DLA MIL-S-7393C-1968 STEEL ALLOY CARBURIZING BARS AND BILLETS STEEL NICKEL-CHROMIUM (3310 3316 AND 9310) AIRCRAFT QUALITY.pdf
《DLA MIL-S-7393C-1968 STEEL ALLOY CARBURIZING BARS AND BILLETS STEEL NICKEL-CHROMIUM (3310 3316 AND 9310) AIRCRAFT QUALITY.pdf》由会员分享,可在线阅读,更多相关《DLA MIL-S-7393C-1968 STEEL ALLOY CARBURIZING BARS AND BILLETS STEEL NICKEL-CHROMIUM (3310 3316 AND 9310) AIRCRAFT QUALITY.pdf(8页珍藏版)》请在麦多课文档分享上搜索。
1、MIL-S-7393C 28 August 1960 Superseding 20 December 1967 MIL-S-7393B MILITARY SPECIFICATION * STBEL ALLOY CARBURIZIN6, BARS AND BILLBTS, STGBL NICKEL-CHROMIUM (3310, 3316 and 9310), AIRCRAFT QUALITY lo scorn * 1.1 Scope.- This specification covers air melted nickel- chromium - molybdenum steels inten
2、ded for use in carburized aircraft parts o 1,2 Classification Q 1.2.1 Compositiono- The steel shall be furnished in three compositions, as specified (see 6,2): Composition I (3310) Composition II (3316) Composition III (9310) 1.2.2 Physical condition.- Products shall be furnished in one of the follo
3、wing physical conditions, as specified (see 6.2): * * (A) As forged (B) As rolled (C) Annealed (D) Normalized (E) Normalized and tempered 1.2,3 Surface conditions.- Products shall be furnished in one of the following surface conditions, as specified (see 6.2): (1) Black, as forged or rolled (2) Pick
4、led or blast cleaned (3) Rough turned (4) Cold or rolled or cold drawn (5) Turned, ground, and polkhed 2. APPLICABLE DOCUMENTS 2,l The following documents, of the issue in effect on date of invitation for bids or request for proposal, form a part of this specification to the extent specified herein.
5、 FSC 9510 Licensed by Information Handling ServicesProvided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-S-7393C SPEC IF ICATIONS Military * MIL-1-6868 STANDARDS Federal FED. STD, NO. 183 FBDo TEST METHOD STD. NO, 151 Military MIL-STD-163 MIL-STD-430 I
6、nspection Process, Magnetic Par ticle Continuous Identification Marking Metals; Test Methods of Iron and Steel Products Steel Mill Products, Preparation for Shipment and Storage Macrograph Standards for Steel Bars, Billets, and Blooms (Copies of specifications, standards, drawings, and publications
7、required by suppliers in connection with specific procurement functions should be obtained from the procuring activity or as directed by the contracting officer.) 2.2 Other publications.- The following documents form a part of this specification to the extent specified herein. Unless otherwise indic
8、ated, the issue in effect on date of invitation for bids or request for proposal shall apply. * Society of Automotive Engineers (Aerospace Material SpecificationsL AMs2301 Aircraft Quality Steel Cleanliness, Magnetic Particle AMs2251 Tolerances, Alloy Steel Bars AMs2640 Magnetic Particle Inspection
9、Inspection Procedure (Copies of SU publications may be obtained from the Society of Automotive Engineers, Inc., 485 Lexington Avenue, New York, New York 10017.) American Society for Testing and Materials ASTM E112 Bstimating.the Average Grain Size of Metals (Copies of ASTM publications may be obtain
10、ed from the American Society for Testing and Materials, 1916 Race Street, Philadelphia, Pennsylvania 19103. ) 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-S-7373C 75 W 777770b OLLL1765 3 W MIL-S-7393C 3. REQUIRBMBNTS * 3.1 Materials.- The st
11、eel shall be of aircraft quality and satisfactory for the fabrication of parts which may be subject to magnetic particle inspection. requirements of AMS2301. The material shall meet the cleanliness 3.1.1 Sufficient discard shall be taken from each ingot to insure freedom from piping and undue segreg
12、ation. 3.2 Chemical composition.- Chemical composition shall be as specified in table I. TAELS I. Chemical composition Check tolerance L/ Composition I Compos;ttion II Composition III analysis E1 emen t (percent ) (per cent ) (percent) Carbon Manganese * Sulfur * Phosphorous Si li con Nickel Chromiu
13、m Molybdenum * Copper * Iron 0.08 - 0.13 O045 - 0.60 0.025 (rnax.) 0.025 (max.) 0.20 - 0.35 3.25 - 3.75 1.25 - 1.75 - 0.35 (mu.) Remainder 0.14 - 0.19 0.45 - 0.60 0.025 (max.) 0.025 (rnax.) 0.20 - 0.35 3.25 - 4.00 1.25 - 1.75 .- - 0.35 (mu.) Remainder 0.07 - 0.13 0.40 0.70 0.025 (rnax.) 0.025 (mu.)
