AIR FORCE MIL-S-38228-1964 SEALING COMPOUND ENVIRONMENTAL FOR AIRCRAFT SURFACES《飞机外部用环保型密封胶》.pdf
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1、Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Milttary MbH-3136 Standard Test Fluids; Hydrocarbon MIL-S-4383 Sealing Compound, Topcoat, Fuel Tank, Buna-I? Type MIL-$5059. %eel, Corrosion-Resistant (18-8), Plate, Sheet and Strip MIL-F-5566 Fluid; An
2、ti-Icing (Isopropyl Alcohol) MILT-7993 Titanium, Sheet, Strip and Plate (Unalloyed) MILP=8184 Plastic Sheet, Acrylic, . Modified STANDARDS Federal Federal Test ilubbert ,Tampling and Testing Method Std. No, 601 Military MIL-STD-129 Varking for Shipment ana Storage (Copies of specifications, standard
3、s, drawings, and publicat ions required by suppliers in connection with specific procurement functions should ba- obtained from the procuring activity or as dLrected by the contracting officer.) 2.2 Other pubiic8tions.d The following document forms a part of this specification to the exbent spedfied
4、 herein. Unless otherwise Tndicated, the issue in effect on date of invitation for bid.s or request for proposal. shall apply: Consolidated Classif cat ion Committee Untfdrm Freight Classification Rules (Application for copies of the above publication should be addressed to the Consolidated Classifi
5、cation Committee, 202 Chicago Union Station, Chicago, Illinois 60606, ) 3 6 REQUIREMENTS 3.1 Preproduction.- This specification makes provisions for. preproductior testing. 3.2 Materials.- The basic ingredient used in the manufacture of the sealing compound safi be a. synthetic rubber. The sealing c
6、ompound shall cure by the addition of a separate curing compound to the base compound and shall not depena on solvent evaporation for curing, Manufacturers will be given a wide latitude in the selection of materials and curing systems Provided by IHSNot for ResaleNo reproduction or networking permit
7、ted without license from IHS-,-,-MIL-S-38228 80 7777706 030b462 3 M MIL-S-38228 (USAI? 3.2.1 Color,- The color of the cured sealing compound shall be gray. 3.2.2 Appearance.- The base compound and curing compound (accelerator) shall be of a contrasting color , shall eagh be of a uniform blend and sh
8、all be free of skins, lunps, and gelled or coarse particles. There shall be no separation of ingredients which cannot be readily dispersed. 3.2.3 Toxicity.- The material shall have no adverse effect on the . health of personnel when used according to provided instructions and for its intended purpos
9、e. Questions pertinent to this effect shall be referred by the procuring activity to the appropriate department medical service who will act as an advisor to the procuring agenoy. 3.3 Physical properties 3.3.1 Specific gravity.- When tested in accordance with 4.7.1, the specific gravity of the cured
10、 sealing compound shall not exceed 1.65 at standard conditions (see 4.5). 3.3.2 Nonvolatile content.- When tested in accordance with 4.7.2 the nonvolatile content of the freshly mixed compounds (types I and 11s shall not be less than 97 percent by weight. 3.3.3 Viscosity of the base compound.- The s
11、ealing compounds shall be suitable for application by extrusion gun or spatula and the viscosity of the base compound shall be within the range of 6000 to 16,000 poises when tested as specified in 4.7.3. 3.3.4 Flow,- Vhen tested inaccordance with 4.7.4, the freshly mixed sealing compound shall exhib
12、it an initial flow within the limits of 0.10 to 0.50 inch when a cylindrical section formed in the flow .test jig is allowed to flow under its own weight on a vertical surface. In addition, the compound shall retain a flow within the limits of 0.10 to 0,50 inch throughout the eatbe application time.
13、 3.3.5 Application time,- 1Jhen.tested in accordance with 4.7.5, the mixed sealing compound shall have an application time as specified in table I and shall remain suitable for application during that period, The end of the application time shall be when the extrusion rate has diminished to.15 grams
14、 per minute, TABLE I Application Time Type I Hours Type II Rows I - 1/2 1-2 1-4 U2 2 4 II - 1/2 II - 2 11 - 4 112 2 4 . 3 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-3-3.6 Tack-free %me.- When tested. in accordance with 4.7.6, the mixed compound
15、shall cure to a tack-free condition as specified in table II. 1 7 1/2 10 24. XI - 1/2 5 24. 1-2 24 48 II - 2 24 48 1-4 48 72 II - 4 36 72 3.3.7 Curing rate.- When tested in aocordance with 4.7.7, the sealing compound shall-have a Rex hardness of not less than 35 after curing under standard condition
16、s (see 4.5) for not more than the time specified in table II. 3.3.8 Low temperature flexibility.- When tested in accordance with 4.7.8, the sealing compound shall withstand the low temperature flexi- bility test at -670 1: 2O F without cracking, checking, or loss of adhesion. 3.3.9 Peel strength.- W
17、hen tested in accordance with 4.7.9, the unaged cured sealing compound shall have a minimum peel strength of 20 pounds . It shall exhibit 100 percent cohesive failure, except for bubbles, knife cuts, and other causes that are obviously not the fault of the compound. The aged sealing compound shall c
18、onform to values specified in table III. 3.3.10 Corrosion.= laen tested in accordance with 4.7.10, the sealing compound Shan cause no visible corrosion of the aluminum panels and shall show no- sign of deterioration. 3.3.11 Tensile strength and elongation.- hen tested in accordance with 4.7.11, the
19、ultimate tensile strength and elongation of the cured compound shall be as specified in table III. 3.3.12 Accelerated storage stability.- After storing in accordance with 4.7.12, the base compound shall show no skinning, hardening, separation, nor settling of the material. It shall also conform to t
20、he original viscoslty specified in 3.3.3. The aged curing compound shall not be adversely affected and shall be restorable by normal agitation to a condition suitable for use. The aged base compound and the aged curing oompound, when mixed, shall be in accordance with conditions for flow, applicatio
21、n time, tack-free time and peel strength as specified in 3.3.4, 3.3.5, 3.3.6 and 3.3.9. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-S-38228 80 H 7777706 OLObllbLI 7 W TABU3 III - Physical Properties Properties Type I Type II Original Tensile
22、strength, psi Elongation, percent at 75O F 72 Hours immersion in MIL-H-3136, type III Tensile strength, psi Elongation, percent Peel strength (lb/in. ) (minimum) 72 Hours immersion in Di-2-ethylhexyl sebacate with 1/2 percent phenothiazine at 140 F Tensile strength, psi Elongat ion, percent Peel str
23、ength (lb/in . ) (minimum) 7 Days at 250 F Tensile strength, psi Elongation Tensile strength, psi Elongatfon, percent 7 Days at 500 F 450 100 “ “- - “ “- “- “W “- “ 40 75 3.3.13 Accelerated crazing.- The sealing compound shall not contain hgredients that will cause acrylic plactic sheet oonforming t
24、o Specification MIL-P-Et184 to craze or crack, when tested in accordance With 4.7.13. 3.3.14. Shrinkage.- Linear shrinkage, based on an initial measure- ment made after the appropriate cure time listed in 4,7.l4 and a - final measurement made after 60 days, shall not exceed 1,O percent. 3.3.15 Shavi
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