NAVY MIL-I-18856 B-1969 INDICATOR ANGLE OF ATTACK 28 VDC MS28062 AND MS28067《 MS28062 及 MS28067型28伏攻角指示器》.pdf
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1、J .- M I L- I - 1 8 8 5 6 B (AS) 27 OCTOBER 1969 SUPERSEDING MILI- 18856A(Wep) 20 October 1960 -.- MIIJTARY SPE CIC ATION INDICATOR, ANGLE OF ATTACK, 28X D. C. MS28062 and MS 28067 This specification has been approved by the Naval Air Systems Command, Department of the Navy. 1. SCOPE 1.1 Scope - Thi
2、s specification covers design and all performance re- quirements for the 1-7/8 inch dial, MS28067, and 2-3/4 inch dial, hB28062, 28v d. c. angle of attack indicators. Configuration of each indicator shall be governed by the dash number for the Military Standard Drawing. 2. APPUCABLE DOCUMENTS 2.1 Ge
3、neral - The following documents of the issue in effecton the date of invitation for bids, form a part of this specification to the extent specified he re in. SPECIFIC 4.TIONS PIIilitary MIL- D- 10 O0 /l Drawings, Engineering and Associated Data AD L-C - 5 O 15 Connectors, Electric, AN Type .IhLC- 14
4、806 Coating, Reflection Reducing, For Instrument Cover / Glasses and Lighting Wedges / XIILI- 180 7 9 3EIL-T- 18303 .Installation of Angle of Attack and Sideslip Systems Test Procedures, -Production and Acceptance for Air- -craft Electronic Equipment, Format for .MIL-T- 19229 Transmitter, Angle of A
5、ttack or Sideslip, ha1 MILP-215G3 Paint System, Fluorescent, for Aircraft Application , . THIS DOCUMENT CONTAINS 21 PAGES. D Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-I-LB85bB 66 m 777770b 0327775 7 m i . IL-I-l8856B(AS) SPECIFICATIONS Mili
6、 t nry (Cont inucd) MIGL-25467 MIL-C-26482 MIG L-2 7 16 O MIGI- 81400 STANDARDS Mi lit arx MIGSTD-143 MIGSTD- 46 1 XILSTD-470 MIGSTD- 47 1 MIGSTD- 7 O 4 MIL-STD-781 BIL-STD- 785 MIGSTD-794 h.1 IL- STD- 8 1 O IUS24367 MS245 15 Lighting, Integral, Aircraft Instrument, General Specification for (Red) C
7、onnector, Electric, Circular, Miniature, Quick Disconnect Lighting, Instrument, Integral, White, General Spec- ification for .Instruments, Aircraft, General Specification for Specifications and Standards, Order of Precedence for the Selection of - Electromagnetic Interference Characteristics Require
8、- -merits . _Maintainability Program Requiremerits (for Systems .and Equipments) Maintainability Demonstration Electric Power, Aircraft, Characteristics and Utili- zation of Reliability Tests, Exponential Distribution .Requirements for Reliability Program . Parts and Equipment, Procedures for Packag
9、ing and Packing of _ .Environmental Test Methods -Lamp, Incandescent-Miniature Integral Lighting .Lamp, Subminiature Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-t MIL-I-185bB bb m 779770b 0129776 7 MI G I- 1 8 85 G B (AS) STANDARDS Military (Cont
10、inued) MS28062 Indicator, Angle of Attack, 2-3/4Dial, 28Volt D. C. MS28067 Indicator, Angle of Attack, 1-7/8 Dial, 28 Volt D. C. MS28105 Window, Dial - Aircraft Instrument Cover, Glass 34533585 Pointer, Dial, Standard Design of Aircraft Instrument Federal FED-STD-595 Colors 2.2 Availability of Docum
11、ents - When requesting any of the applicable documents, refer to both title and number. Copies of this specification and applicable documents may be obtainedupon application to the Commanding Officer, Naval Publications and Forms Center, Code 1051, 5801 Tabor Avenue, Philadelphia, Pennsylvania 19120
12、. 3. XEQUIREhIENTS 3.1 Qualification - This specification makes provision for qualification . testing. 3.2 General DesignRequirements- Selection and use of parts and ma- terials and general requirements for design and construction shall be in accordance with the requirements of MIGI-81400. 3.3 Selec
