NAVY MIL-A-81083 C-1970 ALTERNATOR RECTIFIER (FOR TORPEDO MK 46 MODS O 1 2 AND 4)《MK 46 MODS O 1 2 和4鱼雷整流器发电机》.pdf

1、_.- ; Ji r . 1. pi- .- i. , r 3. . ._ . d 2 February 1970 Super sed ing 1-81083( os) 16 April 1969 i; MILIMY SPECIFICAl?ION TEXNATOR-REXTIFIER (For Torpedo Mk 46 Mas O and 1) This specification has been approved by the Naval Ordnance Systems Commnd, Department of the Navy 1. SCOPE 1.1 This specifica

2、tion covers.one type of brushless alternator- rectifier, referred to herein as the “alternator. 2. APPLICABLE DOCUMENTS 2.1 Government documents. 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 spec

3、ified herein. spANI1ARDS MILITARY . MIL-rn-l29 MIL- -130 DFAWINGS NAVAL 0RDI“CE SYSPE34.S COMMAND LD 546973 LD 269801 Wking for Shipment and Storage Identification Marking of U. S. , Militmy Property Alternator-Rectifier, and all docu- ments listed thereon (Torpedo Mk 4.6 Mod O) Alternator-Rectifier

4、, and all docu- ments listed thereon (Torpedo Mk 4.6 Mod 1) Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-A-81O83C ( OS) LD 269676 DL 1330516 LM 1330509 Dwg 2574648 PUBLICATIONS NAVAL ORDNUTCE SYSIEMS COMMAND $Ap 6024 Alternator-Rectifier, Ship

5、ping (Packing) Condition and an docu- ments listed thereon (Torpedo Mk46ModO) Alternator-Rectifier, chipping (Packing) Co1,ition and ail docu- ment s listed thereop (Torpedo Mk 46 Mod if Alternator-Rectifier and al1 docu- ments listed thereon (Torpedo Mk 46 Mod 1). Regulator, Alternator, Voltage Qua

6、lity Assurance Provisions for the Alternator-Rectifier (Copies of documents required by suppliers in comection with specific procurement functions should be obtained fromthe procuring activity or as directed by the contracting officer.) ification to the extent specified herein. issue in effect on da

7、te of invitation for bids or request for proposal shall apply. 2.2. Other documents. The following document forms a part of this spec- Unless otherwise indicated, the PUBLICATIONS CONSOLIDATED CLACSIFICATION COMMITTEZ Uniform Freight Classification Rules (Application for copies should be addressed t

8、o the Consolidated Classi- fication Committee, 202 chicago Union Station, chicago, Illinois 60606. ) 3.1 .Preproduction sample. Unless othem5se specified in the contract or order, the preproduction sample shall: (a) Be manufactured using the procedures proposed for production. 2 . - Provided by IHSN

9、ot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-A-L083C 13 W 7777706 0358568 7 I MIL-A-81083C ( OS) (b) Consist of two alternators. (c) Be tested as specified in Section 4 herein and is for the pur- pose of determining, prior to starting production, that the sup

10、pliers production methods are capable of yielding items that comply with the . technical requirements of the contract. 3.2 Basic requirements 3.2.1 Contractor-furnished data. . Data required by this specification, or by applicable documents referenced in Section 2, need not be furnished unless speci

11、fied in the contract or order (see 6.2). 3.2.2 Materials and treatments of materials and parts. Unless other- wise specified in the contract or order, all materials and treatments of materials and parts used in the manufacture of the alternator shall be in accordance with the requirements specified

12、herein and with the applicable documents listed in LD 546973, LD 269801, or LM 1330509, as applicable. 3.2.3 Gages. The supplier shall provide whatever gages ake necessary and adequate to ensure that the material and parts of the alternator will meet dimensions and requirements shown on the applicab

13、le documents listed in LD 546973, LD 269801, or LM 1330509, as applicable. When requested by the supplier, the procuring activity will furnish existing pertinent drawings of Naval final inspection gages for use only in the designing of the suppliers gages. responsibility for designing and manufactur

14、ing the gages needed for sat- isfactory fulfillment of the contract requirements. This action does not relieve the supplier of the 3.2.4 Inspection and test equipment and facilities. The supplier shall furnish and maintain all necessary inspection and test equipment and fa- cilities and shall provid

15、e personnel for performing all quality conformance tests. required quality conformance tests. The test equipment shall be adequate to permit performance of the 3.3 Performance requirements and physical characteristics 3.3.1 Performance. The alternator shall meet the performance require- ments specif

16、ied herein while operating at the indicated speeds and with the shunt field windings energized by an external power supply or a volt- age regulator , Drawing 2574648, as specified. 3.3.1.1 Alternating current output. The alternator shall provide 32 pius or minus 4 volts alternating current (vac) roo

17、t-mean-square (rms) with a frequency of 2000 cycles per second (cps) across a resistance of 1000 plus or minus 50 ohms at a rotor speed of 24,000 revolutions per minute (rpm) while being excited and loaded as in 3.3.1.2.1. 3 .I _. Provided by IHSNot for ResaleNo reproduction or networking permitted

