ARMY MIL-E-50739-1973 ELECTRONIC COMPONENT ASSEMBLY 11738818 (CHARGE CONTROL)《11738818(充电控制)电子元件组件》.pdf
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1、MIL-E- 5 07 3 9(MU) 8 August 1973 MILITARi- SPECIFICATION ELECTRONIC COMPOSENT ASSEMBLY: 11738818 I CHARGE CONTROL) This specification is approved for use by all Departments and Agencies oi the Department of Defense. 1. SCOPE 1. 1 This specification covers one type of electronic component assembly k
2、nown as Component -4sseembLy: (see 6.1). 11738818 (Charge Control) 2. APPLICABLE DOCLXENTS 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 specified herein. SPEC IF ICA TIONS Military MIL-F-1
3、3926 . Fire Control Materiel: General Specification Governing the Manu- facture and Inspection of MIL -I- 456 07 Inspection Equipment; Acquisition, Maintenance, and Disposition of MIL-S-45743 Soldering, Manual Type, High Re liability Elect rical, Electronic , Instrument , Communication, and Radar fo
4、r Aerospace and Control Systems , Procedure for FSC- 1240 _ THIS DOCUMENT CONTAINS PAGES. 8 Licensed by Information Handling Services_ MIL-E-50737 LE 7777706 0330424 8 MIL-E - 5073 9( MU) 8 August 1973 MIL-s -4681-1- Solder Bath Soldering of Printed Wiring Assemblies, Automatic Machine Tape STANDARD
5、S Military MIL-STD- 103 MIL-STD- 1 O9 Sampling Procedures and Tables for Inspection by Attributes Quality Assurance Terms and Definitions MIL-STD-31 O Environmenta 1 Te s t Methods DRA WINGS U. S. Army, Trankford Arsenal F1173881 b Electronic Component Assembly; 11738818 (Charge Control) PACKAGISG D
6、ATA SHEET 11738818 Packaging of Electronic Component Assembly; 11738818 (Charge Control) (Copies of specifications. standards, drawings, and packaging data sheets required by suppliers ir. connection with specific procurement functions should be obtained fror. the procuring activity or as directed b
7、y the contracting officer. ) 2 Licensed by Information Handling ServicesMIL- E - 5 O 73 9 (MU) 8 August 1973 3. REQUIREMENTS 3. 1 Fabrication, The electronic component assembly, herein referred to as the assembly, shall be manufactured in accordance with Drawing F11738818 and drawings pertaining the
8、reto. 3.2 General specification. The assembly shall meet the follow- ing requirements, where applicable, of MIL-F- 13926: a. Order of precedence b. Dimensions and tolerances c. Part identifica tion and marking d. Electrical and electronic assemblies e. Workmanship. 3.2. 1 Soldering. Soldering shall
9、be in accordance with MIL-S- 45743 or MIL-S-46844, except that bare copper wire exposure shalt be permitted at clipped ends of component leads. 3.3 Performance, Unless otherwise specified, the assembly shall meet the performance requirements of this specification at standard ambient temperatures bet
10、ween 60 degrees Fahrenheit (OF) and 90F. 3.3.1 Loads, power, signal, and interconnections. The assembly shall perform as specifvd herein when the loads, power, signal, and inter- connections of table I are applied as specified. 3.3.1.1 Low/high battery voltage charge current. With the power source (
11、item 2. 1) of table 1 applied o Pl-24 and adjusted to +24. O *2. O Volts direct current (Vdc), and with the load (item 1. 1) of table I connected, the current flowing through the specified Load shall be 200 I80 miltiamperes (mA). With the load (item 1. 1) of table I disconnected and with the load (i
12、tem 1.2) of table I connected, the current flowing through the specified Load shall be 200 *80 mA. 3.3. 1.2 Charger voltage regulation. With the power source (item 2. 1) of table I applied to Pl-24 and adjusted to +24. O *Z. O Vdc, and with the load (item 1.3) of table I connected as specified, the
