1、- MIL-DTL-53135 m 9999906 2022930 TT2 INCH-POUX2 MIL-DTL-53135 (NE) 9 September 1996 I DETAIL SPECIFICATION AUXILIARY POWER UNIT, 10 KW, 120/240 VAC, 60 HZ This specification is approved for use within the USA Communications- Electronics Command, Logistics and Readiness Center, Department of the Arm
2、y, and is available for use by all Departments and Agencies of the Department of Defense. 1. SCOPE 1.1 Scope. This detail specification covers the requirements for a 10 kW Auxiliary Power Unit, 120/240 VAC, 60 Hz, hereinafter called “APU“. The APU is a power source consisting of a self-contained eng
3、ine and generator, including remote controls, capable of producing electrical power when connected to its hosts source of fuel and starting power. 1.2 APU ratings. Rated voltage shall be 120 and 240 volts alternating current (VAC). Rated frequency shall be 60 Hz. Rated power factor shall be 0.8. Rat
4、ed speed shall be 3,E:O rpm. Rated power shall be 10 kW at 0.8 power factor (pf) lagging. The APU shall be re-connectable for the following voltages : a. 120-volt, single-phase, 2-wire b. 120/240-volt, single-phase, 3-wire 2. APPLICABLE DOCUMENTS 2.1 General. The documents listed in this section are
5、 needed to meet the requirements specified in sections 3 and 4 of this specification. This section does not include documents cited in other sections of this specification or recommended for additional information or as examples. While every effort has been made to ensure the completeness of this li
6、st, document users are cautioned that they must meet all specified requirements documents cited in sections 3 and 4 of this specification, whether or not they are listed. Beneficial comments (recommendations, additions, deletions) and any pertinent data which may be of use in mproving this document
7、should be addressed to: USA 10115 GRIDLEY RD, STE 228, FT BELVOIR VA 22060-5849 by using the Standardization Document Improvement Proposal (DD Form 1426) appearing at the end of this document or by letter. COMMUNICATIONS ELECTRONICS COMMAND, BELVOIR RDE CENTER, ATTN: AMSEL-LC-IEW-D-ED, AMSC N/A FSC
8、6115 DISTRIBUTION STATEMENT A. Approved for public release, distribution is unlimited. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-53135 (ME) 2.2 Government documents. 2.2.1 Specifications and standards. The following specifications and s
9、tandards form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are those listed in the issue of the Department of Defense Index of Specifications and Standards (DoDISS) and supplement thereto, cited in the solicitation (see 6.2). SPECI
10、FICATIONS FEDERAL A-A-52557 - DEPARTMENT OF DEFENSE MIL-L-2104 - MIL-T-5624 - MIL-A-11755 - MIL-A-4 6153 - MIL-F-46162 - MIL-L-4 61 67 - MIL-A-53009 - MIL-T-83133 - STANDARDS DEPARTMENT OF DEFENSE MIL-STD-4 O1 - MIL-STD-705 - MIL-STD-882 - MIL-STD-1472 - HANDBOOKS DEPARTMENTOF DEFENSE MIL-HDBK-705 -
11、 Fuel Oil; Diesel; For Posts, Camps and Stations. Lubricating Oil, Internal Combustion Engine, Tactical Service. Turbine Fuels, Aviation, Grades JP-4 and JP-5. Antifreeze, Arctic-type. Antifreeze, Ethylene Glycol, Inhibited, Heavy Duty, Single Package. Fuel, Diesel, Referee Grade. Lubricating Oil, I
12、nternal Combustion Engine, Arctic. Additive, Antifreeze Extender, Liquid Cooling Systems. Turbine Fuel, Avi.ation, Kerosene Type, Grade JP- 8. Electromagnetic Emission and Susceptibility Requirements for the Control of Electromagnetic Interference. Generator Sets, Engine-Driven, Methods of- Tests an
13、d Instructions. System Safety Program Requirements. Human Engineering Design Criteria for Military System, Equipment and Facilities. Generator Sets, Electrical, Measurements and Instrumentation. (Unless otherwise indicated, copies of federal and military specifications and standards are availab.le f
14、orm the Standardization Documents Order Desk, Building 4D, 700 Robbins Avenue, Philadelphia, PA 19111-5094.) 2.2.2 Other Government drawings and publications. The following other Government drawings and publications form a part.,of this document to the extent specified herein. Unless otherwise speci
15、fied, the issues shall be those in effect on the date of the solicitation (see 6.2). 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-* r MIL-DTL-53135 (ME) DRAWINGS ME TA 1323036218 - Auxiliary Power Unit, 10 KW, 120/240 VAC, 60 Hz. (Copies of draw
16、ings are available from the: US Army Communications- Electronics Command, RDE Center, Command, Control grade low sulfur No. 1-D or No. 2-D diesel fuel conforming to A-A-52557; JP-5 turbine fuel conforming to MIL-T-5624; or JP-8 turbine fuel conforming to MIL-T-83133, shall meet- all requirements Spe
17、cified herein. The APU, while operating on JP-4 turbine fuel conforming to MIL-T-5624 (with a cetane rating of 30 to 351, shall meet all requirements specified herein, except rated load may be reduced 15 percent and a maximum of 300 hours of operation on JP-4 per 3,000 hours of APU operation shall b
