NAVY MIL-C-22284 A-1965 CONTAINER AIRCRAFT FIRE EXTINGUISHING SYSTEM BROMOTRIFLUOROMETHANE CF3BR《CF3BR甲烷飞机灭火系统容器》.pdf
《NAVY MIL-C-22284 A-1965 CONTAINER AIRCRAFT FIRE EXTINGUISHING SYSTEM BROMOTRIFLUOROMETHANE CF3BR《CF3BR甲烷飞机灭火系统容器》.pdf》由会员分享,可在线阅读,更多相关《NAVY MIL-C-22284 A-1965 CONTAINER AIRCRAFT FIRE EXTINGUISHING SYSTEM BROMOTRIFLUOROMETHANE CF3BR《CF3BR甲烷飞机灭火系统容器》.pdf(17页珍藏版)》请在麦多课文档分享上搜索。
1、MIL-C-2228aC WP) 7 September 1965 Superseding MIL-C-22284(Wep) 11 December 1959 MILITARY SPEC IF ICATION CONTAINER , AIRCRAFT FIRE EXTINGUISHING SYSTEM , BROMOTRIFLUOROMETHANE , CF3BR This specification has been approved by the Bureau of Naval Weapons, De- partment of the Navy. 1. SCOPE 1.1 Scope -
2、This specification covers containers for bromo- trifluoromethane, CF3Br, for use in aircraft fire extinguishing systems of the high rate discharge type, 1.2 Classification - The containers shall be of the types listed in Table I, as specified (see 6.2): Type CF-2 CF-OD CF-6 CF-6D CF-11 CF-11D CF-15
3、CF-15D CF-18 CF-18D CF-27 CF-27D CF-30 CF-30D Discharge Outlet Single Dual Single Dual Single Dual Single Dual Single Dual Single Dual Single Dual TABLE Internal Volume Cubic Inches 86 86 224 224 378 3 78 536 536 630 630 945 945 1050 1050 CF3Br Charge Lbs e 2.5 2.5 6.5 6.5 11 11 15 15 18 18 27 27 30
4、 30 Max. Weight Charged Container - Lbs. 10 12 1/2 15 17 1/2 22 1/2 24 28 1/2 31 33 35 1/2 47 50 53 56 ? Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-2. APPLICABLE DOCUMENTS 2.1 Government documents normally furnished - The following documents, of
5、 the issue in effect on date of invitation for bids or re- quest for proposal, form a part of this specification to the extent speci- fied herein. SPECIFICATIONS Mili tarv MIL-P-116 MIL -C -49 O MIL-T-5021 MIL-E-5272 MIL-N-6021 M IL -L - 71 78 MIL-E-7729 MIL-S-7742 MIL -P-8 58 5 MIL-D-8635 Preservat
6、ion, Methods of Cleaning and Preparation of Ferrous and Zinc Coated Surfaces for Organic Protective Coatings Tests,Aircraft Welding Operators Cer t i f icat ion Environmental Testing, Aeronautical and Associated Equipment, General Specification for Nitrogen; Liquid and Gas Lacquer; Cellulose Nitrate
7、, Gloss, for Aircraft Use Enamel; Gloss, for Aircraft Appli- cation Screw Threads, Standard , Aeronautical Primer; Coating, Zinc Chromate, Low Moisture Sensitivity Decals, for Use on Interior Surfaces . 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,
8、-,-MIL-D-70327 STANDARDS Federal FED-STD- 59 5 Mi li tary Colors -_ MIL-C-22284A Lb 7977706 OL920b3 L - MIL-C-22284A(WP) Military (continued) MIL-B-12218 MIL-D-21625 Bromot ri f luorome t hane (Lique f ied ) Design and Evaluation of Cartridges for Cartridge Actuated Devices MIL-E-22285 Extinguishing
9、 System, Fire , Air- craft, High-Rate-Discharge Type, Installation and Test of Drawings, Engineering and Asso- ciated Lists MIL-STD-105 Sampling Procedures and Tables for Inspect ion by Att ribates MIL-STD-143 Specifications and Standards, Order of Precedence for the selection of MIL-STD-794 Parts a
10、nd Equipment, Procedures for Packaging and Packing of MS33586 Metals, Definition of Dissimilar MS 3 3 6 56 Fitting End, Standard Dimensions for Flared Tube Connection and Gasket Se al Air Force-Navy Aeronautical Design Standards AND10050 Bosses, Standard Dimensions for Gasket Seal, Straight Thread (
11、When .requesting applicable documents, refer to both title and number. Copies of unclassified documents may be obtained from the Commanding Officer, Naval Supply Depot (Code 1051), 5801 Tabor Avenue, Philadelphia, Pennsylvania 19120. Requests for copies of classi- fied documents should be addressed
12、to the Naval Supply Depot, via the cognizant Government inspector, ) 3 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-C-22284A 3b 9777906 0392064 3 MIL At the end of this test, the mounting lugs shall be examined. There shall not be any failure,
13、 cracked weld, or permanent deformation, . 4.6.5 Discharge -One charged container shall be discharged through 10 feet of stainless steel tubing terminating in a tee having a total outlet areaof 120 percent of the line area. Ninety percent of the contents of the container shall be discharged in not m
14、ore than 0;8 second. The tubing sizes used for this test shall be as listed below: Container Type Tubing O. D. CF-2 and CF-2D 5/8 inch CF-6 and CF-6D 1 inch CP-11 and CF-11D 1 1/4 inch CF-15 ad CF-15D 1 1/4 inch CF-18 and CF-18D 1 3/4 inch CF-27 and CF-27D 1 3/4 inch CF-30 and CF-JOD 1 3/4 inch 4.6.
15、6 Proof pressure -One container shall be subjected to a proof pressure of 1400 psi, minutes and then released. There shall not be any permanent deformation or damage. furnished by the manufacturer. The pressure shall be retained for 10 Frangible disks, if used, shall be replaced by s,teel disks -. .
16、 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-4.6.7 Overheat safety outlet - Operation of the overheat safety device shall be verified by one of the f)llowing tests, as applicable. 4.6.7.1 Frangible diaphram type - The charged container shall be s
17、ubjected to internal pressure and the diaphragm shall rupture at a pressure between 1250 psi and 1400 psi at 160OF. 4.6.7.2 Fusible plug type - The charged container shall be subjected to heat and the plug shall yield at a temperature beiween 205OF and 220F. 4.6.8 Hydrostatic bursting - One containe
18、r shall be hydro- statically tested to destruction and the bursting pressure recorded. The minimum bursting pressure shall be 1800 psi. Before pressure is applied, the frangible disks, if used, shall be replaced by steel disks furnished by the manufacturer. 4.6.9 Environmental - The charged containe
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