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本文(DLA MIL-DTL-52525 10 D-2011 FITTINGS HOSE SCREW-ON TO 4-BOLT SPLIT-FLANGE STRAIGHT.pdf)为本站会员(postpastor181)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!

DLA MIL-DTL-52525 10 D-2011 FITTINGS HOSE SCREW-ON TO 4-BOLT SPLIT-FLANGE STRAIGHT.pdf

1、 MIL-DTL-52525/10D 21 April 2011 SUPERSEDING MIL-DTL-52525/10C 12 November 2008 DETAIL SPECIFICATION SHEET FITTINGS, HOSE, SCREW-ON TO 4-BOLT SPLIT-FLANGE, STRAIGHT This specification is approved for use by all Departments and Agencies of the Department of Defense. The requirements for acquiring the

2、 product described herein shall consist of this specification sheet and MIL-DTL-52525. FIGURE 1. Fitting, screw-on to 4-bolt split-flange, straight. AMSC N/A FSC 4730INCH-POUND Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-52525/10D 2 Part

3、or Identifying Number (PIN) Hose Tube dash no. Flange head A max inches (mm) B min inches (mm) C max inches (mm) Hose dash no. ID inches (mm) Dash no. inches (mm) M52525/10-8-8 -8 .500 (12.70) -8 -8 .500 (12.70) 3.78 (96.01) 1.27 (32.26) 1.38 (35.05) M52525/10-8-12 -8 .500 (12.70) -12 -12 .750 (19.0

4、5) 4.02 (102.11) 1.32 (33.53) 1.57 (39.88) M52525/10-10-12 -10 .625 ( -12 -12 .750 (19.05) 4.14 (105.16) 1.34 (34.04) 1.66 (42.16) M52525/10-12-12 -12 .750 (19.05) -12 -12 .750 (19.05) 4.25 (107.95) 1.36 (34.54) 1.75 (44.45) M52525/10-12-16 -12 .750 (19.05) -16 -16 1.000 (25.40) 4.50 (111.43) 1.49 (

5、33.53) 1.91 (48.51) M52525/10-16-16 -16 1.000 (25.40) -16 -16 1.000 (25.40) 4.74 (120.40) 1.61 (40.89) 2.06 (52.32) M52525/10-16-20 -16 1.000 (25.40) -20 -20 1.250 (31.75) 4.74 (120.40) 1.61 (40.89) 2.06 (52.32) M52525/10-20-20 -20 1.250 (31.75) -20 -20 1.250 (31.75) 5.35 (135.89) 1.80 (45.72) 2.63

6、(66.80) M52525/10-20-24 -20 1.250 (31.75) -24 -24 1.500 (38.10) 5.35 (135.89) 1.80 (45.72) 2.63 (66.80) M52525/10-24-24 -24 1.500 (38.10) -24 -24 1.500 (38.10) 5.61 (142.49) 2.08 (52.83) 2.94 (74.68) M52525/10-24-32 -24 1.500 (38.10) -32 -32 2.000 (50.80) 5.61 (142.49) 2.08 (52.83) 2.94 (74.68) M525

7、25/10-32-32 -32 2.000 (50.80) -32 -32 2.000 (50.80) 6.37 (161.80) 2.44 (61.98) 3.50 (88.90) NOTES: 1. Dimensions are in inches. 2. Metric equivalents are given for information only. 3. All dimensions not shown shall be in accordance with SAE-J516 and SAE-J518 as applicable. 4. These fittings are sim

8、ilar to SAE-J516 assemble with SAE-J517 hose and SAE-J518 flange to manufacturer MIL-DTL-52471 hose assembly. FIGURE 1. Fitting, screw-on to 4-bolt split-flange, straight - Continued. REQUIREMENTS: Fittings shall be as specified in figure 1 and in tables I and II. The fittings described herein are f

9、or use with MIL-DTL-52471/5, type 100R2, double wire braided hose and hose assemblies in accordance with MIL-DTL-52525/2. If fittings are to be used on an oxygen hose, see MIL-DTL-52525. Materials and finishes shall be in accordance with MIL-DTL-52525 and in table I. All finishes shall be capable of

