NAVY MIL-E-7016 F (1)-1981 ELECTRIC LOAD AND POWER SOURCE CAPACITY AIRCRAFT ANALYSIS OF《飞机电力负荷与电源的容量的分析》.pdf

1、MIL-E-7016FAMENDMENT 118 March 1981and2.1MILITARY SPECIFICATIONELECTRIC LOAD AND POWERSOURCE CAPACITY, AIRCRAFT, ANALYSIS OFThis amendment forms a part of Military SpecificationMIL-E-7O16F, dated 20 July 1976, and is approved for useby all Departments and Agencies of the Department of Defense.PAGE 1

2、Bottom right hand corner showing the FSC: delete “MISC“substitute “1680”.PAGE 2under STANDARDS, MILITARYMIL-STD-704: delete the title “Electric Power, AircraftCharacteristics and Utilization of” and substitute “AircraftElectric Power Characteristics.”PAGE 143.5.4.4.3 add a new sub-paragraph as follo

3、ws: “f. ImpedanceLosses Factor. For AC systems for whcih the nominal rating isspecified in volt-amperes or watts (or KVA or KW) at the electricconnections of the generator and the potential is regulatedelsewhere, the impedance losses factor is the ratio of the nominalpotential at the point of regula

4、tion to the nominal potential atthe electric connections of the generator at rated load. (Thisratio is usually 115/120, or 0.96). If the nominal rating isspecified in amperes or at the point of regulation or both, theimpedance losses factor is one (1).”PAGE 16Add New Paragraph:“3.5.5.1.3 Battery cha

5、rging. Ananalysis of battery chargingeffectiveness shall be made to show battery state of charge versuscharging time, assuming that the battery is completely dischargedwhen charging is initiated.” The most adverse battery temperatureshall be assumed in making the analysis.Preparing ActivityNavy - AS(Project No. 1680-0473)Custodians:Army - AVNavy - ASAir Force - 11 *U.S. GOVERNMENT PRINTING OFFICE: 1981 - 703-023/1785Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-