NAVY MIL-DTL-29576 B-2007 CYLINDERS STEEL COMPRESSED GAS NON-SHATTERABLE WELDED《装压缩气体的不易碎钢瓶》.pdf
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1、INCH-POUNDMIL-DTL-29576B 25 June 2007 SUPERSEDING MIL-C-29576A 2 September 1992DETAIL SPECIFICATION CYLINDERS, STEEL, COMPRESSED GAS, NON-SHATTERABLE, WELDED Reactivated after 25 June 2007 and may be used for new and existing designs and acquisitions. This specification is approved for use by all De
2、partments and Agencies of the Department of Defense. 1. SCOPE 1.1 Scope. This specification covers 1,800 psi (12,400 kPa) and 2,100 psi (14,500 kPa) (rated pressure) non-shatterable steel cylinders of welded construction. 1.2 Classification. Cylinders are of the following types and classes, as speci
3、fied by the applicable part number (see 6.2). 1.2.1 Types. Type A - Internal thread Type B - External thread 1.2.2 Classes. Class 1 - 1,800 psi (12,400 kPa) rated pressure Class 2 - 2,100 psi (14,500 kPa) rated pressure AMSC N/A FSC 8120 Comments, suggestions, or questions on this document should be
4、 addressed to: Commander, Naval Air Warfare Center Aircraft Division, Code 491000B120-3, Highway 547, Lakehurst, NJ 08733-5100 or emailed to thomas.omaranavy.mil. Since contact information can change, you may want to verify the currency of this address information using the ASSIST Online database at
5、 http:/assist.daps.dla.mil. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-29576B 2 2. APPLICABLE DOCUMENTS 2.1 General. The documents listed in this section are specified in sections 3 and 4 of this specification. This section does not incl
6、ude documents cited in other sections of this specification or recommended for additional information or as examples. While every effort has been made to ensure the completeness of this list, document users are cautioned that they must meet all specified requirements of documents cited in sections 3
7、 and 4 of this specification, whether or not they are listed. 2.2. Government documents. 2.2.1 Specifications, standards, and handbooks. The following specifications, standards and handbooks form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these
8、documents are those cited in the solicitation or contract. FEDERAL SPECIFICATIONS BB-A-1034 - Compressed Air, Breathing. (Inactive for New Design) TT-C-490 - Chemical Conversion Coatings and Pre-treatments for Ferrous Surfaces (Base for Organic Coatings) COMMERCIAL ITEM DESCRIPTIONS (CIDs) A-A-58092
9、 - Tape, Antiseize, Polytetrafluorethylene A-A-59503 - Nitrogen, Technical DEPARTMENT OF DEFENSE SPECIFICATIONS MIL-PRF-27210 - Oxygen, Aviators Breathing, Liquid and Gas MIL-M-43719 - Marking Materials and Markers, Adhesive, Elastomeric, Pigmented, General Specification for DEPARTMENT OF DEFENSE ST
10、ANDARDS MIL-STD-101 - Color Code for Pipelines and Compressed Gas Cylinders MIL-STD-130 - Identification Marking of U.S. Military Property Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-29576B 3 MIL-STD-810 - Environmental Engineering Consid
11、erations and Laboratory Tests MIL-STD-2219 - Fusion Welding for Aerospace Applications MS90389 - Cylinder, Oxygen, Non-Shatterable, Welded, 1800 PSI (Straight, U and Spiral Types). (Inactive for New Design) DEPARTMENT OF DEFENSE HANDBOOKS MIL-HDBK-1264 Radiographic Inspection for Soundness of Welds
12、in Steel by Comparison to Graded ASTM E 390 Reference Radiographs (Copies of these documents are available online at http:/assist.daps.dla.mil/quicksearch/ or http:/assist.daps.dla.mil/ or from the Standardization Document Order Desk, Building 4D, 700 Robbins Avenue, Philadelphia, PA 19111-5094.) 2.
13、2.2 Other Government documents, drawings, and publications. The following other Government documents, drawings, and publications form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are those cited in the solicitation or contract. DRA
14、WINGS NAVAL AIR SYSTEMS COMMAND 1684AS100 - Cylinder, Oxygen Non-Shatterable, Welded (1,800 psi) (Copies of the above drawing are available from the Naval Air Technical Data and Engineering Service Command (NATEC), P.O. Box 357031, NASNI, Bldg 90, San Diego, CA 92135-7031 or email to: nani_governmen
15、tdrawingsnavy.mil.) PUBLICATIONS Defense Standardization Manual SD-6 - Provisions Governing Qualification Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-29576B 4 (Copies of defense standardization manuals are available online at http:/assist
16、.daps.dla.mil/quicksearch/ or from the Standardization Document Order Desk, Building 4D, 700 Robbins Avenue, Philadelphia, PA 19111-5094.) 2.3 Non-Government publications. The following documents form a part of this document to the extent specified herein. Unless otherwise specified, the issues of t
17、hese documents are those cited in the solicitation or contract. AEROSPACE INDUSTRIES ASSOCIATION (AIA) NAS847 - Caps and Plugs, Protective, Dust and Moisture Seal (Copies of the above document are available online at http:/www.aia-aerospace.org/pubs/ or from the Aerospace Industries Association, 100
18、0 Wilson Blvd, Suite 1700, Arlington, VA 22209-3901.) AMERICAN SOCIETY FOR QUALITY (ASQ) ANSI/ASQ-Z1.4 - Sampling Procedures and Tables for Inspection by Attributes (Copies of the above document are available online at http:/www.asq.org/ or from the American Society for Quality, P.O. Box 3005, 600 N
19、orth Plankinton Avenue, Milwaukee, WI 53203.) AMERICAN SOCIETY FOR TESTING and no particles larger than 175 micrometers per 100 ml of solvent. 3.5.2.3 Halogen. When tested as specified in 4.6.2.3, there shall be no evidence of cleaning compound residue. 3.5.3 Leakage. When tested as specified in 4.6
20、.3, the cylinder shall not show any evidence of gas bubbles after 2 minutes of submergence. 3.5.4 Permanent volumetric expansion. When tested as specified in 4.6.4, the cylinder shall not have a permanent volumetric expansion greater than 10 percent of the total volumetric expansion. 3.5.5 Burst pre
21、ssure. When tested as specified in 4.6.5, class 1 cylinders shall not burst at a pressure less than 4,500 psi (31,030 kPa) and class 2 cylinders shall not burst at a pressure less than 5,250 psi (36,200 kPa). Failure of the cylinders shall occur in a ductile manner. 3.5.6 Endurance. When tested as s
22、pecified in 4.6.6, the cylinder shall not show any evidence of material failure. 3.5.7 Flattening. When tested as specified in 4.6.7, the cylinder shall not show any evidence of cracking when examined visually without magnification. 3.5.8 Macrostructure defects. When tested as specified in 4.6.8, th
23、e cylinder shall show no evidence of abnormal segregation, pipes, cracks, seams or abnormal change in structure from the surface to the center. 3.5.9 Radiographic inspection. When tested as specified in 4.6.9, welded sections of the cylinder shall be in accordance with MIL-HDBK-1264. 3.5.10 Fragment
24、ation resistance. 3.5.10.1 Procedure I. When tested as specified in 4.6.10.1, the cylinder shall remain in one piece. 3.5.10.2 Procedure II. When tested as specified in 4.6.10.2, the cylinder shall be allowed to separate into two pieces. The projected area of any piece shall be not less than 2.0 squ
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