NAVY MIL-C-17435 C-1976 CUSHIONING MATERIAL FIBROUS GLASS《玻璃纤维缓冲物》.pdf
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1、MIL-C-17435C 4 March1976 SUPERSEDING 2 May 1955 MIL-C-17435B MILITARY SPECIFICATION CUSHIONING MATERIAL, FIBROUS GLASS s specification is approved for use by all departments and agencies of the Department of Defense. 1. SCOPE 1.1 Scope. This specification covers cushioning material composed of bonde
2、d fibrous glass. 1.2 Classification. The cushioning material shall be of the following types and classes as specified (see 6.3) : Type I - Uncoated Type II - Coated. Classes shall be as indicated in table II. 2. APPLICABLE DOCUMENTS * 2.1 The following documents of the issues in effect on date of in
3、vitation for bids or request for proposals form a part of this specification to the extent specified herein. Issue of documents. SPECIFICATIONS Federal *O - M- 2 32 *P-D-680 -/- Methanol (Methyl Alcohol). Dry Cleaning Solvent *QQ-A-250/4 Aluminum Alloy 2024, Plate and Sheet ru -=- -._,-+- THIS DOCUM
4、EgT CONTAliYS f I PAGES. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-*QQ- C - 5 76 Copper Flat Products with Slit, Slit and Edge-Rolled, Sheared, Sawed or Machined Edges (Plate, Bar, Sheet, RR-S-366 Sieve, Test “MMM-A-260 Adhesive, Water-Resistan
5、t (For Sealing Waterproofed Paper) “PPP- B-585 Boxes, Wood, Wirebound *PPP-B-591 Boxes, Shipping PPP - B-60 1 Boxes, Wood, Cleated-Plywood *PPP-B-621 Boxes, Wood, Nailed and Lock-Corner * PP P.- B - 6 36 Boxes, Shipping, Fiberboard MIL-STD-129 Marking for Shipment and Storage I I (Copies of specific
6、ations, standards, and .drawings zequirec contractors in connection with specific procurement functions should be I obtained from the procuring activity or as directed by the contracting I r- Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-C-1743
7、5C 1 W 9997706 0282343 7 MIL-C-17435C 3. REQUIREMENTS 3.1 Materials. The cushioning material shall consist of glass fibers matted, bonded, and otherwise treated to meet the requirements of this specification for the type and class specified. The surface fibers of type II material shall be coated wit
8、h an elastomeric material to prevent dusting, by the procuring activity. When required, a backing material shall be applied as specified 3.1.1 Fiber size and orientation. Unless otherwise specified, the glass fibers shall be oriented in a direction approximately perpendicular to the direction of loa
9、ding of the cushioning material, the range of fiber diameters shall be as specified by the procuring activity (see 6.3). When required, 3.2 Forms and dimensions. Unless otherwise specified (see 3,2.1), fibrous glass cushioning material shall be furnished in sheet form, or in rolls when feasible, in
10、the standard thicknesses shown in table I, and in lengths and widths specified by the procuring activity. lengths of sheets and on widths shall be *1/4 inch. Tolerance on lengths of rolls shall be k1.5 percent. Tolerances on TABLE I. Standard thicknesses. ! Thickness (inch) Tolerance (inch) 1/4 +O ,
11、031 1/2 tr ,062 3/4 f ,062 1 f ,062 3.2.1 Special forms and dimensions. When specified by the procuring activity, cushioning material cut or molded to special forms, thicknesses, or other dimensions shall be furnished. Tolerances shall be as indicated in the applicable drawings or other documents. 3
12、.3 Load-deflection values. The fibrous glass cushioning material shall have the load-deflection properties shown in table II and 3.3.1, Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-C-17435C MIL-Cl37435C BL 979990b 0282342 9 W TABLE II. Load-de
13、flection values. Class Load range at 25% deflect i on (psi) O 2-0.5 0.5-1.5 1 ,o-2 ,o 2.0-4.0 3.0-8.0 6 $0-15 low20 20-50 50-100 Maximum test deflect ion (%I 60 55 50 50 45 40 35 35 30 Load range at maximum test deflection (Psi 0.5-3.0 2.0-12 5 ,O-15 10-25 15 -30 25-50 40-80 45 -90 50-120 3.3.1 Over
14、load. When tested as specified in 4.4.4.4, the redetermined load shall be within 15 percent of the original load required to produce the maximum test deflection value indicated in table II for the class of material tested. 3.4 Compression set. After compression to the maximurn test deflection shown
15、on table II (see 4.4.5) corresponding to the class of material, the cornpression set after 48 hours shall not exceed 5.0 percent of the original thickness. 3.5 Load-deflection at 250 F.l At a temperature of 250 1: 5 F, the load (see 4.4.6) required to produce the maximum test deflection shown in tab
16、le II for material of the corresponding class shall be at least 50 percent of the load for the same deflection at room temperature, 3.6 Compression set at 250 F.l The material, when tested as specified in 4.4.7 at a temperature of 250“ 1: 5“ F, using deflection values one-half as great as the maximu
17、m test deflections for the corresponding class in table II, shall show a compression set not exceeding 5 percent of the original thickness. 3.7 Accelerated aging. After heating as Specified in 4.4.8 for 15 hours at 300 1: 10 F, then testing at room temperature as in 4.4.4.4, the loads required to pr
18、oduce the maximum test deflections shown in table II shall be within 5 percent of the original loads. INot applicable for Air Force purchases. 4 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-C-17935C 41 9999706 0282193 O W MI L-C- 17435C 3.8 Du
19、sting. When tested as specified in 4.4.9, the weight loss for type I material shall not exceed 0.25 percent of the original weight of the sample. 0.05 percent, and the surface coating shall show no separation from the fibers, For type II material the weight loss shall not exceed 3.9 Flame resistance
20、, When tested as specified in 4.4.10, the material shall not support combustion after removal from the flame. A glow is permitted for not more than 15 seconds thereafter. * 3.10 Metal corrosion. inen tested as specified in 4.4.11, specimens of steel, copper, and aluminum alloy in contact with the cu
21、shioning material shall show no more corrosin than the control specimens. - 3.11 Water resistance. The binder shall not dissolve in distilled water, and the cushioning material shall retain its original shape and form after removal from water, when tested as specified in 4.4.12. 3.12 Workmanship. Cu
22、shioning material shall be manufactured in accordance with the highest standards of workmanship. The material shall be as uniform as commercially possible and shall be practically free of irregularities, loose or unbonded fibers, nonfibrous glass, or other occlusions. 4. QUALITY ASSURANCE PROVISIONS
23、 * 4,l Responsibility for- inspection. Unless otherwise specified in the contract or purchase order, the contractor is responsible for the performance of all inspection requirements as Specified herein. Except as otherwise specified in the contract or order, the contractor may use his own or any oth
24、er facilities suitable for the performance of the inspection requirements specified herein, unless disapproved by the Govern- ment. The Government reserves the right to perform any of the inspections set forth in the specification where such inspections are deemed necessary to assure supplies and se
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