NAVY MIL-T-46691 B-1993 THRUSTER CARTRIDGE ACTUATED M16 METAL PARTS ASSEMBLY《M16金属零件集合发动弹药筒推进器》.pdf

《NAVY MIL-T-46691 B-1993 THRUSTER CARTRIDGE ACTUATED M16 METAL PARTS ASSEMBLY《M16金属零件集合发动弹药筒推进器》.pdf》由会员分享，可在线阅读，更多相关《NAVY MIL-T-46691 B-1993 THRUSTER CARTRIDGE ACTUATED M16 METAL PARTS ASSEMBLY《M16金属零件集合发动弹药筒推进器》.pdf（17页珍藏版）》请在麦多课文档分享上搜索。

1、 INCH-POUND 1 MIL-T-4669 1B 12 April 1993 SUPERSEDING 10 January 1969 MIL-T-4669 1 A MILITARY SPECIFICATION THRUSTER, CARTRIDGE ACTUATED, Ml6 METAL PARTS ASSEMBLY his specifcation is approved for use by all Depaments and Agencies of the Deparnent of Defense. 1. SCOPE 1.1 Scope. This specification co

2、vers the requirements for the M16 Cartridge Actuated Thruster Metal Parts Assembly (see 6.1). 2. APPLICABLE DOCUMENTS 2.1 Government documents. 2.1.1 Specifications and standards. The following specifications and standards form a part of this document to the extent specified herein. Unless otherwise

3、 specified, the issues of these documents are those listed in the issue of the Department of Defense Index of Specifications and Standards (DODISS) and supplements thereto, cited in the solicitation (see 6.2). 0 SPECIFICATIONS MILITARY MIL-A-2550 Ammunition, General Specification For STANDARDS MILIT

4、ARY MIL-STD- 105 MIL-STD- 109 MIL-STD-4 13 Sampling Procedures And Tables For Inspection By Attributes Quality Assurance Terms And Definitions Visual Inspection Guide for Elastomeric O-rings Beneficial comments (recommendations, additions, deletions) and any pertinent tiaia which may be of use in im

5、proving this document should be addresse to: Coder, Mian Head Division, Naval Surface Warfare Center, Standardization Branch (Code 8420), 101 Strauss Avenue, Indian Head, MD 20640-5035, by using the Sadardization Document improvement Proposai (DD Form 1426) appearing at the end of this document or b

6、y sending a letter. AMSC NIA FSC 1377 DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited. O Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-YbbSLB 999SOb LSYSb4 TTO MIL-T-4669 1 B (Unless otherwise indicated, copie

7、s of federal and military specifications and standards are available from Standardization Documents Order Desk, Bldg. 4D, 700 Robbins Avenue, Philadelphia, PA 191 11-5094.) 2.1.2 Other Government documents, drawings, and publications. The following Government drawings form a part of this specificati

8、on to the extent specified herein. Unless otherwise specified, the issues are those cited in the solicitation (see 6.2). DRAWINGS Naval Surface Warfare Center, Indian Head Division (CAGE Codes 19200 and 19203) 1052 1322 8845243 8845244 92 17557 U.S. Air Force TPO 00-849-02 14 Thruster, Cartridge Act

9、uated, M16 Metal Parts Assembly Box, Packing, Ammunition, For Thruster, Cartridge Actuated, M16 Box, Fiberboard (inner), Packing, Ammunition, For Thruster, Cartridge Actuated, M16 Box, Fiberboard (Outer), Alternative, Packing Ammunition, for Thruster, Cartridge Actuated, M16 Thruster, Cartridge Actu

10、ated, M16 (Application for copies should be addressed to: Commander, Indian Head Division, Naval Surface Warfare Center, Data Control Branch (Code 8410), Indian Head, MD 20640-5035.) 2.2 Order of precedence. In the event of a conflict between the text of this document and the references cited herein

11、, 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 3.1 First article. When specified in the contract or purchase order (see 6.2), a sample shall be subjected to the

12、 first article inspection (see 4.3 and 6.3). 3.2 Materials. All materials used in the manufacture of the thrusters 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 d

