ImageVerifierCode 换一换
格式:PDF , 页数:21 ,大小:692.22KB ,
资源ID:981425      下载积分:10000 积分
快捷下载
登录下载
邮箱/手机:
温馨提示:
如需开发票,请勿充值!快捷下载时,用户名和密码都是您填写的邮箱或者手机号,方便查询和重复下载(系统自动生成)。
如填写123,账号就是123,密码也是123。
特别说明:
请自助下载,系统不会自动发送文件的哦; 如果您已付费,想二次下载,请登录后访问:我的下载记录
支付方式: 支付宝扫码支付 微信扫码支付   
注意:如需开发票,请勿充值!
验证码:   换一换

加入VIP,免费下载
 

温馨提示:由于个人手机设置不同,如果发现不能下载,请复制以下地址【http://www.mydoc123.com/d-981425.html】到电脑端继续下载(重复下载不扣费)。

已注册用户请登录:
账号:
密码:
验证码:   换一换
  忘记密码?
三方登录: 微信登录  

下载须知

1: 本站所有资源如无特殊说明,都需要本地电脑安装OFFICE2007和PDF阅读器。
2: 试题试卷类文档,如果标题没有明确说明有答案则都视为没有答案,请知晓。
3: 文件的所有权益归上传用户所有。
4. 未经权益所有人同意不得将文件中的内容挪作商业或盈利用途。
5. 本站仅提供交流平台,并不能对任何下载内容负责。
6. 下载文件中如有侵权或不适当内容,请与我们联系,我们立即纠正。
7. 本站不保证下载资源的准确性、安全性和完整性, 同时也不承担用户因使用这些下载资源对自己和他人造成任何形式的伤害或损失。

版权提示 | 免责声明

本文(NAVY MIL-R-82879-1993 REMOVER CARTRIDGE ACTUATED RAU-3 A ASSEMBLY《RAU-3 A火药驱动装配清洗剂》.pdf)为本站会员(ownview251)主动上传,麦多课文库仅提供信息存储空间,仅对用户上传内容的表现方式做保护处理,对上载内容本身不做任何修改或编辑。 若此文所含内容侵犯了您的版权或隐私,请立即通知麦多课文库(发送邮件至master@mydoc123.com或直接QQ联系客服),我们立即给予删除!

NAVY MIL-R-82879-1993 REMOVER CARTRIDGE ACTUATED RAU-3 A ASSEMBLY《RAU-3 A火药驱动装配清洗剂》.pdf

1、a MIL-R-82879 = 9999906 1970368 363 I INCH-POUND I 20 December 1993 MIL-R-82879 MILITARY SPECIFICATION REMOVER, CARTRIDGE ACTUATED, RAU-3/A ASSEMBLY is specifcation is approved for use by all Departments and Agencies of the Deparment of Defense. 1. SCOPE 1.1 Scope. This specification covers the requ

2、irements for the RAU-3/A Cartridge Actuated Remover Assembly (see 6-11. 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 specified, the issues

3、 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). SPECIFICATIONS MILITARY MIL-A-2550 MIL-C-554 1 MIL-R-82689 Ammunition, General Specification For Chemical Films

4、and Chemical Film Material for Aluminum and Aluminum Alloys Release, Firing Pin, Gas Actuated, M1A1 STANDARDS MILITARY MIL-STD-105 Sampling Procedures And Tables For Inspection By Attributes MIL-STD-109 Oualitv Assurance Terms And Definitions Beneficial comments (recommendations, additions, deletion

5、s) and any pertinent data which may be of use in improving this document should be addressed to: Coder, Indian Head Division, Naval Surface Warfare Center, Standardization Branch (Code 8420), 101 Strauss Avenue, Indian Head, MD 20640-5035, by using the Standardizat ion Document Improvement Proposal

6、D Form 1426) appearing at the end of this document or by sending a letter. AMSC N/A FSC 1377 DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-R-82879 99999Ob L9703b

7、2TT MIL-R-82879 MIL-STD-413 Visual Inspection Guide for Elastomeric O-Rings MIL-STD-453 Inspection, Radiographic MIL-STD-1168 Ammunition Lot Numbering MS28741-4 Hose Assembly, Detachable End Fitting, Medium Pressure (Unless otherwise indicated, copies of federal and military specifications and stand

8、ards 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 specification to the extent specified herein. Unless otherwis

9、e specified, the issues are those cited in the solicitation (see 6.2). DRAWINGS Indian Head Division, Naval Surface Warfare Center (CAGE Codes 19200, 19203, and 53711) DL5 184966 MIA1 Firing Pin Release DL6783541 Remover, Cartridge Actuated, RAU-3A Assembly DL8593625 Cartridge, Impulse, M29A2 Assemb

