NAVY MIL-I-23832 A-1980 INDICATOR TACHOMETER TRIPLE POINTER HELICOPTER《直升机三重指针转速表指示器》.pdf
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1、O 25 June 1980 MI L - I - 23832 (AS I 19 March 1972 MILITARY SPECIFICATION INDICATOR, TACHOMETER, TRIPLE POINTER, HELICOPTER This specification is approved for use by the Naval Air Systems Command, Department of the Navy, and is available for use by all Departments and Agencies of the Department of
2、Defense. 1.1 Scope. This specification covers design and all .-? performance requirements for helicopter triple pointer tachometer indicators. 1.2 Classification. The indicators shall be of the - following types: 100 percent RPM Indicated Engine 1 Engine 2 Engine 3 MS18099-1 Unlighted 4200 4200 4200
3、 MS18099-2 Lighted 4200 4200 4200 MS18099-3 Unlighted 3794 3794 3900 MS.1809 9-4 Unlighted 3900 2. APPLICABLE DOCIJMENTS 3900 2640 2.1 The following documents of the issue in effect on date of invitation for bfds or request for proposal, form a part of this specification to the extent specified here
4、in. SPECIFICATIONS Federal i BB-N-4 1 1 - QQ-C- 3 2 O QQ-N- 2 9 O Nitrogen Chromium Plating (Electrodeposited) Nickel Plating (Electrodeposfted) QQ-Z-3 25 Zinc Plating, Electrodeposited , Requirements for Beneficial comments (recommendations, additions, deletions) and any pertinent data which may be
5、 of use in improving this document should be addressed to: , Commanding Officer, Naval Air Engineering Center, ESSD, Lakehurst, NJ 08733, by using the self-addressed Standardization Document Improvement Proposal (DD Form 1426) appearing at the end of this document, Provided by IHSNot for ResaleNo re
6、production or networking permitted without license from IHS-,-,-MIL-I-Z3832A bb 77997Ob 0332280 b MIL-I- 23832A( AS) SPECIFICATIONS (Continued) Mi 1 it ar y MIL-P- 11 6 MIL-M- 3 1 7 1 MIL-E-52 7 2 MIL-C-554 1 MIL-S-6872 MI L-S - 7 7 4 2 MIL-A- 86 25 MIL-G-93 98 MIL- C- 14 8 O 6 MIL-C-254 67 MIL-C-26
7、48 2 MIL-G- 2 6 6 1 1 MIL-G-81704 MIL-B-81793 STANDARDS Federal FED-STD-595 Preservation-Packaging, Methods of Magnesium Alloy, Processes for Corrosion Protection of Environmental Testing, Aeronautical and Associated Equipment, General Specification for Chemical Films for Aluminum and Aluminum Alloy
8、s Soldering Process, General Specification for Screw Threads, Standard Optimum Selected Series, General Specification for Anodic Coatings, for Aluminum and Aluminum Alloys Generator, Tachometer, Two-Pole, High Temperature, Aircraft, Type ME-6 Coating, Reflection Reducing, for Instrument Cover Glasse
9、s and Lighting Wedges Lighting, Integral, Aircraft Instrument, General Specif ication for Connectors, Electric, Circular, Miniature Quick. Dis connect Generator, Tachometer GEU-7-A, Miniature Glass, Aircraft Instrument, Lighting Wedge and Cover Bearing, Ball, Precision, for Instruments and Rotating
10、Components Colors 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,- *NIL-I-23832A 66 W 7779706 OL322L W O STANDARDS (Continued) Military MIL-STD- 130 Identification Marking of U.S. Military Property MIL-STD- 143 Specifications and Standards, Order o
11、f Precedence for the Selection of MIL-STD-756 Reliability Prediction MIL-STD-781 Reliability Tests, Exponential Distribution s MIL-STD-794 Parts and Equipment Procedures for Packaging and Packing of MIL-STD-889 Dissimilar Metals MS18099 Indicator, Tachometer, Triple Pointer, Helicopter MS 24 367 Lam
12、p, Incandescent-Miniature Integral Lighting MS 2 45 15 Lamp Sub-Miniature Numerals and Letters, Aircraft Instrument Dial, Standard Form of Pointers, Dial, Standard Design of Aircraft Instrument (Copies of specifications, standards, drawings, and publications required by contractors in connection wit
13、h specific procurement functions should be obtained from the procuring activity or as directed by the contracting officer.) P 3.1 First article. When specified (see 6.2), the contractor shall furnish sample unit(s) for first article inspection and approval (see 4.3.1 and 6.2). 3.2 Selection of Gover
14、nment documents. Specifications and standards for necessary commodities and services not specified herein shall be selected in accordance with MIL-STD-143 except as provided in 3.2.1 and 3.2.2. 3.2.1 Commercial parts. Commercial parts having suitable properties shall be used, where on the date of in
15、vitation for bids, there are no suitable standard parts. In any case, commercial parts such as screws, bolts, nuts, cotter pins, having suitable properties, may be used provided: 3 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-I-23832A bb W 999
16、7Ob 0332282 T a. They can be replaced by the standard parts (MS or AN) without alteration. b. The corresponding part numbers are referenced in the parts list and if practicable, on the contractors drawings. 3.3 Materials. Materials shall conform to applicable specifications and shall be as specified
17、 herein. there are no applicable specifications, or which are not specifically described herein, shall be of the best quality, of the lightest practicable weight and suitable for the purpose intended, materials shall be encouraged to the maximum extent possible. Materials for which . The use of recl
18、aimed 3.3.1 Critical materials. Non-critical materials shall be used where practicable. to meet specification requirements, the material used shall be the least critical of those which are adequate for the purpose. shall be used for all parts of the tachometer indicator, except where otherwise speci
19、fied, Where the use of a critical material is essential 3.3.2 Non-magnetic materials. Non-magnetic materials 3.3.3 Metals. Metals shall be of the corrosive resistant type, or shall be suitably protected as specified herein to resist corrosion due to fuels, salt spray or atmospheric conditions, to wh
20、ich the switch may be subjected when in storage or during normal service life. 3.3.3.1 Dissimilar metals. Dissimilar metals as defined in MIL-STD-889, shall not be used in intimate contact with each other, unless suitably protected against electrolytic corrosion by means of protective coatings, meta
21、ls are in a sealed atmosphere as described in 3.4.3.2. Protective coatings will not be necessary if the 3.3.3.2 Magnesium alloy parts. Magnesium alloy parts shall be treated in accordance with MIL-M-3171. When abrasion resistance is a factor, an anodic treatment approved by the procuring activity sh
22、all be used, 3.3.3.3 Aluminum alloy parts, Where practicable, aluminum Small holes, pipe threads and case inserts need not be anodized. alloy parts shall be covered with an anodic film conforming to MIL-A- 8625. Aluminum alloys which do not anodize satisfactorily shall be coated with a chemical film
23、 in accordance with MIL-C-5541. 3.3.3.4 Iron and steel parts. Iron and steel parts shall be chromium, nickel or zinc plated in accordance with QQ-C-320, QQ-N-290 or QQ-2-325 respectively. requirements of paragraph 3.3.4, The class and type of plating shall meet the Provided by IHSNot for ResaleNo re
24、production or networking permitted without license from IHS-,-,-construction of the indicator are subjected to atmospheric or environmental conditions likely to cause corrosion in normal service life, they shall be protected against corrosion in a manner that will in no way prevent compliance with t
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