NAVY MIL-R-23761 B-1975 REGULATORS VOLTAGE AND CONTROL PANELS AIRCRAFT DIRECT CURRENT GENERATOR GENERAL SPECIFICATION FOR《飞机直流发电机控制面板及电压监视器的一般规定》.pdf
《NAVY MIL-R-23761 B-1975 REGULATORS VOLTAGE AND CONTROL PANELS AIRCRAFT DIRECT CURRENT GENERATOR GENERAL SPECIFICATION FOR《飞机直流发电机控制面板及电压监视器的一般规定》.pdf》由会员分享,可在线阅读,更多相关《NAVY MIL-R-23761 B-1975 REGULATORS VOLTAGE AND CONTROL PANELS AIRCRAFT DIRECT CURRENT GENERATOR GENERAL SPECIFICATION FOR《飞机直流发电机控制面板及电压监视器的一般规定》.pdf(35页珍藏版)》请在麦多课文档分享上搜索。
1、MIL-R-23761B 1 October 1975 SUPERSEDING MIL-R-237 6 1A (AS) 16 May 1974 MILITARY SPECIFICATION REGULATORS, VOLTAGE, AND CONTROL PmLS AIRCRAFT DIRECT CURRENT GENERATOR, GENERAL SPECIFICATION FOR This specification is approved for use by all Depart- ments and Agencies of the Department of Defense. 1.
2、SCOPE Scope - This specification covers solid state direct current voltage regulators or control panels used to regulate, control and protect aircraft engine driven direct current generators. - 1.1 . * 1.2 Classification - The regulators and control panels shall be of the following classes as specif
3、ied: Class A - Regulators and control panels that are operable under the temperature and altitude conditions of Curve II of MS33543. Class B - Regulators and control panels that are operable under the temperature and altitude conditions of Curve I of MS33543 to a maximum temperature of 85OC. Class C
4、 - Regulators and control panels that are operable under the temperature and altitude conditions of Curve I of MS33543. 2. APPLICABLE DOCUMENTS 2.1 The following documents, of the issue in effect on date of invitation for bids or request for proposal, form a part of this specification to the extent
5、specified herein. SPECIFICATIONS Federal QQ-P-416 Plating, Cadmium (Electrodeposited) THIS DOCUMENT CONTAINS 06 PAGES: Licensed by Information Handling ServicesMIL-R-237bLB bL 7777706 00887Y7 I MIL-R-23761B SPECIFICATIONS Military MIL-P-116 MIL-D-1000 MIL-M-3i 7 1 MIL-E-5400 MIL-C-5541 MIL-G-6 162 M
6、IL-S-7742 MIL-A-8625 MIL-S-8879 MIL-P-15 O24 STANDARDS Military MIL-STD-129 MIL-STD-130 MIL-STD-143 MIL-STD-454 2 Preservation-Packaging, Methods of Drawings, Engineering and Associated Lists Magnesium Alloy; Processes for Pretreatment and Prevention of Corrosion on Electronic Equipment, Airborne, G
7、eneral Specification for Chemical Conversion Coatings on Aluminum and Aluminum Alloys Generator, 30 Volts, Direct Current, Aircraft Engine Driven, General Specifi- cation for Screw Threads, Standard, Optimum Selected Series, General Specification for Anodic-Coatings, for Aluminum and Aluminum Alloys
8、 Screw Threads, Controlled Radius Root with Increased Minor Diameter, General Speci- fication for Plate, Tags and Bands for Identification of Equipment Marking for Shipment and Storage Identification Marking of U.S. Military Property Standards and Specifications, Order of Precedence for the Selectio
9、n of Standard General Requirements for Elec- tronic Equipment Licensed by Information Handling ServicesMIL-R-23761B STANDARDS Military (Continued) MIL-STD-461 MIL-STD-462 MIL-STD-749 Electromagnetic Interference Character- istics Requirements for Equipment Electromagnetic Interference Character- ist
10、ics, Measurement of Preparation and Submission of Data for Approval of Non Standard Parts MIL-STD-781 Reliability Tests: Exponential Distribution MIL-STD-794 ,Parts and Equipment, Procedures for Packaging and Packing of MIL-STD-810 Environmental Test Methods MIL-STD-889 DissimiAar Metals MS33543 Cri
11、teria Temperature and Altitude Range Self-Cooled Electric Equipment PUBLICATIONS NAVAIR AR (Aeronautical Requirements) AR-8 AR-9 AR-10 Versatile Avionics Shop Test System/ Avionics System Compatibility, General Requirements for Test Program Sets, General Require- ments for Maintainability of Avionic