13、voltage of Pl-4 shall be t43. O *4. O Vdc. P1-15 connected to Pl-16, the voltage of Pl-4 shall be t36. O *3, O Vdc. With the above conditions existing, and with 3 Licensed by Information Handling ServicesMIL-E-50737 12 H 9779706 0330426 L H MIL- E - 5 073 9 (MU) 8 August 1973 TABLE I LOADS, POWER, S
14、IGNAL, AND INTERCONNECTIONS item 1. 1.1 1.2 1.3 1.4 1.5 2. 2.1 2.2 2.3 3. 3.1 4. Cond ition s Loads Resistor Resistor Re sistor Capacitor Re sis to.r Power sources +l7 to t31 Vdc t5 Vdc -6Vdc Signal Source Voltage. source Inte rcon - ne c t ion s C ha r ac t e r ist ic s 51 ohms (Q)I5 percent 13052
15、*5 percent 3008 *5 percent 100pf *20 percent 75 Vdc working voltage 10 kQ *5 percent Ad jus table Ripple: SO. 1 Vrms Tolerance: *0.2 Vdc Ripple: S25mVp-p Tolerance: *O. 2 Vdc Ripple: 5 25MVp-p Waveform as shown in figure 1. Source imped- ance 100Q *5 percent 4 Connections Connected between the follo
16、wing pins: P1-4(+) and P1-7( -) when specified herein P1-4(+) and P1-7( -) when specified herein P1-4(t) and P1-7(-) when specified herein Pl-4(+) and PI -7(-) P1-8(t) and P1-7(-) Applied between P1-24(+) and P1-7(-) except as specified he re in. Between P1-12(+) and Pl-7(-) Between P1- 11 (-) and P
17、1-7(+) Applied to Pl-5, and Pl-6 as shown in figure 1 PI-15 and Pl-16 when s pe cif ied her ein, P1-10 and P1-7 Licensed by Information Handling Servicesr P1- 5 L MIL-E-50739 12 m r17999Ob 0430733 b m - - - - - - to.2 *0.2v MIL- E - 5 07 39 (MU) 8 August 1973 4 3. 3. 1, 3 Input voltage /charge curre
18、nt regulation. With the power source (item 2. 1) of table 1 applied to Pl -24 and adjusted to t18. O *Os 5 Vdc and then t30. O IO. 5 Vdc, and the load (item 1.2) of table I connected as specified, the current flowing through the specified load shall be 200 I80 mA for each input condition. to. 2 *o.
19、2v - 3. 3. 1.4 Charger sense voltage. With the power source (item 2. 1) of table I applied to Pl -24 and adjusted to t24. O rt2. O Vdc, and with the load (item i. 2) of table I connecte-d as specified, the voltage at P1-8 shall be equal to the voltage at Pl-4 within *l. 5 Vdc. 3. 3. 1. 5 Charge enab
20、le signal. With the power source (item 2. 1) of table I applied and adjusted to t24. O 12. O Vdc, with the load (item 1. 2) of table I connected as specified, and with P1-10 disconnected from P1-7, the current flowing through the specified load shall be O 110 mA. 5 Licensed by Information Handling S
21、ervicesMIL-E-50737 12 = 7977706 Oq30734 8 e MIL- E - 5 073 9(MU) 8 August 1973 3.3. 2 Environmental 3. 3.2.1 Storaue temperature. The assembly shall meet the require- ments of 3. 3. 1 at ambient temperature after exposure to and thermal stabilization at -80 OF and tl60 “F. 3. 3.2.2 Operating tempera
22、tures. The assembly shall meet the requirements of 3. 3. 1 while exposed to and thermally stabilized at -40F and +125OF, subsequent to which the requirements of 3.3. 1 shall be met at ambient temperature. 3. 3.2.3 Vibration, The assembly shall show no physical failure and shall meet the requirements
23、 of 3.3. 1 after being exposed to tbe follow- ing vibratory conditions: a. Amplitude: b. Vibratory motion: c. Sweep time: d. Vibration cycling: 1/64 inch, constant (1 /32 inch double amplitude) Simple ha rmonc 5 to 55 to 5 Hertz in a 5 -minute period Three linear or logarithmic sweeps applied to eac
24、h of three mutually perpendicular axes. 6 las s i- .i ca t ion 101. 102. 103, 104. 105. TABLE II FUNCTIONAL TESTS Characteristic Low/high battery voltage charge current C ha r ge r voltage regulation Input voltage /c ha r ger cur rent regula tion Charger sense voltage Charge enable signal 8 I Requir
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