AIR FORCE MIL-T-87976-1985 TEST STAND HYDRAULIC SYSTEM COMPONENTS《液压系统元件试验台》.pdf
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1、1. MIL-T-7976 LI9 9999906 0258LI52 3 a o f -J7/ v MIL-T- 87976 16 June 1985 MILITARY SPECIFICATION TEST STAND, HYDRAULIC SYSTEM COMPONENTS This specification is approved for use by all Departments and Agencies of the Department of Defense. SCOPE 1.1 Scope. This document covers the requirements for a
2、 non-portable test stand that will test aircraft hydraulic components, 2, APPLICABLE DOCUMENTS 2.1 Government documents. 2.1.1 Specifications and standards. Unless otherwise specified (see 6,2), the following specifications and standards of the issue listed in that issue of the Department of Defense
3、 Index of Specificaeions and Standards (DoDISS) specified in the solicitation, form a part of this specification to the extent specified herein. SPECIFICATIONS MILITARY MIL-P-116 MIL-H-5440 MIL-R-5520 MIL-H-5606 MIL-H- 6 08 3 MIL-S-26716 MIL-F-27 656 Preservation, Methods of Hydraulic Systemss Aircr
4、aft, Type I and II, Design and Installation Requirements for. Reservoir, Aircraft, Hydraulic, Nonseparated Type. Hydraulic-Fluid, Petroleum Base, Aircraft, Missile and Ordnance. Hydraulic Fluid, Petroleum Base, for Preservation and Testing. Stand, Test, Aircraft Hydraulic Systems, Non- Portable, Gen
5、eral Specification. Filter Unit , Fluid, Pressure MXU-408/M, 5 Micron, Hydraulic. . Beneficial comments (recommendations, data which may be of use in improving this document should be addressed to: the Engineering Division, San Antonio ALC/MMEDO, Kelly AFB, Texas 78241 by using the self-addressed St
6、andardization Document Improvement Proposal (DD Form 1426) appearing at the end of this document or by letter. u_ FSC 4920 DISTRIBUTION STATEMENT A. Approvedfor public release; distributionis unlimited. THIS DOCUMENT CONTAINS 13 PAGES Provided by IHSNot for ResaleNo reproduction or networking permit
7、ted without license from IHS-,-,-MIL-T-87976 ri9 999990b 0258Y53 5 = MIL-T- 87976 STANDARDS FEDERAL FED-SMI-595 Colors MILITARY MIL-STD-129 MIL-STD-4 54 MIL-STD-470 MIL= STD-7 9 4 MIL-STD-808 MIL-STD-882 1-1s 3 3 6 11 MS2 19 19 MS 33 656 Marking for Shipment and Storage. Standard General Requirement
8、s for Electronic Equipmen t. Maintainability Program Requirements (for Systems and Equipment). Parts and Equipment Procedures for Packaging and Packing of, Finish, Protective, and Codes for Finishing Schemes for Ground and Ground Support Equipment, System Safety Program Requirements. Clamp, Loop-Typ
9、e, Cushioned, Support. Tube, Bend Radii Fitting End, Standard Dimensions for Flared Tube Connector and Gasket Seal. AIR FORCE - NAVY AERONAUTICAL AND10059 AND10104 Tubing, Steel, Corrosion Resistant, Round AND20001 Drive-Type XI Engine Accessory. AND20002 Drive-Type XII Engine Accessory. Fitting - S
10、tyle of Pipe Threaded Flared Tube and Hose. Standard Dimensions for. (Copies of specifications and standards required by manufacturers in con- nection with specific acquisition functions should be obtained from the con- tracting activity or as directed by the contracting officer.) 2.1.2 Other public
11、ations, The following document(s) form a part of this specification to the extent specified herein, which are indicated as DoD adopted shall be the issue listed in the current DoDISS and the supplement thereto, if applicable. The issues of the documents AMERICAN SOCIETY FOR TESTING AND MATERIALS (AS
12、TM) ASTI1 D 3951 Standard Practice for Commercial Packaging. 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-R . -.r MIL-T-87776 47 7777706 0258454 7 , i ! O I I , ! 1 i. I f t ! I i. L MIL-T-87976 (Applications for copies of ASIIM publications sho
13、uld be addressed to the American Society for Testing and Materials, 1916 Race Street, Philadelphia, PA 19103.) AMERICAN STANDARDS C-50 Rotating Electrical Machinery. (Copies of the ASA standard.s may be obtained from the American Standards Association, 10 East 40th Street, New York, NY 10016.) NATIO
14、NAL ELECTRICAL MANUFACTURERS ASSOCIATION Standard MG-1 Motors and Generators. (Copies of the NEMA may be obtained from the National Electrical Manufac- turers Association, Engineering Department, 155 East 44th Street, New York, NY 10017. ) NATIONAL FIRE PROTECTION ASSOCIATION Code 70 National Electr
15、ical Code (Electric Wiring Apparatus) . (Copies of the NFPA may be obtained from the National Fire Protection Asso- ciation, 60 Batterymarch Street , Boston, MA, 02110.) * 2.1.3 Order of precedence. In the event of a conflict between the text of this specification and the references cited herein, th
16、e text of this specifica- tion shall take precedence. 3. REQUIREMENTS 3.1 General. Each test stand console shall meet the requirements of MIL-S-26716. Detail requirements specified herein supplement or alter the requirements of MIL-S-26716. The requirements specified herein are minimum; items provid
17、ing additional characteristics, greater accuracy and improved per- formance will be acceptable. 3 12 General requirements. The requirements of MIL-H-5440 for materials , fluids, reservoir venting, tubing, and cleaning of parts and systems apply as requirements of this specification with the exceptio
18、ns and additions specified herein. This test stand shall be designed for the performance testing of hydraulic system components such as valves, actuating cylinders, solenoid Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-8797b Li9 W 777790b O2
19、58455 7 W MIL-P.87976 valves, reservoirs, accumulators, pumps, etc., using either MIk-H-5606 gr MIL-11-6083 hydraulic fluids at an operating temperature of 100 F to 160 F. The test stand shall contain the following basic flow and pressure circuits or capabilities : a, A pump test circuit suitable fo
20、r testing fixed and variable volume pumps with displacements up to 30 GPM, discharge pressures up to 3200 pcig, inlet pressures from O to 150 psig, and case drain flows from 0.13 to 1.66 gpm at pressures from O to 160 psig. b, A 500 to 5000 rpm variable speed drive which shall deliver sufficient tor
21、que to drive a hydraulic pump with a displacement of 30 gpm at 3750 rpm and at a pressure of 3000 psig. c. A hydraulic static pressure circuit capable o? generating hydrostatic pressures up to 25,000 psi. d, h pneumatic static pressure test circuit capable of providing pres- sures up to 3,000 psig.
22、A dynamic test circuit: capable of testing a variety of aircraft com- ponents such as actuating cylinders, relief valves, selector valves, shuttle valves, etc., at flow rates up to 30 gpm with pressures up to 3750 psig and back pressures up to 200 psig, capable of generating 5000 psig pressures at r
23、educed flow rates. P e, The system shall be f, DC and AC electrical power supplies. g, I-feasuring instruments and circuits shall be provided so that the above can be measured throughout their various ranges. 3.2.1 Cabinet. The test stand equipment shall 5e located within a two section cabinet. One
24、section shall contain the drive console and the other section shall contain the control console, In use the two sections are to be fastened together, contractor furnished. All hardware required to make this connection shall be 3.2.1.2 Drive console cabinet. The drive console cabinet shall contain th
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