18、e required. Operation on JP-4 shall only be,required at temperatures from -18 to 38 C (O to 100 F) and at altitudes up to 914 meters (m) (3,000 feet ftl) . 3.7.4 Lubricants. The engine shall operate on lubricating oil conforming to MIL-L-2104, when temperatures are above -26 C (-15 F). The engine sh
19、all operate on lubricatingoil conforming to MIL-L-46167 when temperatures are at or below 4 .“C (40 OF). 3.7.5 Coolant. The APU shall operate with the following coolants: a. MIL-A-11755 antifreeze from -32 to 49 OC (-25 to 120 OF) ambient. b. Water with MIL-A-46153 inhibited antifreeze from -32 to 4
20、9 OC (-25 to 120 FI ambient. c. Water withMIL-A-53009 additive from 4 to 49 OC (40 to 120 OF) ambient. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-53135 (ME) 3.8 Audio noise. When tested as specified in 4.7.2.1, audio noise sound- pressur
21、e levels (SPLs) emanating from the APU shall not exceed 15 dBA at 7 m (22.9 ft) from the perimeter of the APU, when measured at 1.2 m (3.9 ft) above the ground. In addition, audio noise emanating from the APU shall not exceed 85 dBA at the operators station, defined to be 0.7 m (2.3 ft) from the con
22、trol panel. These requirements apply under all operating conditions specified herein with the APU operating at all loads from no load to rated load. 3.9 Environmental requirements. 3.9.1 Starting and operating. The APU shall start and operate under each and any combination of the following operating
23、 conditions: a. All possible relative humidities, with ambient temperatures ranging from -32 to 49 C (-25 to 120 F) at sea level; and from -32 to 35 “C at 1,219 m (-25 to 95 F at 4,000 ft). The high temperature requirement remains at 35 C (95 OF) at altitudes above 1,219 m (4,000 ft) . b. Altitudes
24、up to and including 2,438 m (8,000 ft). Rated load may be reduced by 3.5 percent for each 305 m (1,000 ft) above 1,219 m (4,000 ft) (e.g., at 8,000 ft rated load may be reduced by 14 percent). Exhaust smoke conditions shall be measured during all altitudes. Exhaust smoke testing shall be in accordan
25、ce with 4.7.2.20. c. When mounted in the host system with 127 millimeters (mm) (5 inches) of rain per hour impinging on the host system at angles from the vertical up to 45 degrees. d. When mounted in the host system, with 355 British thermal units (BTUs) per square foot per hour of solar radiation
26、on the host system. e. When mounted in the host system, with sand and dust article concentration of up to 1,400 milligrams per cubic meter (mg/m T ). Particle sizes shall range from less than 74 micrometers in diameter to 1,000 micrometers with the bulk of the particles ranging in size from 74 to 35
27、0 micrometers. f. When mounted in the host system, with a steady windspeed of 22 meters per second (m/s) (73 ft per second ft/s) and gusts up to 29 m/s (95 ft per secondft/s) at a height of 3 m (10 ft) above ground level. g. When mounted in the host system, with accumulations on the host system of i
28、ce glaze, freezing rain and hoarfrost of up to 13 mm (0.5 inch) and up to a specific gravity of 0.9. h. When mounted in the host system, in a salt fog or sea spray environment. 3.9.2 Storage. The APU without packaging shall not be damaged (see 6.4.3.1) by exposure to: a. Storage at -51 to 71 “C (-60
29、 to 160 F). b. Salt fog environment. c. All possible relative humidities. 11 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-53L35 M 9999906 20229211 888 II MIL-DTL-53135 (ME) 3.10 High altitude electromagnetic pulse (HAEMP). The APU shall wi
30、thstand the HAEMP nuclear environment as specified in the US Army Nuclear and Chemical Agency Memorandum, dated 17 April 1987. The APU shall meet the operational requirements specified herein within 5 minutes after being. subjected to the specified HAEMP nuclear environment. The recovery may not inc
31、lude the ,replacement of piece parts or components. 3.11 Electromagnetic interference. When tested in accordance with Appendix B, TM 101.1, the electromagnetic interference emission and susceptibility characteristics of the APU shall not exceed the UM04 limits of class C2 equipment of MIL-STD-461, P
32、art 9. 3.12 Treatment and painting. Treatment and painting shall be in accordance with the drawings. 3.13. Maintainability. The maintenance ratio (see 6.4.14) shall not exceed 0.05. 3.14 Endurance. The APU shall operate for 1,500 hours without critical failure (see 6.4.11d) at all loads, continuous
33、and intermittent, up to and including rated load, under all conditions specified in 3.9. The APU shall have a minimum life of 3,000 hours. 3.15 Safety and health. The APU shall conform to the provisions of MIL-STD-882, 5.13 of MIL-STD-1472 (as specified in 3.16) and shall use Requirement 1 of MIL-HD