13、esign activity prior to manufacture. When alternate materials or methods of manufacture are specified on the drawings, the bidders selections shall be clearly stated in the proposal. 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-nIL-T-4bb9LB m 99

14、9990b L495b5 937 m MIL-Ta9 1 B 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 intended for use in manufacture. 3.3 Hardness and other physical proper

15、ties. 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 pressure. The cylinder and head shall withstand a hydrostatic pr

16、essure of 10,OOO pounds per square inch (psi) for 15 seconds, minimum, without leaking, deformation, or mechanical failure (see 6.4.1). 3.5 Shear pin strength. The shear pin, after application of protective finish, shall shear when a load of 41 f 5 pounds is applied at the steady rate of 0.125 inch

17、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 and the following. 3.6.1 Fluid leakage. The thruster subassembly (less head, cartridge retainer, and spring) shall show no evidence of fluid lea

18、kage after a minimum of 16 hours, when kept in a vertical position with the open end of the cylinder pointing down. 3.6.2 Head and cylinder. The head and cylinder shall be assembled with a sufficient torque to lightly bottom components. 3.6.3 Presence of piston, shear pin. Upon completion of assembl

19、y, a load of 20 i- 2 pounds shall be applied to the locking pin to determine if the shear pin is properly engaged. 3.7 Protective finish. Protective finish shall be in accordance with the applicable specifications and shall apply to all surfaces of the component regardless of contour configuration.

20、3.8 Residual magnetism. The metal parts assembly shall not deflect the indicator of the compass more than five degrees in either direction using procedures in 4.6.7. 3.9 Workmanship. Thrusters shall be free of cracks, splits, or other defects which might prevent proper mating with connecting parts o

21、r proper functioning of the device. 3.9.1 Metal defects. All components shall be free from cracks, splits, cold shuts, inclusions, porosity, 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 per

22、sonnel handling the item. 3.9.3 Foreign matter. No part or assembly shall contain chips, dirt, grease, rust, corrosion, or other foreign matter. 3 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-L MIL-T-4bbSLB 999999b 19495bb 873 MIL-T-4669 1B 4. QUA

23、LITY ASSURANCE PROVISIONS 4.1. Responsibility for inspection. Unless otherwise specified in the contract or purchase order, the contractor is responsible for the performance of all inspection requirements (examinations and tests) as specified herein. Except as otherwise specified in the contract or

24、purchase order, the contractor may use his own or any other facilities suitable for the performance of the inspection requirements specified herein, unless disapproved by the Government. The Government reserves the right to perform any of the inspections set forth in this specification where such in

25、spections are deemed necessary to ensure supplies and services conform to prescribed requirements (see 6.2). 4.1.1 Responsibility for compliance. All items shall meet all requirements of sections 3 and 5. The inspection set forth in this specification shall become a part of the contractor?s overall

26、inspection system or quality program. The absence of any inspection requirements in the specification shall not relieve the contractor of the responsibility of ensuring that all products or supplies submitted to the Government for acceptance comply with all requirements of the contract. Sampling ins

27、pection, as part of manufacturing operations, is an acceptable practice to ascertain conformance to requirements; however, this does not authorize submission of known defective material, either indicated or actual, nor does it commit the Government to acceptance of defective material. 4.1.2 Quality

28、assurance terms and definitions. Reference shall be made to MIL-STD-109 to define the quality assurance terms used. 4.1.3 Inspections. Inspections shall be in accordance with MIL-A-2550. 4.2 Classification of inspections. The inspection requirements specified herein are classified as follows: a. Fir

29、st article inspection (see 4.4) b. Quality conformance inspection (see 4.5) 4.3 Inspection conditions. Unless otherwise specified (see 6.2), all inspections shall be performed under the following conditions: a. Temperature: room ambient (68 to 77F) b. Altitude: sea level c. Humidity: 50 percent rela

30、tive, maximum d. Atmospheric pressure: 14.7 psi 4.4 Rrst article inspection. At the beginning of regular production, the contractor 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 unasse

31、mbled parts, one set of unassembled parts without plating or final protective finish, and fifty shear pins from the same lot of shear 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

32、production. All parts and materials, including packaging and packing, must be the same as will be used for regular production and shall be obtained from the same source of 4 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-4bbLB m 999990b 194956

