AIR FORCE MIL-T-9157-1953 TACHOMETER ELECTRIC TYPE E-15 (FOR AIRCRAFT TURBO SUPERCHARGER)《E-15型(涡轮增压器)电力转速计》.pdf
《AIR FORCE MIL-T-9157-1953 TACHOMETER ELECTRIC TYPE E-15 (FOR AIRCRAFT TURBO SUPERCHARGER)《E-15型(涡轮增压器)电力转速计》.pdf》由会员分享,可在线阅读,更多相关《AIR FORCE MIL-T-9157-1953 TACHOMETER ELECTRIC TYPE E-15 (FOR AIRCRAFT TURBO SUPERCHARGER)《E-15型(涡轮增压器)电力转速计》.pdf(11页珍藏版)》请在麦多课文档分享上搜索。
1、HILITARY SPECIFICATION 1.1 TUS upcification covers one type of ramota incating, electric, ircraft, turbo supercharger tachometer, range 0 to 35,000 rpi, with built-in djustable contaots designed for u80 with an extarnal waning lamp, dedgnatod gpe E-15. APPLICABLE SPECIFICATIONS, STANDARDS, ANDLICATI
2、GNS 2.1 The foliowing specifiaatlme, stsndarcb, and publication, of th 804 In effect on date of invltatioli for bids, form 8 part of thir qmdfiuati#r B the extent specified hereint SPECIFICATIONS MILITAM . MIL-sm129 mricing of Shlprusnts -T01i30 Idmtification Harking of U. S. PKiitarg Propsrty * AIR
3、 FORCLNAVP AERONAUTICAL m553 Gemerator - Electric Tachomotsr ANmoo66 ANRldrOO AM1OLO1 Case - Stand Mnisqsians for 2-3/4 Dia1 Instntasnt L * Receptacle - Electrical Connector, Inhgral Haunting hnaral8 and Lettara - Iliraraft instrument md, Standnrd Forra Of (Without Sump) 3 ,. L. o Provided by IHSNot
4、 for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-9357 66 W 9999906 0327076 -2- IIIL-T=9157 (USAF) PUBLICATION AIR FORCE-NAW AERONAUTICAL 405 Storage Life - Aeronautical ArtAcles . (Copies of specifications, standards, and publications required by contzactors in c
5、onnection with specific procurement functions should be obtained fra the procuring agency or as directed by the contracting officer.) 3. REQUIREMEEITS 3.1 The rquirementa specified in Specifications MIL-F-su3 and MIL-1-709 3.1.1 Where the requirements of the general specification and this 3.2 Design
6、 and constructiont 3.2.1 Tachometer.- The tachmeter shall consist of an indicator and are appl$.cable as general requirements of this specificrtion. specification conflict, the requirements of this specification shall govern. one tachometer generator. 3.2.2 Indicator.- The indicator shall be in acco
7、rdance with Specification 3.2.2.1 Case.- The case shall be in accordance with Standard AND10401, Mn-1-7098. except as shown on Figure 1. accordance with Specification MIEa-skl3. The mounting arrangement for the generator shall be in accordance with Specification NiL4=sierals.- !lunerals shall distin
8、ctly indicate the graduation to Any confusion resultinr? in doubt as to which graduation wldch each applies. the numeral apply will be cause for rejection. IrWn several rnunerals are used in one mp, the space between shall not be less than y64 inch. be finished in fluorescent-luminescent material in
9、 accodnce with Specification 3-1-1, Color ?io. 650 The dimensions of the markings shall be as follows 3.2.8.2 Fluorescent-luninescent material.- The following markines shall iiumerals 15, 20, 25, and 30 Graduations at 10, 15, 20, 25, Lettering, turbo RpEI 190 RPE maduations from 15 to 30 Letterinp,
10、thousands. ?werals O, 5, 10, and 35 Graduations at O, 5, and 35 100 RYTI Waduations from O to 15 and from 30 to 35 and 30 Height or Length, Inch 1/4 7/32 min. 5/32 min. 7/32 min. 5/32 1/16 . v4 5/32 min. Ilidth of Lhe or Graduation Inch kO.005 1/32 1/32 1/32 .O20 1/64 1/32 1/32 . .o20 , o Provided b
11、y IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-3.2.C.3 Durabledull black.- The f oilowin? rsarldngs shall be permanently and legibly marked on the dial in durabl
12、e dull black. The heicht of the maricings sh.11 be cis follows: Height, Inch USAF l/i6 3.2.9 Finish.- The background of the dial and the unsbded part of the 3.3 Identification of product.- Equipment, assemblies, and parts shaU Type d-15 1m pointer shall be finished in durable dull black, be marked f
13、or identification in accordance with Standard IlIL.TW3.30. b SATPLIUG , INSPlXTIOIJ, AX.) TEST PROCEEJRES 14.1 The.tachometer indicator shall be subjected to inspection and test8 in accordance Hi th SFecification 1.11L-I-7091.1.1 The speed at which the lamp lights shall be within S5 rpm of the cut-i
14、n speed specified herein. shall not be greater than 150 rpm below the cut-in speed, as determined in the preceding test, The sped at which the lemp goes out 4.4.2 Sampling tests.- Five indicators which have been manufactured under eseentcially the same conditions shall-be selected at rand tests are
15、Specified on a number of indicators that am selected as representative of a certain lot, and one or more of this number fails to meet the specified tests, acceptance of all indicators shall be withheld until the extent and cause reasons, individual tests may be continued pending investigation of a a
16、aj.ng test failure, but the final acceptance of the indicator is contingent.upon the inspectors decision recarding the over-all conformance of the indicator to specification requirements. exist on indicators previously accepted, full particulars concerning the defects found, including recommendation
17、s for correction, will be furnished to the Procurlng Aeency, failure is detemined. For operation If investigation indicates that the defects may J.j.,2.2 Lou temperature test =3SoC.- The indicator shall be subjected to a tanperature of -35.C for a period of one hour and then subjected to the operati
18、on test, at this temperature. vary more than 1s rpm fran those specified in the operation test at room temperature, unless within rom temperature tolerances. The cut-in and cutrout points shall not 4.L.2.3 Hirh temperature test.- The indicator shall be subjected to a temperature of k7l.C for a perio
19、d of one hour and then subjected to tho operation test, at this temperature. The cut-in and cubout points shall not vary more than 25 rpm from those specified in the operation test at room temperahre, unless within rom temperature tolerances. The average change in pointer readings obtained from this
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- AIRFORCEMILT91571953TACHOMETERELECTRICTYPEE15FORAIRCRAFTTURBOSUPERCHARGERE15 涡轮 增压 电力 转速 PDF

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