14、0.20 - 0.35 3.00.- 3.50 1-00 - 1.40 0.08 - 0.15 0.35 (mu.) Remainder *o. o1 f .O3 + .O05 + .O05 g .o2 f .o1 + .O7 L + .O5 + .O3 - i/ Individual determination may vary from the specified range to the extent shown in the check analysis column, except that elements in any heat shall not vary both above
15、 and below the specified range. For sizes over 100 square inches in cross sectional area, the check analysis shall be negotiated. 3.3 Grain size.- The austenitic grain size shall be predominantly No. 5, or finer, with grains as large as No. 3 permissible, in accordance with ASTM B112. * 3.4 Hardness
16、 limits for conditions (Cl, and (E).- * 3.4.1 nie hardness for material in physical conditions (C), and E shall be not more than Brinell 229 (Rockwell C-21) when furnished in surface condition (i), (2), or (3). 3.4.2 The hardness for material in physical conditions (C) and (E) shall be not more than
17、 Brinell 248 (Rockwell C-24) when furnished in surface condition (4). 3.5 Hardenability .- 3 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-S-7393C 3.5.1 shall be Rockwell C-43 maximum at 1/16 inch and Rockwell C-31 minimum at 6/16 inch. 3.5.2 s
18、hall be Rockwell C-47 maximum at 1/16 inch and Rockwell C-35 minimum at 8/16 inch. End-quench hardenability values for composition I steel End-quench hardenability values for composition II steel 3.5.3 End-quench hardenability values for composition III steel shall be Rockwe1.i C-41 maximum at 1/16
19、inch and Rockwell C-32 minimum at 6/16 inch. 3.6 Macrostructure.- Visual examination of deep acid etched specimens shall comply with MIL-STD-430 at levels S-2, R-1, and C-2. 3.7 Identification marking.- Each bar shall be identified in In lieu accordance with Fed. Std. No. 183. The markings shall inc
20、lude the heat number of the metal and the designation of the specification. of continuous marking, bars under 0.5 inch in diameter may be bundled and each bundle identified by metal tags impression stamped with the legend specified in Fed. Std. No. 183 and securely attached near each end of the bund
21、le. 3.8 Tolerances.- 3.8.1 Diameter or thickness.- The permissible variations in the dimensions of bar or billets shall be as shown in AMS2251, except that when bars are intended for reforging, the requirements of AMs2251 are waived. 3.9 Angles and corners.- The angles and corners of square, rectang
22、ular, and hexagonal bars shall be in accordance with best mill practice. 3.10 Workmanship.- Material shall be sound, of uniform quality and condition, free from pipe, and shall not contain laps, cracks, twists, seams, or other defects detrimental to the fabrication or performance of parts. 4. QUALIT
- 1.请仔细阅读文档,确保文档完整性,对于不预览、不比对内容而直接下载带来的问题本站不予受理。
- 2.下载的文档,不会出现我们的网址水印。
- 3、该文档所得收入(下载+内容+预览)归上传者、原创作者;如果您是本文档原作者,请点此认领!既往收益都归您。
下载文档到电脑,查找使用更方便
10000 积分 0人已下载
下载 | 加入VIP,交流精品资源 |
- 配套讲稿:
如PPT文件的首页显示word图标,表示该PPT已包含配套word讲稿。双击word图标可打开word文档。
- 特殊限制:
部分文档作品中含有的国旗、国徽等图片,仅作为作品整体效果示例展示,禁止商用。设计者仅对作品中独创性部分享有著作权。
- 关 键 词:
- DLAMILS7393C1968STEELALLOYCARBURIZINGBARSANDBILLETSSTEELNICKELCHROMIUM33103316AND9310AIRCRAFTQUALITYPDF

链接地址:http://www.mydoc123.com/p-693442.html