NAVY MIL-DTL-60519 B-2000 INITIATOR CARTRIDGE ACTUATED M53 METAL PARTS ASSEMBLY《M53型金属零件装配 延时弹筒驱动引发器》.pdf

1、INCH-POUND MIL-DTL-605 19B 12 September 2000 SUPERSEDING MIL-1-605 19A 21 September 1992 DETAIL SPECIFICATION INITIATOR, CARTRIDGE ACTUATED, M53 METAL PARTS ASSEMBLY This specification is approved for use by all Departments and Agencies of the Department of Defense. 1. SCOPE 1.1 Scope. This specific

2、ation covers the requirements for the M53 Cartridge Actuated Initiator Metal Parts Assembly (see 6.1). 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 include documents cited in other sections of

3、 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 documents specified in sections 3 and 4 of this specification, whether o

4、r not they are listed. 2.2 Government documents. 2.2.1 Specifications and standards. The following specifications and standards form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are those listed in the Department of Defense Index o

5、f Specifications and Standards (DODISS) and supplement thereto, cited in the solicitation (see 6.2). SPECIFICATIONS DEPARTMENT OF DEFENSE MIL-A-2550 Ammunition, General Specification For Beneficid comments (rmmendctions, distribution is unlimited. Provided by IHSNot for ResaleNo reproduction or netw

6、orking permitted without license from IHS-,-,-MIL-DTL-605 19B STANDARDS DEPARTMENT OF DEFENSE MIL-STD-4 13 Visual Inspection Guide for Elastomeric O-rings (Unless otherwise indicated, copies of federal and military specifications and standards are available from Standardization Documents Order Desk,

7、 Bldg. 4D, 700 Robbins Avenue, Philadelphia, PA 191 11-5094.) 2.2.2 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 are tho

8、se cited in the solicitation. DRAWINGS NAVAL ORDNANCE STATION (CAGE Codes 19200 and 19203) 10520621 Initiator, Cartridge Actuated, M53 Metal Parts Assembly (Application for copies should be addressed to Commander, Naval Surface Warfare Center, Indian Head Division, 101 Strauss Avenue, Data Control B

9、ranch (Code 8410), Indian Head, MD 20640-5035.) 2.3 Non-Government publications and drawings. The following documents form a part of this document to the extent specified herein. Unless otherwise specified, the issues of the documents which are DOD adopted are those listed in the issue of the DODISS

10、 cited in solicitation. Unless otherwise specified, the issues of documents not listed in the DODISS are the issues of the documents cited in the solicitation (see 6.2). PUBLICATIONS AMERICAN SOCIETY FOR QUALITY CONTROL ASQC 21.4 Sampling Procedures and Tables for Inspection by Attributes ASQC A8402

11、 Quality Management and Quality Assurance Vocabulary (Appl icat ion for copies shoul d be addressed to the American Society for Qual it y Control, POBox 3005,611 E. Wisconsin Ave., Ml waukee, Wr53201-4606.) 2.4 Order of precedence. In the event of a conflict between the text of this document and the

12、 references cited herein (except for related associated specifications or specification sheets), the text of this document takes precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained. 3. REQUIREMENTS 2 Provided by IHSN

13、ot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-605 19B 3.1 First article. When specified in the contract or purchase order (see 6.2), a sample shall be subjected to the first article inspection (see 4.4 and 6.3). 3.2 Materials. All materials used in the man

14、ufacture of the initiators shall conform to the specifications referred to on the respective drawings unless specific approval in writing covering a departure therefrom has been obtained from the cognizant Navy design activity prior to manufacture. When alternate materials or methods of manufacture

15、are specified on the drawings, the bidders selections shall be clearly stated in the proposal. 3.2.1 Raw material. The contractor shall be responsible for selecting from the classification list contained in the raw material specification the surface and physical condition of the raw material intende

16、d for use in manufacture. 3.3 Hardness and other physical properties. Hardness and other physical properties required by the drawing shall be uniform throughout the part within specified tolerances. Requirements for all alloy steel parts shall be achieved by quenching and tempering. 3.4 Hydrostatic

17、pressure. The initiator chamber and cap shall withstand a hydrostatic pressure of 14,000 to 15,000 pounds per square inch (psi) for 15 seconds, minimum, without deformation or mechanical failure (see 6.4.1). 3.5 Shear pin strength. The shear pin, after application of protective finish, shall shear w