10、 withstanding 96 hours minimum of salt spray. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-52525/10D 3 TABLE I. Material and finish identification codes. 1/ 2/ PIN code material/plating finish Material Plating finish A Aluminum alloy 6061

11、or 7075 Anodize in accordance with MIL-A-8625, type II. AN Anodize in accordance with MIL-A-8625, type II and NAVAIR trivalent chromium pretreatment (TCP) in accordance with MIL-DTL-81706, type II, class 1A. BN Bare aluminum with NAVAIR TCP in accordance with MIL-DTL-81706, type II, class 1A. C Stee

12、l 3/ Cadmium plating in accordance with SAE-AMS-C-81562, type II, class 3 or SAE-AMS-QQ-P-416, type II, class 2. CN Cadmium plating in accordance with SAE-AMS-C-81562, type II, class 3 or SAE-AMS-QQ-P-416, type II, class 2 and NAVAIR TCP in accordance with MIL-DTL-81706, type II, class 1A. YC Chrome

13、-molybdenum steel alloy 4130 Cadmium plating in accordance with SAE-AMS-C-81562, type II, class 3 or SAE-AMS-QQ-P-416, type II, class 2. DN Cadmium plating in accordance with SAE-AMS-C-81562, type II, class 3 or SAE-AMS-QQ-P-416, type II, class 2 and NAVAIR TCP in accordance with MIL-DTL-81706, type

14、 II, class 1A. F Steel 3/ NAVAIR TCP in accordance with MIL-DTL-81706, type II, class 1A. FN Chrome-molybdenum steel alloy 4130 G Steel 3/ Zinc plating with colorless passivate in accordance with ASTM B633, type VI, Fe/Zn 25. YG Chrome-molybdenum steel alloy 4130 H Steel 3/ Zinc phosphate finish in

15、accordance MIL-DTL-16232, type Z, class1. 4/ YH Chrome-molybdenum steel alloy 4130 J Steel 3/ Zinc plating with chromate conversion in accordance with ASTM B633; type II or III, Fe/Zn 5, or ASTM B695, type II, class 5. YJ Chrome-molybdenum steel alloy 4130 K Nickel-copper alloy UNS N04400 No additio

16、nal finish. M High-chromium nickel alloy UNS N06690 No additional finish. N Steel 3/ Zinc aluminum in accordance with ASTM F1136, grade 3, NC. YN Chrome-molybdenum steel alloy 4130 P Steel 3/ Zinc plating with colorless passivate in accordance with ASTM B633, type VI, Fe/Zn 5. YP Chrome-molybdenum s

17、teel alloy 4130 S Corrosion resistant steel No additional finish. Passivation in accordance with SAE-AMS2700, type 6 or 7. SN Passivation above and NAVAIR TCP in accordance with MIL-DTL-81706, type II, class 1A. T Titanium Anodize in accordance with SAE-AMS2488, type 2. V Steel 3/ Zinc-nickel in acc

18、ordance with SAE-AMS2417, type 1. W Steel 3/ Any zinc plating above. YW Chrome-molybdenum steel alloy 4130 Z Steel 3/ Any zinc plating above with NAVAIR TCP in accordance with MIL-DTL-81706, type II, class 1A. YZ Chrome-molybdenum steel alloy 4130 1/ All materials and finishes shall be in accordance

19、 with MIL-DTL-52525. 2/ Embitterment test need not be run. 3/ All steels except 4130. 4/ Zinc phosphate finish is hexavalent chromium free. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-52525/10D 4 Maximum operating pressure shall be as spe

20、cified in table II. TABLE II. Maximum operating pressures of fittings. 1/ 2/ SAE dash size Hose ID inches (mm) Steel, CRES, titanium, nickel-copper alloy , and high-chromium nickel Aluminum psi MPa psi MPa -8 .500 (12.70) 3500 24.1 2500 17 -10 .625 (15.88) 2750 19.0 1750 12 -12 .750 (19.05) 2250 15.