13、tion of Government Documents - Specifications and standards for necessary commodities and services not specified herein and in MIGI-81400 shall be selected in accordance with MIL-STD-143. 3.4 Weight - The weight of each indicator shall not exceed that speci- fied for each dash number. 3.5 - Performa
14、nce shall nect the Test Methods of Sectiori 4. 3.5.3 Reliabilit; - The supplier shall establish a reliability assurance yrogrniii for the iiidicntor in accordance with MIL-STD-785. 3.5.1.1 Operational Stability - The indicator shall operate with satisfactory performance, continuously or intermittent
15、ly for a period of at least 1,500 hours with- out the necessity for readjustment or relubrication. 3 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-F -MIL-I-15bB 66 7777706 0327777 O MIGI-l8856B(AS) 3.5.2 Operating Life - The, indicator shall have a
16、 minimum operating life of 6,000 hours with reasonable servicing and replacement of parts. Parts requiring scheduled replacement shall be specified by the supplier. 3.5.3 Reliability in Nean Timc Retween Failure (MTRF) - The indicator shall have 1.500 hours of mean (operating) time between failures
17、when tested and ac- cepted as outlined under the Reliability Assurance Test requirements. 3.6 - Dial andPointer - 3.6.1 Visibility ofDial - The pointer, numerals, at least 1/16th inch of the shortest graduations and all other specified markings on the dial shall be visible from any point within the
18、frustum of a cone whose side makes an angle of 20“ with a perpendicular to the dial and whose small diameter is the aperture of the case. 3.6.2 Dial Marking - The dial shall be marked as shown in Figure 1 or Figure 2, as applicable. 3.6.3 Pointer - The pointer of the indicator shall conform to Figur
19、e 1 or Figure 2. 8s applicable. 3.7 . CoverGlass - The dimensions of the cover glass shall be in ac- cordance with MS28105 unless the glass is part of the integral lighting. 3.7.1 Cover Glass and Wedges - The indicator cover glass and any other transparent element between the glass and the dial, suc
20、h as a lighting wedge, shall be provided with a reflection reducing coating that meets the requirements of MILC- 14806. 3.7.2 Cover Glass Mounting - The distance from the -inner surface of the cover glass to the surface of the dial on which the marking is applied shall not exceed O. 25 inch. 3.8 3.8
21、.1 Electrical Requirements - Fuses or circuit breakers not pedtted. Primary Input Power Requirements - The indicator shall give specified performance from power sources with characteristics as defined in MIL- STD-704 having limits as specified herein. The power required shall not exceed the specifie
22、d amounts. (a) D.C. power 28v Category ItB“ 10 watt max for servo. 3.8.1.1 Integrally LightedIndicator - The integrally lighted indicator, op- -erating on 5 f O. 1 volts a. c. or d. c. , 3 watts max. for exch color, using lamps .MS24367-715AS15 or MS24515-718AS15, shall illuminate all markings withi
23、n the indi- cator case as specified in MILL-25467 and MILL-27160 for the red and/or white integral lighting utilized. -. 4 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-30 . -_ HEIGHT OH UrJFH OF LINE MARKING LENGTH OR GRADUATION +. O10 f. 005 MIL-
24、I-3885b 66 977790b 0327778 2 MATERML OR FIhTSH EQUAL SPACES DIAL ANGLEOF ATTACK - MAJOR GRADUATIONS INTERMEDIATE GRADUATIONS NUMERALS LETTERS SHADED PORTION OF POINTER - ,120 . O90 h L.8402 .O29 .o21 ,023 .o21 LUS r E RLF ss WHITE NO. 3787: OF FED-SID-595 R .125 a 093 CLIMB AND REFERENCE INDICES BAC
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