROPHOTOMETRY AND/OR THERMAL ANALYSIS IR spectra and thermograms from initial material approval shall constitu
7、te the reference standard and shall be kept on file at the designated material laboratory. The material supplier shall ensure that all future material supplied to the specification shall produce IR spectra and thermograms that correspond to the reference standard when tested under the same condition
8、s. 3.4 SAMPLE SIZE Refer to Table 1 for number of samples required for each test to establish conformance to specification limits 3.5 MATERIAL TESTING 3.5.1 Preparation of Test Specimens ENGINEERING MATERIAL SPECIFICATION WSS-M2D486-A Copyright 2016, Ford Global Technologies, LLC Page 2 of 6 Wheneve
9、r possible, all test specimens shall be die-cut from the finished parts. When not feasible, specimens cut from molded test sheets manufactured from the same material and with equivalent cure to molded parts are recommended. The test sheets shall have the following dimensions: 150 x 150 mm, min x 2.0
10、 +/- 0.2 mm 3.6 ORIGINAL PROPERTIES 3.6.1 Density 1.11 - 1.35 g/cm3 (ISO 1183, Method A/ASTM D 297) 3.6.2 Hardness, Durometer A 40 - 55 (ISO 868/ASTM D 2240) 3.6.3 Tensile Strength at Break 6 MPa min (ISO 37/ASTM D 412, Die C, 500 mm/minute test speed) 3.6.4 Elongation at Break 200% min (ISO 37/ASTM
11、 D 412, Die C, 500 mm/minute test speed) 3.6.5 Tensile Modulus at 100% Elongation 0.86 MPa min (ISO 37/ASTM D 412, Die C, 500 mm/minute test speed) 3.6.6 Tear Strength 9 kN/m min (ISO 34, Method B, procedure (a)/ ASTM D 624, Die B) 3.6.7 Low Temperature Brittleness pass (ISO 812, Type B specimen/AST
12、M D 2137, Method A) 9.3.2, non-brittle after 3 min at -55 C 3.6.8 Ozone Resistance (FLTM BP 101-01, Procedure A) “0“ Rating 3.6.9 Compression Set 50% max (ISO 815/ASTM D 395, Method B, except 25% compression, plied-up specimens, 22 h at 175 +/- 2 C) 3.7 HEAT AGED (ISO 188/ASTM D 573, 150 +/- 50 air
13、changes/h, 168 h at 175 +/- 2 C) 3.7.1 Hardness Change +10 3.7.2 Tensile Strength Change +30% max 3.7.3 Elongation Change -40% max 3.7.4 Visual Evaluation No surface tackiness or cracks when folded flat against itself. ENGINEERING MATERIAL SPECIFICATION WSS-M2D486-A Copyright 2016, Ford Global Techn
14、ologies, LLC Page 3 of 6 3.8 HEAT AGED (ISO 188/ASTM D 573, 150 +/- 50 air changes/h, 1000 h at 175 +/- 2 C) 3.8.1 Hardness Change +20 3.8.2 Tensile Strength Change -40% max 3.8.3 Elongation Change -50% max 3.8.4 Visual Evaluation No surface tackiness or cracks when folded flat against itself. 3.9 I
15、MMERSION IN OIL IRM 901 (ISO 1817/ASTM D 471, 168 h at 23 +/- 2 C) 3.9.1 Hardness Change 0 to -10 3.9.2 Tensile Strength Change -20% max 3.9.3 Elongation Change -20% max 3.9.4 Volume Change 0 to +15% 3.9.5 Visual Evaluation No surface tackiness or cracks when folded flat against itself. 3.10 SILICON
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