12、s Equipment and Systems, General Requirements for (Copies of specifications, standards, drawings, and publications required by supplies in connection with specific procurement functions should be obtained from the procuring activity or as directed by the contracting officer). 3. REQUIREMENTS 3.1 Qua
13、lification - The regulator or control panel furnished under this specification shall be a product which has been tested and passed the qualification tests specified herein and has been approved for listing on the applicable qualified products list. 3 Licensed by Information Handling ServicesMIL-R-23
14、7bLB bL m 9999906 0088349 5 W MIL-R-23761B 3.2 Specification sheets - The individual regulator or control panel requirements shall be as specified herein and in accordance with the applicable detail specification sheet. In the event of any con- flict between requirements of this specification and th
15、e detail specification sheet, the latter shall govern. * 3.3 Design and construction - The voltage regulator or control panel shall conform to the requirements specified on the appli- cable detail specification sheet and this specification: lator shall be completely solid state and shall have no mov
16、ing parts. Component parts, design and construction shall enable the regulator or control panel to have a minimum shelf life of five years. reliability requirements shall be met after storage. or.contro1 panel shall not use any liquid, gas or vacuum, or device which depends upon elevated temperature
17、 for operation. The voltage regu- Performance and The voltage regulator 3.3.1 Materials - Materials shall be of a corrosion resist- ant type or suitably processed to resist corrosion. 3.3.1.2 Dissimilar metals - Dissimilar metals, as defined by MIL-STD-889, shall not be used in contact with each oth
18、er. contact is unavoidable, the metals shall be protected against electrolytic corrosion. When protection is used, it shall be of such a type that a low impedance path is offered to radio frequency currents. Where such 3.3.1.3 Non-metallic materials - Non-metallic materials used including plastics,
19、fabrics, and protective finishes shall be moisture re- sistant and shall not support fungus growth. ly affected by weather, sunlight, aircraft fluids, temperatures, and ambient conditions encountered during operation of the aircraft. Materials shall.not be adverse- 3.3.1.4 Flammable materials - Mate
20、rials which will support combusion shall not be used. Definitions and restrictions on the use of flammable materials sliall be in accordance with MIL-STD-454 Requirement 3. 3.3.2 Finish - 3.3.2.1 Aluminum alloy parts - Aluminum alloy parts shall be anodically treated in accordance with MIL-A-8625 or
21、 shall receive an approved chemical film in accordance with requirements of MIL-(2-5541. deposited by these treatments shall be removed from the actual contact area of all surfaces required to act as a path for electrical power and from the localareas under screws, nuts, or the like used for assembl
22、y or mounting purposes, to provide an adequate bonding connection. The films 3.3.2.2 Magnesium alloy parts - Magnesium alloy parts shall not be used without approval of the procuring activity, use magnesium alloy parts shall be surface treated in accordance with MIL-M-3171 to provide protection agai
23、nst corrosion. When approved for 4 1 “- Y, - I. . : 5% G Licensed by Information Handling ServicesMIL-R-237bIB 61 7777906 0088750 I E MIL-R-23761B 3.3.2.3 QQ-P-416, Plating - Cadmium plating shall be in accordance with 3.3.3 Parts, materials, and processes - 3.3.3.1 Use of standard parts - Standard
24、parts shall be used wherever they are suitable for the fulfilment of the design objectives and shall be identified on drawings by their standard part number. 3.3.3.2 processes shall be selected trom documents which are specified as standards in MIL-E-5400, Where there is no suitable document specifi
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