34、BK-454 for guidance. Exposed parts of such nature as to be a hazard to personnel shall be insulated, enclosed or guarded without impairing the function of those parts. 3.16 Human factors engineering. The APU shall conform with the criteria of desiqn for human factors enqineering as described in MIL-
35、STD-1472. The APU shall be transportable, operabie and maintainable during day and night by 5th percentile through 95th percentile soldiers when wearing clothing which is appropriateto the environments described in 3.6 and 3.8.1, including Arctic. and MOPP IV mittens and clothing. Particular design
36、attention shall be given, but not limited to the following paragraphs of MIL-STD-1472: general requirements, -control/display integration, visual display, audio display, controls,. labeling, anthropometry, design for maintainability, hazards and safety. 3.17 Government-furnished property. When speci
37、fied, the APU shall be mounted in the Government-furnished SICPS or JTACS host system (see 6.6). 3.18 Workmanship. Workmanship shall be of a quality.to assure delivery of APUs that are free from defects (see 6.4.15). resulting from defective material and incorrect manufacturing or assembly practices
38、. 4. VERIFICATION 4.1 Classification of inspection-. Inspection shall be classified as follows: 12 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-53135 (ME) 4.2 Inspection conditions. Unless otherwise specified, all inspections shall be perf
39、ormed in accordance with the test conditions specified in the applicable test method document or applicable paragraphs in the specification, 4.2.1 Fuel, lubrications, and coolant for inspection. Grade low sulfur No. 2D fuel conforming to A-A-52557 shall be used for all tests unless otherwise specifi
40、ed herein. Grade low sulfur No. 1D fuel (A-A-52557) shall be used for all testing with ambient temperatures between -32 to -18 “C (-26 to O “F). Lubricating oil shall be as follows: SPECIFICATION MIL-L-2104 MIL-L-2104 MIL-L-2104 MIL-L-2104 II MIL-L-46167 GRADE DAILY LOW AMBIENT I TEMPERATURE (C/F) O
41、E/HDO-15/40 (O to 120 “F) OE/HDO-10 (-15 to 40 “F) OE/HDO-30 -9 to 49 “c I (15 to 120 “F) Coolant shall conform to either MIL-A-11755, water with MIL-A-46153 inhibited antifreeze, or water with MIL-A-53009 additive for all testing conducted at temperatures from 4 to 49 “C (40 to 120 F). Below 4 OC (
42、40 “F), either MIL- A-11755 or water with MIL-A-46153 inhibited antifreeze shall be used for testing. 4.3 First article preproduction inspection. The separate generator, with excitation system, and complete APUs shall be examined and tested as specified herein to determine compliance with this speci
43、fication. 4.3.1 Examination of components and subassemblies. Examination of components and subassemblies shall be made prior to assembly of the APU. Evidence that any components or subassemblies do not comply with the requirements of this specification shall be cause for rejection of that component
44、or subassembly. 4.3.1.1 Examination of generator with excitation system and APUs. Examination of the separate generator with excitation system and the five APUs shall be made without disassembly. Evidence that the generator, excitation system, or APUs do not comply with the drawings shall be cause f
45、or rejection of the generator, excitation system, or APUs. 4.3.2 Preproduction tests. Two preproduction APUs shall be subjected to the applicable tests marked “X“ under column 1 of table I except for the reliability test. Three preproduction APUs shall be subjected only to the reliability test of ta
46、ble I. All generators shall be subjected to the generator only tests marked “X“ in column 1 of table I. The separate generator with excitation system shall be subjected to the qenerator with excitation system tests marked “X“ under column 1 of table 1. In addition to 13 Provided by IHSNot for Resale
47、No reproduction or networking permitted without license from IHS-,-,-MIL-DTL-53135 9999906 2022923 650 m I MIL-DTL-53135 (ME) any test specified as part of the preproduction tests, the Government reserves the right to conduct any and all other tests contained in this specifications as part of the pr
48、eproduction tests. Failure of such additional tests shall have the same effect as failure of those tests specified as preproduction tests. TABLE I. Test schedule. t “ XI XI X X X X X X X X I I . i CENERATOR ONLY: XI High Poteztial XI IInsulation Resistance X Winding Resistance 6ENERATOR WITH EXCITAT
49、ION SYSTEM: I IDirect-axis Transient I I Reactance I X Iteneracor Power Input lopen Circuit Saturation I I Cirve Rated load Current Saturation Curve I Synchronous Impedance Curve (Short-circuit lsaturation Curve) I 1Zero Power Factor lsaturation Curve I X INoise level XI lcircuit Interrupter vervoltage) X Sample Endurance X Frequency Adjustment Range X Frequency One point at rated voltage only for individual testsi TM 625.1