18、without license from IHS-,-,-MIL-A-8iO83C( OS) 3.3.1.2 Direct current tutput using an external power supply 3.3.1.2.1 Steady state load. The aLternator, with a rotor speed of 20,000 rpm and the field excited with a current of 1.05 plus 0.20 or minus 0.35 -res by an extemal power supply, shall develo

19、p a potentid- of 40 plus or minus 0.3 volts direct current (vdc) average, from minus to common, across a resistive load of 10 plus or minus 0,5 ohms after a maximum of three pulses (see 3.3.1.2.2). from plus to comon SU be within plus or minus 1.0 vdc of the absolute value of the voltage, fromminus

20、to common, across a 10 plus or minus 0.5 ohm resistance. Slrmil“caneously, the potential 3.3.1.2.2 Pulse loading. The aJternator, after conforming to 3.3.1.2.1, sball respond to an additional pulsed load in accordance with the toler- ances of Figure IC. puise circuits aze to be nearmred at the refme

21、nce points of Figure 2. The pulse load resistance SU be 1.81 plus or minus 0.01 ohms, applied to the pulse circuit as a step function for a duration of 60 plus 10 minus 5 miiiisecons (ms). Both plus and minus voltages of the steady state and 3.3.1.3 Direct current output using a voltage regulator 3.

22、3.1.3.1 St;eay state loads. The alternator, with the shunt field excited by the voltage regulator (3.3.1)? shall develop the followin; potentials across the specified load resistances and at the specified rpm when measured at the reference points shown on Figure 3. . (a) oad resistance. 12 pius or m

23、inus 0.6 ohms resistance from the plus steady state line to common; 10 plus or minus 0.5 ohm resistance fromthe minus steady state line to common. (b) 16,000 rpm. At 16,000 revolutions per minute (rpm) the potential shal be 40 plus 1.0 minus 1.5 vdc across the 10 ohm resistance. tential across the l

24、2 ohm resistance shall be within 2 volts of that across the 10 ohm resistance. The po- (c) 20,000 rpm, At 20,000 rpm tbough 25,200 rpm the potential shall be 4-0 plus or minus 0.5 vdc across the 10 ohm resistance. potentid across the I2 ohm resistance shall be within plus or minus 1 volt of that acr

25、oss the 10 ohm resistance. - The The ripple voltage, measured from the steady Figure 3), shall not exceed 2 volts peak-to- peak. 4 . Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-. _ . . _ . -. - -. . - . . . _ MIL-A-BL083C 13 E 9979706 0358570 5 W

26、! MZL-A-81083C ( OS) 3*3.1.3.2 Pulse loading. The alternator, while conforming to 3.3.3.1.(), shall respond to an additiona puiseil oa of 3200 watts minimum In accordance wlth Figures la and lb vhen measured at reference pointsshuwn on Piwe 3. The puise load p hall. be applied to the pulse circuit a

27、t 0.5 plus or minus 0.1 second intervals for 30 pulses minimum before evaluation of performance. the pulse lines 60 cmn, shall not exceed 1.0 wltpeak-to-peakbe- tween pulses. speed for 5 minutes without abnormal vibration or damage while developing the following potentials: The potentid shall be 4.0

28、 plus 1.0 minus 1.5 vdc across the 10 ohm resistance. The potentidi. across the 12 ohm resis- tance shall be within plus or minus 2.0 volts of that across the 10 ohm resistance. The ripgle voltage, dasured from 3.3.1.4 Overspeed. The alternator shall be capable of a 27,000 qpm 3.3.1.5 Acceleration.

29、The E II Shock Schedule Duration (Milliseconds) 8.0 to 10.0 18.0 to 20.0 0.5 to 1.5 0.5 to 1.5 Ac celeration Direction* 3 fwd or aft axis 3 left or right axis 3 UP or down axis Long fwd axiE 3 up or down axis 3 right or left axis Long aft axi: impacts YSee Figure 4 for axes of alternator TABLE III 3

30、.4.5 Teqperature 3.4.5.1 Temperature, nonoperating and ready nonoperating. The alternator shall be capable of conforming to the requirements of this specification after being at any temperature within the range of minus 45 to plus i40 degrees F. 7 Provided by IHSNot for ResaleNo reproduction or netw

31、orking permitted without license from IHS-,-,-VI MIL-A-BL3C 13 = 79Ob 0358573 O i! MIL-A-81083C( OS) 3.4.5.2 Re-. The alternator shall be capable of conforming to the requirements of this specification after being at ny temperature be- tween O and plus 140 degrees F. 3.4.5.3 Operating temperature ra

32、nge. The alternator shall be cap- able of meeting the performance requirements specified herein while being subjected to an environment in which the anibient temperature rises from O to 250 degrees F in the first 2 minutes of operation and stabilizes at 250 degrees F for the remainder of a 10 minute

