NAVY MIL-V-23219-1962 VALVE MANIFOLDS HIGH PRESSURE AIR REDUCING《高压空气减少阀组》.pdf
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1、i - . , . . . . . . . . . . . . . . . ._. , , . . . . . . . . . . . . . . . . . . ._ * MILITARY SPECIFICATION . VALVE MANIFOLDS,. HIGH PRESSURE AIR REDUCING , ._ .r - . :. . . : * . R .* _- -_ -:-i 1. SCOPE 1.1 Scope. - This specification cbvcrs thc de- sign, construction, test and operating require
2、ments for high pressure air reducing valve manifolds for the ASROC launcher. MIL-P-15137 -,Provisioning Teclmica) . Parts for Electrical and Mechanical Equipment (Haval Shipboard Use). . Documentation for Repair 1.2 Classification. - Manifo!ds shall be of the following classes,. as specified (see 6.
3、1): Class I - 4500/100 pounds per square inch gage ,psig) manifoid., Class I - 4500/300 psig manifold. STANDARDS . *. MILITARY ML-STD-130 - Identification Marking of U. S. Military Property, . AIL-STD-167 - Mechanical Yibrations of . Shipboard Equipment. 5 i, .- .,- . Class I and class II manifolds
4、differ only in capacity dferentiation will be made only in the capacity, specification. WOG IPS. DRA WINGS and the type of reducing valve employed; Lerefore, regulator and end connection requirements of this BUREAU OF SHIPS 810-1385884 - Union Fittings 6000 PSI .- r: . 2. APPLICABLE DOCUMENTS (Copie
5、s of specifications, standards, drawings, f 2.1 The following documents of the issue in ef- and publications required by contractors in connec- tion witli specific procurement functions should be . obtained from the procuring activity or as directed by the contracting officer.) fect on date of invit
6、ation for bids, orm a part of this specification to the extent spccificd herein. . -: . 4- .1 SPECIFICATIONS 3 REQUIREMENTS MILITARY MIL-P-116 - Preservation, Methods of, MIL-S-901 - Shockproof Equipment, Class HI (High-Impact) Shiphoard Application, Tests for. MIL-D-963 - Drawings, Electrical, Hull
7、 aiid Mechanical Equipment for Naval Shipboard Use. MIL-E-5272 - Environnieiit:il Testing, Acroii;iutic;il aiid Associ- ated Equipiiiciit, Ciericral. Specification for. MIL-$7742 - Screw Threads, Standard, Optimum Selected Series: Gcncrul Specification for. MIL-P-I5024 - Plates. Identification - 1ii
8、orm;ition and Marking for Idwitification of Elec- trical, Electronic nnd Mcchunical Equipment. MIL-M-15071 - hlunual, Scrvicc (Iiistruc- - tion ookj for +hipiward . . Elcr*ti.icnl aiid Mcchanic;il Equ i pni mit. / 3.1 ciencrai _ requirements. -. 3 1.1 Dcs$+-jo, evaluation of the equipment for subjec
9、t application. . . 3.1.3 . durability, strength and quietness. Space, weight structiori of the m:inifoltl shall II o the best coni,-,:. K ,.i . . _. -. -. - . ! L Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-V-23219(SHIPS) Table I - Regulation
10、 lockup .conditions (nominal) . . pressure range i I. : (psi) . . I ,. 1- 4500 1500 . -15. 4500 1500 - . 300. -15 + 3.1.3.1 Dissimilar metals. - Unless suitably , protected against electrolytic corrosion, dissimilar metals shall not be used in dirept contact with each other. same manufacturers part
11、number shall be directly interchangeable with each other with respect to in- stallation and performance. 3.1.5. Safety wiring. - Accidental loosening of all threaded parts shall be prevented by safety wir- ing, self-locking bolts and nuts, and other approved methods. 3.1.6. Threads,- All threads sha
12、ll conform to MIL- S- 7742. *. 3.1.7. Mounting, - The body of the manifold ahall be designed for permanent installation in the ships pneumatic system. All of the individual com- ponents used in the manifold assembly shall be eas- ily accessible for service or removal from the mani- fold. 3.1.8 Ident
13、ification plates and markings. - Iden- tification plates and markings shall be furnished in accordance with Ma-P-15024 and MIL-STD-130. In addition, the manifold shall have an identification plate which shows the schematic diagram of the manifold and detailed itrstructions for its use. 3.1.4. interc
14、hangeability. - All parts having the 3.1.9 Environmental conditions, - Manifold per- formance shall not be adversely affected by varying ambient conditions within the following limits: (a) Temperature - 28F to 125OF (b) Pressure - 30 inches 2 6 inches Hg. (c) Salt spray - Exposure to atmosphere con-
15、 taining salt laden moisture, to meet the applicable E- qiremenls of Ma-%-5272. (d) Vibration ,. To meet vibration test rer,uire- ment6 for type I o hlL-STD- 167. . .- 2 * I _i; ., I . c: -. !:;:;, . ,_ . . , . . . . . . (e) Shock - h1;inifoldshall meet high shock impact requirements as defined . sa
16、tisfactorily passes the shock I test, it shall be repaired in ac- . cordance with the applicable para- graph for disposition of shock , tested equipment as specified in MIL-S-901 and offered for accept- ;, ance as a production unit. , - . in MIL-S-901. II the manifold . . *. . , . . I 1: : : .: I“.
17、. . I - . -.- . . . . .-.- -.-. . - . . “I -1-1.1 -. . . “ - - -. . .-. - . . . . . . _- . - ._._. -_ _-_-_ ._-.- _- . . .-_. . . -.-.- . . . “ ._-_ .+. -. -.- . . . . . . . - ,- . . 3. 1. 10 Noise level, - Design, construction and-. . . ,- . , workmanship shall be such that minimum practical noise
18、level will result under all operating conditions . . i. .- . . -. . .- . . , specifled herein. 3.2 Detail requirements. -+ 3: 2,l Design and test pressures. - Design and test pressures o the manifold shall be as shown in table II. 3.2.2 - Manifold-ports for classes I and II shall be equipped with 60
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