10、ly U.S. Air Force SPI 01-364-3955 Remover, Cartridge Actuated RAU-3/A (Application for copies should be addressed to: Commander, Indian Head Division, Naval Surface Warfare Center, 101 Strauss Avenue, Data Control Branch (Code 8410), Indian Head, MD 20640-5035.) 2.2 Order of precedence. In the event

11、 of a conflict between the text of this document and the references cited herein, 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

12、 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 manufacture of the removers and release mechanisms shall conform to the specifications referred to on the respective drawings unless s

13、pecific 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 are specified on the drawings, the bidders selections shall be clearly stated in the proposal. 2 Provided by I

14、HSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-R-82879 9999906 I1970370 TLL Seating or bottoming, I Run-ON, min (inch pounds) I including A (inch pounds) Components MIL-R-82879 3.2.1 Raw material. The contractor shall be responsible for selecting from the cl

15、assification list contained in the raw material specification the surface and physical condition of the raw material intended for use in manufacture. Breakaway, min (inch pounds) 3.3 Hardness and other physical properties. Hardness and other physical properties required by the drawing shall be unifo

16、rm throughout the part within specified tolerances. Requirements for all alloy steel parts shall be achieved by quenching and tempering. Firing head and inside tube with cartridge installed 3.4 Components. 10 400 + 50 300 3.4.1 Primary components. For the purpose of this specification the M29A2 Impu

17、lse Cartridge (Drawing 8593625) and the MIA1 Release (Drawing 5184966) are defined as primary components. Only primary components from a single lot shall be used in a production lot of removers; however, one primary component production lot may be used in more than one remover production lot. 3.4.2

18、Component parts. The M1A1 Release shall meet the requirements of MIL-R-82689 and the following: 3.4.2.1 Hydrostatic pressure. The components listed in table I shall withstand a constant internal pressure, as indicated, for 15 seconds minimum, without application of any external load and shall show n

19、o evidence of leakage or mechanical failure (see 6.5.1). TABLE I. Hvdrostatic Dressure reauirements. II Hydrostatic pressure I (psi, minimum) II Outside tube I 2900 II II Telescoping tube I 2000 II II Inside tube I 2500 II 3.4.2.2 Torque. Torque requirements shall be as specified in tables II and II

20、I. No loosening or deformation shall occur upon application of the breakaway torque. 3.4.2.2.1 Assembly torque. Torque requirements shall be as specified in table II. No movement shall occur upon application of the breakaway torque. TABLE II. Toraue reauirements for assemblv. A B C 3 Provided by IHS

21、Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-R-82877 W 7777906 l197037L 958 A Run-ON, min (inch pounds) 75 min 75 min - MIL-R-82879 3.4.2.2.2 Component torque. ?orque requirements shall be as specified in table III. No loosening or deformation shall occur up

22、on application of the breakaway torque. TABLE III. Toraue reauirements for comuonents. B C Seating or bottoming, including A (inch pounds) Breakaway, min (inch pounds) 500 + 50 400 min - - - 300 min IrBise and outside tube Firing head and inside Stop telescoping tube I- and outside tube 3.4.2.3 Asse

23、mbly. The boss face surface of the firing head shall be in complete contact with the cartridge. 3.4.2.4 M1Al firing pin release. Each MIA1 used in the RAU-3A remover shall have met the icspection and test requirements of MIL-R-82689 and DL5184966 prior to installation and shall have been assembled w

24、ithin the past 6 months. 3.5 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 and includes interior surfaces. Special internal electrodes may be required to get the prop

25、er internal coating. 3.6 Residual magnetism. The metal parts assembly shall not deflect the indicator of the compass more than five degrees in either direction (see 4.5.3.5). 3.7 Radiographic examination. Each remover shall be radiographically examined for defects (see 4.6.2). 3.8 Functional. 3.8.1

26、Ballistics. Removers loaded with accepted M29A2 cartridges shall propel a 300-pound mass horizontally and shall comply with the requirements of table IV. 3.8.2 Initiation. The remover shall be fired by a source delivering an output pressure of 250 + 25, - O pounds per square inch gage Sig) at the en

27、d of 15 feet of aircraft hose, MS28741-4 at 70 f 5F. 3.8.3 Misfires. There shall be no misfires. 3.8.4 Mechanical failures. The remover shall function without mechanical failure (see 6.5.1). 4 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-. Tempera

28、ture (OF) - 60to - 70 65 to 75 195 to 205 MIL-R-82879 9999906 I1970372 89i.1 Velocity, min (fps) Thrust, min (pounds) Ignition delay, max (milliseconds) 17 1930 40 20 2745 40 24 3345 40 MIL-R-82879 TABLE IV. Ballistic reauirements. 3.9 Workmanship. Removers shall be free of cracks, splits, or other