33、run, using sea water coolant as specified in 3.3.2. 3.5 - Life 3.5.1 Service life. The alternator shall have a minIImm service life of 7 hours under room Wient conditions. This shall consist of 42 duty cycles as shown in Figure 5. shall be without water cooling and the remaining 8 minutes shall be w

34、ith cooling in accordance Hth 3.3.2. tests contained in this document may, with the permission of the procuring activity, be charged to the operational service life of the alternator. The first 2 minutes of each duty cycle Operation during any of the rUnctiona1 3.5.2 Storage life, reay nonoperating

35、and ready. After storage of one dar minimum in the ready nonoperating or ready condition, the altehator, when connected t8 a voi.tage regulator, shall deliver the rated output (3.3.1.3), by self-excitation, within 0.5 second after reaching 16,000 rpm. 3.5.3 Storage life, nonoperating. The alternator

36、 shall meet the per- formance requiremats specified herein after storage of five years mini- m in the nonoperating condition and after the reestablishment of the required level of residual magnetism. 3.6 Identification. The alternator shall be identified in accordance with MIL-sTD-l3O and the applic

37、able documents listed in LD 546973, 269801, or LM 1330509, as applicable. 3.7 Worlnnansbip. The workmanship and finish shall be of sufficiently high grade to ensure satisfactory operation consistent with the require- ments of this specification. thoroughly clean and free of excess materials, chips,

38、and loose or splattered foreign niaterids. any approved preproduction sangle, subject to any qualifications stated in the Governments notice of approval, shall be determinative of the contract relative to workmanship insofar as not specifically covered by the applicable specifications. All pts used

39、in the assembly shall be The standards of workmanship exhibited in 8 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-A-81083C( OS) 4. QUALITY AS-CZ PROVISIONS 4.1 Responsibility for inspection. Unless otherwise specified in the contract or Durcha

40、se order, the supplier is responsible for the perform- ance of all inspection reqbementi-as specified herein. wise specified in the contract or order, the sqpplier may use his own or any other facilities suitable for the perforpmcq oftthe inspection re- quirements specified herein, unless disapprove

41、d by the Government. The Government reserves the right to perform any of the inspections set forth in the specification where such inspections are deemed necessary to as- sure supplies asid services conform to prescribed requirements. lkcept as other- 4.2 Classification of inspection. Inspection of

42、the alternator shall be classified as follows: I (a) Preproduction inspection (i) Preprouction sqle (see 4.3;i) (2) Beprouction tests (see 4.5) (b ) Periodic production inspection (1) Periodic production sampling (see 4.3.2) (2) Periodic production tests (see 4.6) (c) mity conforniance inspection (i

43、) (2) Wity conformance sampling (see 4.3.3) Qua.ity conformance tests and examinations (see therefore, there shall be no sampling plan for acceptance. shall. be rejected. Defective units 4.4 Test conditions. Unless otherwise specified, the alternator sul be subjected to tests under the following con

44、ditions: (a) Temperature: Room mbient (60 to 95 degrees F). (b) Humidity (relative): Room Wien%, up to 95 percent. (c) Coolant (clean tap wter): Temperature 60 plus or minus 15 de- grees F, flow rate 1.5 plus or minus 0.3 gpm. 10 Provided by IHSNot for ResaleNo reproduction or networking permitted w

45、ithout license from IHS-,-,-MIL-A-L083C 13 m 9999906 0358576 b m MIL-A=81083C( OS) 4.5 Preproduction tests. The alternators within the preproduction sample lidentified 8s alternator nurtibers 1 and 2) shall be subjected to the preproduction tests as specified in Table IV. Certified inspection data c

46、overing the results of preproduction tests shall be foswasded to the Nad Ordnance Systems Comand. sist of the following: Certified inspection data shall con- (a) (b) (c) (a) Date of tests an n-s of persons?conucting tests. Run or test plan used. Serial number of the alternator. Test results of prepr

47、oduction tests (4.5.2 through 4.5.5). wu IV Preproduction Test Schedule Te st Nuniber 1 2 2 5 6 7- 8 .9 10 Test Description Quality conformace tests and examinations (w 6m4) Minimum rpm operation (16,000) (4.5.2) Overspeed (4.5.3) OperationaL temperature test (4.5.4ii) Temperature, storage (4.5.4.2)

48、 Acceleration (4.504.3) Vibration (4.5.4.4 Shock (4.5.4.5) Quality conformance tests and examinations (QAP 6024, except paragraph 20.6.1) -ration=A-81083c ( OS) and exminations, subsequent to the environmental tests, constitutes a failure. 4.5.4.1 Ope rationus:2 degrees F and start For the n-A-81083

49、C( OS) 4.5.4.4.2 Reay nonoperating and reads The unpackaged alternator, mounted on a support frame, see Figure 4, shall be rigidly attached to the vibration equipment. n-Us support frame shall be capable of trans- mitting the vibrations listed in Table I to the alternator, along the Saris, shown in Figure 4. The alternator shall be subjected to 180 minutes of cycling vibratio