33、7 70T m MIL-T-4669 1B supply. After inspection and provisional acceptance at source, the first article sample shall be inspected O for all requirements of the drawings and specifications. The Government reserves the right to require new first article samples until an acceptable sample is submitted (

34、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 MIL-STD-105. 4.5.1.2 Size of lot. The production lot size shall be as specified in the cont

35、ract. 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 visual examinat

36、ion 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 acceptability. All nonconf

37、orming material shall be rejected. 4.5.2.1 Pin, Firing, Drawing 8596416, covering a detail of Drawing 10521322. Critical None defined Major 101 102 103 104 105 106 107 108 109 110 111 112 113 114 115 116 Concentricity of groove with body Concentricity of striker with body True position of pin hole D

38、iameter of body, min Diameter of groove Diameter of striker Diameter of pin hole, max Length of striker, min Profile of striker Profile of groove Metal defective Protective finish inadequate or defective Surface finish of body improper Surface finish of striker improper Foreign matter Burr or sharp

39、corners Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Visual Visual Visual Visual Visual Visual 5 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Minor 201 202 203 204 205 206 207 208 209 210 21 1 212 213 MIL-T-4669 1B Diameter of body, rnax Diam

40、eter of pin hole, min Total length Length of striker, rnax Location of pin hole Depth of slot in base Width of slot in base Width of groove Location of groove Location of slot in base Marking missing, incorrect, or illegible Radii incorrect Surface finish improper, except as otherwise classified Gag

41、e Gage Gage Gage Gage Gage Gage Gage Gage Gage Visual Gage Visual 4.5.2.2 Piston, Floating, Drawing 11596417, covering a detail of Drawing 10521322. Critical None defined Major 101 102 103 104 1 05 106 107 108 109 110 111 112 Minor 201 202 203 204 205 206 207 208 209 2 10 21 1 212 Concentricity of g

42、roove with body Pitch diameter of thread, max Major diameter of thread, max Diameter of groove Diameter of body, min Length of effective thread, min Profile of groove Metal defective Protective finish inadequate or defective Thickness Burr or sharp corner Foreign matter Pitch diameter of thread, min

43、 Diameter of body, rnax Diameter of hole through body Diameter of wrench holes Depth of wrench holes Radii or chamfer incorrect Width of groove Depth of threaded cavity Location of wrench holes Location of groove Marking missing, incorrect, or illegible Surface finish improper Gage Gage Gage Gage Ga

44、ge Gage Gage Visual Visual Gage Visual Visual Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Visual Visual 6 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-QbbIB W 9Ob L495b 582 D MIL-T-4669 1B 4.5.2.3 Piston, Drawing 8596418, covering a de

45、tail of Drawing 10521322. Critical None defined O Major 101 102 103 104 1 o5 106 107 108 109 110 111 112 113 114 115 116 117 Minor 20 1 202 203 204 205 206 207 208 209 210 21 1 2 12 213 214 215 216 217 Concentricity of pitch diameter of thread with body Concentricity of head with body Concentricity

46、of groove with head Pitch diameter of thread, max Minor diameter of thread, max Diameter of head, min Diameter of body, min Diameter of groove Length of effective thread, min Width across slot, min Width of slot Profile of groove Metal defective Protective finish inadequate or defective Surface fini

47、sh of body improper Burr or sharp corner Foreign matter Pitch diameter of thread, min Diameter of undercut, min, if applicable Diameter of head, max Diameter of body, max Diameter of hole through head Depth of threaded cavity, max Total length Length of head Width of groove Width across slot, max Lo

48、cation of slot Location of hole through head Width of undercut, max, if applicable Location of groove Marking missing, incorrect, or illegible Radius or chamfer incorrect Surface finish improper, except as otherwise classified Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Visual Visual

49、 Visual Visual Visual Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Gage Visual Gage Visual 4.5.2.4 Pin, Shear, Drawing 8596419, covering a detail of Drawing 10521322. Critical None defined 7 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-4bbSLB 9999906 I1949570 2T4 m MIL-T-4669 1B Major 101 Diameter, max Gage 102 Total length, min Gage 103 Metal defective V