29、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, porosity, or any similar defect. 3.9.2 Burr. No part shall have a burr which might interfere with the as

30、sembly 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 foreign matter. 4. QUALITY ASSURANCE PROVISIONS 4.1 Responsibility for inspection. Unless otherwise specif

31、ied 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 purchase order, the contractor may use his own or any other facilities suitable for t

32、he 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 inspections are deemed necessary to ensure supplies and services conform to prescribed

33、requirements (see 6.2). 4.1.1 Responsibility for compliance. Ail items shall meet all requirements of sections 3 and 5. The inspection set forth in this specification shall become a part of the contractors overall inspection system or quality program. The absence of any inspection requirements in th

34、e 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 inspection, as part of manufacturing operations, is an acceptable practice to ascertain c

35、onformance 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 assurance terms and definitions. Reference shall be made to MIL-STD-109 to define the

36、quality assurance terms used. 4.1.3 Inspections. Inspections shall be in accordance with MIL-A-2550. 5 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-R-82879 999990b 1970373 720 MIL-R-82879 4.2 Classification of inspections. The inspection requi

37、rements specified herein are classified as follows: a. First article inspection (see 4.4) b. Quality conformance inspection (see 4.5) c. Remanufacture program inspections (see 4.6) 4.3 Inspection conditions. Unless otherwise specified (see 6.2), all inspections shall be performed under the following

38、 conditions: a. b. Altitude: sea level c. d. Atmospheric pressure: 14.7 psi Temperature: room ambient (68 to 77F) Humidity: 50 percent relative, maximum 4.4 First article inspection. At the beginning of regular production, the contractor shall submit an initial production sample to a Government appr

39、oved facility for evaluation. The sample shall consist of five metal parts assemblies, nine sets of unassembled parts, and one set of unassembled parts without plating or final protective finish. The sample shall be manufactured in the same manner, using the same materials, equipment, processes, and

40、 procedures as used in regular production. All parts and materiais, including packaging and packing, must be the same as will be used for regular production and shall be obtained from the same source of supply. After inspection and provisional acceptance at source, the first article sample shall be

41、inspected 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 (see 6.3). - 4.5 Quality conformance inspection. 4.5.1 Lot. 4.5.1.1 Submission of product. Unless otherwise specified by t

42、he 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 contract. 4.5.2 Examination. One hundred percent examination shall be performed for all critical defects. Examination for m

43、ajor 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 examination for such defects as burr and foreign matter. Inspection for rubber O-rings shall be in accordance with MIL-STD-413.

44、 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 nonconforming material shall be rejected. 6 Provided by IHSNot for ResaleNo reproduction or networking permitted without licen

45、se from IHS-,-,-. MIL-R-82879 m 9999906 1970374 667 m MIL-R-82879 4.5.2.1 Cartridge, Aircraft Canopy Remover, M29A2, Drawing 8593625, covering a detail of Drawing 6783541. Characteristics Critical 1 2 3 4 5 Major 101 102 103 Minor 20 1 202 Defect Mixed cartridges Metal defective O-ring missing or im

46、properly secured Sealing disc missing or damaged Marking missing, incorrect, or illegible Cartridge discolored, dirty, oily, corroded, or stained Case dented O-ring split, cut, or cracked Case scratched, wrinkled, or bulged Varnish missing or inadequate Method of Inspection Visual Visual Visual Visu

47、al Visual Visual Visual Visual Visual Visual 4.5.2.2 Assembly, Drawing 6783541, less ali drawings except 8593729, 6783601, 6783542, 8593794, and AN 565DC1032H2. Critical None defined Major 101 Thread damaged Visual 102 Burr Visual 103 Foreign matter Visual Minor None defined 4.5.2.3 Assembly, Drawin

48、g 6783541, less Drawings 8593658, 8593734,8593786,8593787, and 8593791. Critical 1 2 Cartridge missing Visuai 3 Seal on inside tube missing Visual Boss face surface of firing head not in complete contact with Gage cartridge 7 Provided by IHSNot for ResaleNo reproduction or networking permitted witho

49、ut license from IHS-,-,-Major 101 102 MIL-R-82879 999990b 1970375 5T3 W MIL-R-82879 Burr Foreign matter Minor None defined 4.5.2.4 Assembly, Drawing 6783541, less Drawing 5184966. Critical 1 Tubes not free to slide Visual Visual Manual Major 10 1 Concentricity of body, large end, with datum location Gage Minor None defined 4.5.2.5 Assembly, Drawing 6783541. Critical 1 Improper assembly 2 Any part missing 3 Mixed removers 4 5 M1A1 fir

copyright@ 2008-2019 麦多课文库(www.mydoc123.com)网站版权所有
备案/许可证编号:苏ICP备17064731号-1