18、hen a load of 20 f 1 pounds is applied at the steady rate of 0.125 inch per minute. 3.6 Metal parts assembly. Parts shall be combined to produce an assembly which conforms to the requirements of the metal parts assembly drawing. All threaded joints shall be assembled handtight. 3.7 Protective finish

19、. Protective finish shall be in accordance with the applicable specifications and shall apply to all surfaces of the component regardless of contour configuration. 3.8 Residual magnetism. The metal parts assembly shall not deflect the indicator of the compass more than five degrees in either directi

20、on using procedures in 4.6.5. 3.9 Workmanship. Initiators shall be free of cracks, splits, or other defects which might prevent proper mating with connecting parts or proper functioning of the device. 3.9.1. Metal defects. All components shall be free from cracks, splits, cold shuts, inclusions, por

21、osity, or any similar defect. 3.9.2 Burr. No part shall have a burr which might interfere with the assembly or function of the item or which might be injurious to personnel handling the item. 3.9.3 Foreign matter. No part or assembly shall contain chips, dirt, grease, rust, corrosion, or other forei

22、gn matter. 4. QUALITY ASSURANCE PROVISIONS 3 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-605 19B 4.1 Classification of inspections. The inspection requirements specified herein are classified as follows: a. First article inspection (see 4

23、.2) b. Conformance inspection (see 4.3). 4.1.2 Quality assurance terms and definitions. Reference shall be made to ASQC A804 to define the quality assurance terms used. 4.1.3 Inspections. Inspections shall be in accordance with MIL-A-2550. 4.1.4 Inspection conditions. Unless otherwise specified (see

24、 6.2), all inspections shall be performed under the following conditions: a. Temperature: room ambient (68 to 77EF) b. Altitude: sea level c. Humidity: 50 percent relative, maximum d. Atmospheric pressure: 14.7 psi 4.2 First article inspection. At the beginning of regular production, the contractor

25、shall submit an initial production sample to a Government approved facility for evaluation. The sample shall consist of five metal parts assemblies, nine sets of unassembled parts, one set of unassembled parts without plating or final protective finish, and fifty shear pins from the same lot of shea

26、r pins tested by the contractor. The sample shall be manufactured in the same manner, using the same materials, equipment, processes, and procedures as used in regular production. All parts and materials, including packaging and packing, must be the same as will be used for regular production and sh

27、all be obtained from the same source of supply. After inspection and provisional acceptance at source, the first article sample shall be inspected for all requirements of the drawings and specifications. The Government reserves the right to require new first article samples until an acceptable sampl

28、e is submitted (see 6.3). 4.5 Quality conformance inspection. 4.5.1 Lot. 4.5.1.1 Submission of product. Unless otherwise specified by the contracting activity, formation and identification of lots shall be in accordance with ASQC 21.4. 4.5.1.2 Size of lot. The production lot size shall be as specifi

29、ed in the contract. 4.5.2 Examination. One hundred percent examination shall be performed for all critical defects. Examination for major and minor defects shall be performed on a defect basis in accordance with the classification of defects. Four power (4x) magnification may be used in performing v

30、isual examination for such defects as burr and foreign matter. Inspection for rubber O-rings shall be in accordance with MIL-STD-413. When compliance with the applicable requirement is in doubt as a result of visual examination, the characteristic shall be measured or gaged to determine acceptabilit

31、y. All nonconforming material shall be rejected. 4 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-605 19B 4.5.2.1 Chamber, Initiator, Drawing 10520407, covering a detail of Drawing 10520621. Characteristics Defect Critical None defined Major

32、 101 102 103 104 105 106 107 108 109 110 111 112 113 114 115 116 117 118 119 120 Minor 201 202 203 204 205 206 207 208 209 210 21 1 212 Pitch diameter of large external thread, min Major diameter of large external thread, min Pitch diameter of small external thread, min Major diameter of small exter

33、nal thread, min Pitch diameter of internal thread, max Minor diameter of internal thread, max Concentricity of datum location with pitch diameter of small external thread Concentricity of pitch diameter of large external thread with cavity Concentricity of large external thread pilot with large exte