21、5 1650 11 -16 1.000 (25.40) 2000 13.8 1000 7 -20 1.250 (31.75) 1625 11.2 850 6 -24 1.500 (38.10) 1250 8.6 750 5 -32 2.000 (50.80) 1125 7.8 600 4 1/ Dimensions are in inches. 2/ Metric equivalents are given for information only. PIN: The PIN consists of the letter “M” the specification sheet number,

22、a dash, a number for hose size, a dash, a number for tube size, a dash, a number for flange, and a material finish designator. M 52525/10 -20 -24 A PIN example: M52525/10-20-24A, describes a split flange for a 1.250 inch (31.75 mm) hose, with a 1.500 inch (38.10 mm) flange, aluminum with an anodized

23、 finish. To the users of this document, it is recommended that the use of carbon steel material with cadmium plating be used only when the other materials and finishes specified in this document cannot meet performance requirements. Color identification. Color identification shall be in accordance w

24、ith SAE-AS4841. Marking shall include the manufacturers name or trademark, size, and hose identifier R2. Location of marking is optional. Harmonization to SAE-J516 and SAE-J518 cross reference PIN in table III is for reference only. SAE style fittings may not have the same material/finish as require

25、d by MIL-DTL-52525 and legacy with MIL-DTL-52471. Size dash number for hose (see figure 1) Specification sheet number M prefix Material/finish designator (see table I) Size dash number for flange (see figure 1) Provided by IHSNot for ResaleNo reproduction or networking permitted without license from

26、 IHS-,-,-MIL-DTL-52525/10D 5 TABLE III. Harmonization to SAE-J516 and SAE-J518 cross reference PIN. 1/ PIN SAE-J516 PIN M52525/10-8-8 SAE J516 8-8 390154 M52525/10-10-8 SAE J516 10-8 390154 M52525/10-10-12 SAE J516 10-12 390154 M52525/10-12-12 SAE J516 12-12 390154 M52525/10-16-16 SAE J516 16-16 390

27、154 M52525/10-16-20 SAE J516 16-20 390154 M52525/10-20-20 SAE J516 20-20 390154 M52525/10-20-24 SAE J516 20-24 390154 M52525/10-24-24 SAE J516 24-24 390154 M52525/10-24-32 SAE J516 24-32 390154 M52525/10-32-32 SAE J516 32-32 390154 1/ Material and finish designators are omitted from PINs see table I

28、 and SAE-J846. Notes: 1. For design feature purposes, this standard takes precedence over the procurement document referenced herein. Referenced documents shall be of the issue in effect on the date of invitation for bid. 2. In the event of a conflict between the text of this standard and the refere

29、nced cited herein, the text of this standard shall take precedence. Changes from previous issue. Marginal notations are not used in this revision to identify changes with respect to the previous issue, due to the extent of the changes. Referenced documents. In addition to MIL-DTL-52525, this documen

30、t references the following: MIL-A-8625 MIL-DTL-16232 MIL-DTL-52471 MIL-DTL-52471/5 MIL-DTL-52525/2 MIL-DTL-52525/16 MIL-DTL-52525/17 MIL-DTL-81706 ASTM B633 ASTM B695 ASTM F1136 SAE-AMS-C-81562 SAE-AMS-QQ-P-416 SAE-AMS2417 SAE-AMS2488 SAE-AMS2700 SAE-AS4841 SAE-J516 SAE-J517 SAE-J518 SAE-J846 Provid

31、ed by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-52525/10D 6 CONLUDING MATERIAL Custodians: Preparing activity: Army - AT DLA - CC Navy - SH Air Force - 99 (Project 4730-2011-051) DLA - CC Review activities: Army - CR4 Navy - AS, CG, MC, SA, YD NOTE

32、: The activities listed above were interested in this document as of the date of this document. Since organizations and responsibilities can change, you should verify the currency of the information above using the ASSIST Online database at https:/assist.daps.dla.mil. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-

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