NAVY MIL-S-5458 A-1951 SLEEVES SPARK PLUG TERMINAL [Use NAVY MIL-L-19844 A CANC NOTICE 2 NAVY MIL-L-19844A NOTICE 1 NAVY MIL-L-19844A]《火花塞线接头衬套》.pdf
《NAVY MIL-S-5458 A-1951 SLEEVES SPARK PLUG TERMINAL [Use NAVY MIL-L-19844 A CANC NOTICE 2 NAVY MIL-L-19844A NOTICE 1 NAVY MIL-L-19844A]《火花塞线接头衬套》.pdf》由会员分享,可在线阅读,更多相关《NAVY MIL-S-5458 A-1951 SLEEVES SPARK PLUG TERMINAL [Use NAVY MIL-L-19844 A CANC NOTICE 2 NAVY MIL-L-19844A NOTICE 1 NAVY MIL-L-19844A]《火花塞线接头衬套》.pdf(7页珍藏版)》请在麦多课文档分享上搜索。
1、1, SCOPE I8 APRIL, 1951 Superseding MIL-S-5450 14 December zl9Li9 MI LTTARY SPECIFICATION BLEEag, Preparation of (For Engines, Accessories and Other Auxiliary Equipment) mel; Aircraft Reciprocating Engine Fuel; Aircraft Engine, Grade JP-1 r Fuel; Aircraft Turbine and Jet Engine, kade JPi3 Packaging
2、and Packing for Overseas Shipmerit - Packaging and Packing for Oversea5 Shipment - , Packaging and Packing for Overseas Shipment - Packaging and Packing for Overseas Shipment - Paokaging nnd Paoking for Overseas Shipmen* Packaging and Packing for Overseas Shipment - Packaging and Packing for Oversea
3、s Shipment - . Boxes; Wood, Cleated, Plywood Boxes; Wood, Nailed Cartons, Folding, Paperboard : Barries-Materials, Waterproofl Flexible Boxes, Set-Up, Paperboard Plywood, Container Urade Adhesive, Water-Resistant, Case-LineP ._ . Air Force-Navy Aeronautical AN-P-u U. S. Amy Preservation and Packagin
4、g; Parts and Equipment (mneral Specification for) 94-40645 Marking j Exterior, Domestia and Export Shipment, by Contractors Nongovernmental Society of Automotive Engineers, Inc, 5688 Steel Wire, Corrosion Reslatant, 318 Chromium, 8 Nickel (Spring 1 (Copies of this specification may b obtained from t
5、he Society of Aufo- motive Engineers, InIC I P % Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-2.1.2 Other Publicationsr- Bureau of Supplies and Accounts Navy Shipment Marking Handbook 2.1.3 Drawings.- Air Force-Navy Aeronautical Standard Drawin4 A
6、N4164 Sleeve - Spark Plug Terminal. . (Copies of this specification and copies of other publications referenced herein or required for Government procurement, and the Index of Military Aeronautical (AN or MIL) Standards, may be obtained upon application to the Commanding General, Air Materie1 Com- m
7、and, Wright-Patterson Air Force Base, Dayton, Ohioj or the Commanding Officer, U. 3. Naval Air Station, Johnsville, Pennsylvania,) . 3e RXQUIREMENTS 3.1 Materia$.- Materiala shall conform to applicable Government specificationsr Materials which are not covered by applicable specifications shall be o
8、f the best com- mercial quality and suitable for the purpase intended. 3.1.1 Metals.- The spring shall be fabricated of corrosion-resistant steel wire (18 chromium, Bnickel) conforming to AM9 Specification No. 5688 or equal, The eyelet shall be of a corrosion-resistant type, .I 3.1.2 from carbon, no
9、n-tracking, and free from burrs, nicks; cracks, and other defects. 3.1.2.1 Solubility.- The materials shall be insoluble in carbon tetrachloride, acetone, and fuels conforming to Specificatd-ons MIL-F-5572, MIL-F-5616 and MTL-F-5624 at temperatures up to 65“ (150); and in oil and in ethylene glycol
10、at temperatures up to approximately 15OC (300F) I Insulating Material.- All insulating material ahal.1 be white ceramic free 3.1.2.2 Moisture Absorption.- The materials shail not absorb moisture in excess of 0.01 percent by weight. l 3.2 DeSiFPe- 3.2.1 Sises and Dimendone.- The 8iaes and dmensions s
11、hall be as shown on Draw- ing ANU64* 3 *3 Interchangeability.- Al1 parts having the same manufacturer18 part number Changes in manufacturers part numbers shall be governed by the shall te directly and completely interchangeable with each other with respect to installa- tion and performance, drawing
12、number requirements of Specification MIL-D.5028. speoified in Section 4 when subjected to the tests headed a8 follower 3.4 Performance ,- The terminal sleeves shall satisfy the pePfarmeti6e requirements (a) Transverse Load (b) Dielectric Strength (c) Arc Resistance (d Quenching (e mdurance I 3.5 Ide
13、ntification of ,Product.- (-. . 35.1 Each sleeve ehdl be aleaily and pemanently idet The portion of the sleeve between the electrodes shall be a uniform cylinder. of 60 cycles per second shall be applied in the sequence of steps show in table II until failure occurs. ducting, at which time the arc i
14、n air disappears and a bright Une appears on the surface of the sleeve between the electrodes, TABLE II Current Application A1t.ernating current at a commercial frequency Failyre occurs when the surface of the material under test becomee con- I Approximatt- - Heat Genera uon I (wnttul Current Time C
15、ycle I (ma) Y naw uf Total Test Time . .-IA I - -t (sec) 10 l/4 on 3/4 off 6 120 10 114 on lous re- jection and the action taken to correct the defects found in the o.ginal shall be -shed the Ins ector. approvay of the Procuring Service, Terminal sleeves which have been I Units rejected after reteat
16、 shall not be resubinitted without the apecifio 4 I Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-“ MIL-S-5LI58A 27 9 777770b OLA4673 5 Y HETAL CONTAmR TERMiNAL SLEEVE l/W THICK OL RESISTAN RUBBER INSULhTCR 3/32 DUmTEZ OUTER CIRCULAR SPRNfl TYPE 3/
17、32“ DIAMETE% INNER CIRCULAR SPRINO TYPE IEISLATiN OIL BAT , Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-m L-S-545 8A 5 PREPARATION FR DFLIVERY (April 1951) 5.2 AppJ.ication*- The preservation, packaghg, pficking, and marking requirements specifie
18、d herein apply only to direct purchases by or direct shipments to the Government. 5.2 Preservation.- Unit packages shall be protected from cob-osion or deteriora- tion during shipment and storage in accordance with Specification AN-P-13, mothod lA, with- out preservation. 5.3 Packaging.- 5.3.1 Unit
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