AIR FORCE MIL-DTL-7891 G-2008 FILLER VALVE AIRCRAFT OXYGEN《飞行器用氧气充气阀》.pdf
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1、 AMSC N/A FSC 1660 MIL-DTL-7891G 10 October 2008 SUPERSEDING MIL-PRF-7891F 22 December 1997 DETAIL SPECIFICATION FILLER VALVE, AIRCRAFT OXYGEN This specification is approved for use by all Departments and Agencies of the Department of Defense. Comments, suggestions, or questions on this document sho
2、uld be addressed to: Oklahoma City Air Logistics Center/ENSDAA, 3001 Staff Drive, Tinker AFB, OK 73145-3036 or emailed to af71tinker.af.mil. Since contact information can change, you may want to verify the currency of this address information using the ASSIST Online database at http:/assist.daps.dla
3、.mil. INCH-POUND Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-7891G 2 1 SCOPE 1.1 Scope. This specification covers low pressure and high pressure aircraft oxygen filler valves. 1.2 Classification. The valves are classified as follows: Clas
4、s L - Low pressure H - High pressure Style F - Female M - Male Configuration (see figure 1, 4, 5 and 6) 1.2.1 Part or Identifying Number (PIN). The PIN is constructed as follows: M 7891 X X - X Configuration (see figure 1 through 6) Style F Female M Male Class L Low pressure H High pressure Specific
5、ation number M prefix 2. APPLICABLE DOCUMENTS 2.1 General. The documents listed in this section are specified in sections 3, 4, or 5 or this specification. This section does not include documents cited in other sections of this specification or recommended for additional information or as examples.
6、While every effort has been made to ensure the completeness of this list, document users are cautioned that they must meet all specified requirements of documents cited in sections 3, 4, or 5 of this specification, whether or not they are listed. Provided by IHSNot for ResaleNo reproduction or netwo
7、rking permitted without license from IHS-,-,-MIL-DTL-7891G 3 2.2 Government documents. 2.2.1 Specifications, standards, and handbooks. The following specifications, standards, and handbooks form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these d
8、ocuments are those cited in the solicitation or contract. INTERNATIONAL STANDARDIZATION AGREEMENTS AIR-STD-25/34A(1) - Aircraft Gaseous Oxygen Replenishment Connections FEDERAL SPECIFICATIONS BB-A-1034 - Compressed Air, Breathing COMMERCIAL ITEM DESCRIPTIONS A-A-59503 - Nitrogen, Technical DEPARTMEN
9、T OF DEFENSE SPECIFICATIONS MIL-PRF-25567 - Leak Detection Compound, Oxygen Systems MIL-PRF-27210 - Oxygen, Aviators Breathing, Liquid and Gas DEPARTMENT OF DEFENSE STANDARDS AN800 - Cone and Union (Copies of these documents are available online at http:/assist.daps.dla.mil/quicksearch/ or from the
10、Standardization Document Order Desk, 700 Robbins Avenue, Building 4D, Philadelphia, PA 19111-5094.) 2.3 Non-Government publications. The following documents form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are those cited in the s
11、olicitation or contract. AMERICAN NATIONAL STANDARDS INSTITUTE/AMERICAN SOCIETY FOR QUALITY (ANSI/ASQ) ANSI/ASQC Z1.4 - Sampling Procedures and Tables for Inspection by Attributes (ANSI documents may be obtained at www.ansi.org or from American National Standards Institute, 25 West 43rd Street, New
12、York, NY 10036.) Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-7891G 4 AMERICAN SOCIETY FOR TESTING AND MATERIALS (ASTM) ASTM B117 - Salt Spray (Fog) Apparatus, Operating (ASTM documents may be obtained at www.astm.org or addressed to the A
13、merican Society for Testing and Material, 100 Barr Harbor Drive, West Conshohocken, PA 19428-2959.) AMERICAN SOCIETY OF MECHANICAL ENGINEERS (ASME) ASME B46.1 - Surface Texture, (Surface Roughness, Waviness, and Lay) ASME B1.1 - Unified Inch Screw Threads, (UN and UNR Thread Form) (ASME documents ma
14、y be obtained at http:/www.asme.org/ or addressed to American Society of Mechanical Engineers, United Engineering Center, 345 East 47th Street, New York, NY 10017-2392) METALS AND ALLOYS IN THE UNIFIED NUMBERING SYSTEM (UNS) UNS C36000 - Free Cutting Brass UNS C37700 - Forging Brass UNS N04405 - Ni-
15、Cu Alloy Solid Solution Strengthened (Monel R405) UNS S30200 - Austenitic Cr-Ni Stainless Steel UNS S30400 - Austenitic Cr-Ni Stainless Steel (UNS documents may be obtained at http:/www.sae.org/servlets/index or addressed to Society of Automotive Engineering, 400 Commonwealth Drive, Warrendale, PA 1
16、5096-0001) SOCIETY OF AUTOMATIVE ENGINEERS (SAE) SAE AMS3305 - Silicon Rubber, General Purpose 80 Durometer SAE AS5202 - Port or Fitting End, Internal Strait Thread SAE AS568 - O-Rings, Aerospace Size Standard For Provided by IHSNot for ResaleNo reproduction or networking permitted without license f
17、rom IHS-,-,-MIL-DTL-7891G 5 SAE AS4395 - Tube Connection, Fitting End Flared, Design Standard SAE AS5201 - Fitting End, External Taper Pipe Thread, Design Standard SAE J1926-1 - Connections for General Use and Fluid Power Ports and Stud Ends with ASME B1.1 Threads and O-Ring Sealing Part 1: Threaded
18、 Port with O-Ring Seal in Truncated Housing (SAE documents may be obtained at http:/www.sae.org or addressed to Society of Automotive Engineering, Inc., 400 Commonwealth Drive, Warrendale, PA 15096.) 2.4 Order of Precedence. Unless otherwise noted herein or in the contract, in the event of a conflic
19、t 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 Qualification. The valves furnished under
20、this specification shall be products that are authorized by the qualifying activity for listing on the applicable qualified products list before contract award (see 4.2 and 6.3). 3.2 Recycled, recovered, or environmentally preferable materials. Recycled, recovered, or environmentally preferable mate
21、rials should be used to the maximum extent possible, provided that the material meets or exceeds the operational and maintenance requirements, and promotes economically advantageous life cycle costs. 3.3 Materials. All materials shall be corrosion resistant or suitably treated to resist corrosion du
22、e to electrolytic decomposition, salt air, and any other atmospheric conditions that may be encountered during operational use or storage. All lubricants used shall be compatible with a pure oxygen environment and shall create no health or fire hazards (see 6.7). The use of toxic chemicals, hazardou
23、s substances, or ozone depleting chemicals (ODC) shall be avoided, whenever feasible. 3.4 Interface. 3.4.1 Safety-specific materials. All mating surfaces that are exposed to oxygen flow must resist wear from repetitive coupling and uncoupling and shall be nickel-copper alloy conforming to UNS N04405
24、. Surfaces that are exposed to oxygen flow, but are not mating surfaces, shall conform to UNS C36000, C37700, or N04405. Springs, if not directly in the oxygen flow path, may conform to UNS S30200 or S30400. Alternative materials that perform as well as, or better than these materials may be propose
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