34、rnal thread Concentricity of counterbore cavity, including perpendicularity with base of counterbore Diameter of counterbore Diameter of large thread pilot Depth of cavity Length to datum location Thickness of wall, min Metal defective Protective finish inadequate or defective Surface finish of cavi

35、ty and angle of gas port, improper Burr or sharp corner Foreign matter Pitch diameter of large external thread, rnax Pitch diameter of small external thread, rnax Pitch diameter of internal thread, min Diameter of small external thread relief Diameter of small external thread pilot Diameter of hole

36、in gas port Diameter of cavity Depth of counterbore Length of gas port Length of small thread relief Length from face of gas port to small thread Length of large external thread pilot Method of Inspection Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Visual Visual Visual

37、 Visual Visual Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage 5 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-605 19B Thickness of wall, rnax Depth of threaded hole Diameter of chamfer at internal thread Total length Length of

38、large external thread Marking missing, incorrect, or illegible Radius or chamfer missing or incorrect Surface finish improper, except as otherwise classified 213 214 215 216 217 218 219 220 Gage Measure Measure Measure Measure Visual Visual Visual 4.5.2.2 Cap, Initiator, Drawing 10520473, covering a

39、 detail of Drawing 10520621. Critical 1 Major 101 102 103 104 105 106 107 108 109 110 111 112 113 114 115 116 117 118 119 120 121 122 123 124 125 126 127 128 129 Surface finish of cavity Pitch diameter of large internal thread, rnax Minor diameter of large internal thread, max Pitch diameter of smal

40、l internal thread, ma Minor diameter of small internal thread, max Pitch diameter of external thread, min Major diameter of external thread, min Pitch diameter of pin hole thread, max Minor diameter of pin bole thread, max Concentricity of striker hole with small cavity Concentricity of large intern

41、al thread undercut with large thread Concentricity of cartridge head recess with large internal thread Concentricity of large internal thread with small cavity Concentricity of chamfer at striker hole with small cavity Concentricity of small internal thread with small cavity Symmetry of pin hole wit

42、h small cavity Symmetry of flats with pitch diameter of thread at small end Diameter of small cavity Diameter of large thread undercut Diameter of boss, min Diameter of striker hole, min Diameter of pin hole, max Diameter of cartridge head recess Diameter of counterbore at small thread cavity Diamet

43、er of mouth at small thread cavity Depth of cartridge head recess Depth to bottom of counterbore, small threaded end, max Depth of cartridge head recess, including chamfer Length of effective exterior thread, min Length of end of effective exterior thread, max Gage Gage Gage Gage Gage Gage Gage Gage

44、 Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage 6 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-605 19B Length of effective small interior thread, min Thickness of boss, min Loc

45、ation of pin hole Chamfer at striker hole missing or incorrect Metal defective Protective finish inadequate or defective Surface finish of cavity counterbore and mouth improper Burr or sharp corner Foreign matter 130 i31 132 133 134 13s 136 137 i38 Minor 201 202 203 204 20s 206 207 208 209 210 21 1

46、212 213 214 21s 216 217 218 219 220 221 222 223 Pitch diameter of large internal thread, min Pitch diameter of small internal thread, min Pitch diameter of external thread, max Pitch diameter of pin hole thread, min Pitch diameter of setscrew thread Minor diameter of setscrew thread, max Diameter of

47、 boss, max Diameter of striker hole, max Diameter of pin hole, min Diameter of body, large end Depth to bottom of counterbore, small threaded end, min Depth of small threaded cavity, including chamfer, max Depth of large cavity, including undercut Total length Length of body, large end Length from f

48、ace of large cavity to shoulder Length of flat Width across flat Width of large thread undercut Thickness of boss, max Location of setscrew hole Radius or chamfer missing or incorrect Surface finish improper, except as otherwise classified 4.5.2.3 Pin, Shear, Drawing Critical None defined Major 101

49、102 103 104 10s 0520622, covering a detail of Drawing Diameter, max Total length, min Metal defective Protective finish inadequate or defective Surface finish improper Gage Gage Gage Visual Visual Visual Visual Visual Visual Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Visual Visual Visual 0520621. Gage Gage Visual Visual Visual 7 Provided by IHSNot for ResaleNo reproduction or networking permitted without license