AIR FORCE MIL-E-26248 A-1972 ENGINES GASOLINE GROUND USE PACKETTE GENERAL SPECIFICATION FOR《袋装地面使用汽油发动机一般规格》.pdf
《AIR FORCE MIL-E-26248 A-1972 ENGINES GASOLINE GROUND USE PACKETTE GENERAL SPECIFICATION FOR《袋装地面使用汽油发动机一般规格》.pdf》由会员分享,可在线阅读,更多相关《AIR FORCE MIL-E-26248 A-1972 ENGINES GASOLINE GROUND USE PACKETTE GENERAL SPECIFICATION FOR《袋装地面使用汽油发动机一般规格》.pdf(30页珍藏版)》请在麦多课文档分享上搜索。
1、!:ILITARY SPECIFICACIOR EBGI$iE_:S, GAEOLIHE y Gi?OUI?D IJUE P/CKEX!l?E, GEXXl1AL SPECiFICATIOA FOI? 1. SCOPE 1.1 ; docwnents of the issue in effect on date of invitation for bids or request for proposal form a part of this specifkxtion: SPECIPICATIOKS Federal KIL-P-114 HI L-D- 10 O O : IL-c- 3703 P
2、1 tinc, Cadmium (El ctrodeposit 5) 7 !namel, ALkyd, MOSS (For FXterjor Anci Interior Firfaces ) Priver Coatin;, P.lkyd hod And Ferrous ?et a 1 Gasoline Automotive Gasoline, Autorotive, OW Leaded Or Gn 1 e ?-de d ?reservat%on, !ethoas Of Lirawiny;s Inpineerinp_ And Associated Lists Lidx-icati nc 05.1
3、, Intemp 1. Combust ion %,rine, Tectica.1 Yervice ksoline !.tomot.ive Corbat YaCgnesiim Alloyy Precesses For Pretreatmint And Orevention Of Corrosion On Cable, Power, ?Ckctrical; f,rnition, Ilicti-Tensi on EnvironPenta1 Iesting , Aerotmutical And Associated l!qiriprent, General Cpe ci f i c at ion F
4、or Chemical Conversion Coatings On Alurinm An(? AluTinurn Alloys Gsicoline , Aviatior! : Sratles 30/87, ioo/im, 115/1h5 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,- MIL-E-2b24A 28 !,:I 1,- I!- R79 5 SIIL- E-lOOC2 i.33.t ary I!IL-STI)- 4 80 Air Fo
5、rce -Xavy Aeronaut ad Equipxxent Procedures For Packaging And Packing Of Test Reports, Preparation Of ni ssi”:il.ar Yet als Clisliioning . finchorinE, Bracing, Rlockinp, And Waterproofing; Vith Apyropri nix Ties t !-lethods Vaaor Pressure Chart (Copies of specifications , standards, drawings , and o
6、ublications required by suppliers in connection with succific procurement functions should be obtained from the Drocuririn activity or as darected by tnne contracting officer. ) * 2.2 ? holes shall have helical coil thread inserts. or equivalent. Tubular steel removable pushrod. housinys shall be re
7、tained in the cylinder head by sprinl: pressure and scaled to the crankcase mounted flanges by special synthetic-rubber seals. Pushrods shall be tubulsr stpe alloy with hardened-steel ball ends. Valve rockers shall be alloy-steel forsinEs hardened on wearing surfaces , equinped with bronze bushings,
8、 and drille? for pressure lubrication of the bushings. Valves shall be alloy-steel forgings with hardened tips. The exhaust-valve faces shall be coated with Stellite Wo. 6 alloy, or equivalent. Rocker sha.fts shall be seamless alloy-steel tubes, ground to size after hardening. Positive valve rotator
9、s on the outer spring ends shall he locked to valve-sten grooves by hardened, split conical keys to rotate the valves slightly each cycle. * 3.11 Pistons m_d_-npA. Pisfons shall be aluminum-alloy castings of frill trunk desir;r? machined wit5 necessary ricg grocves to properly control oil usage WIE
10、i:rev2nt co:.;r?ssior, 1eiiks;c xiLti mixklrn YV ar,d ring sticking. The pistor, skirt shall be cm groucd to fit the circular cylimier walls with adequate contact area at normal cylinder operatifig temperature. ?he pin bore shall be finished to a surface roughncss of not more than 2 microinches, roo
11、t nean square (rmc), and truly square with the piston axis. of oistons of any gi-xm part nu?:ker shnll v:ary not more thcm one-half ounce. Only a single type anci part number of piston shall be used in my pck-ette engine Rodel. Piston pins sfia.11- e of scaxleus alloy-steel tubinr, shall be carburiz
12、ed, shall !lave ah-iizix: e:d. ;ilugc pressed in I or alz*.i tim: 3-zo:x.j.: plugs forrise contac?, arid shnll be rachined before center- less grinding and polishir?g of tke pins. Piston rincs shall be fabricated from the best quality, close-grained, piston ring cast iron. The top com;iression ring
13、shall be of the centrifugal cast type or equivelent. P.1.1 rings shall be rr,olybdenun faced to resist scuffing and increase ring life. shall be of the center-slotted type with circw.ferentia.1 e-Ganders . The weights Oil control rings 3.12 ghAuEt-sxs+ two sinple exhust pipe assemblies, one attached
14、 to the exhaust port of each cylinder. Xode1.s havins Cour or more cylinders shaU be eqiiipped with two exhaust manifold assemblies. one a.ttachec1 to each bank of cglinders. A heat- resistant gasket shall be installed betveen each pipe attaching flange and the cylinder port pad to seal the joint. F
15、a.ch flanre shall be attached hy brass hex nuts to twc c:rlinder ctucls. Rach exhaust pipe or manifold assembly shall be constructed of corrosion-resistant steel or e$iivalent metal selected to withstand exhaust, gas heat and corrosive pffect,s. Tach pipe shall be cut from seamless tubing, and each
16、attaching fimge shall be fabricatea of flat s%ock o? sufficient thickness too resist warning under attaching nut bendinc stresses. Attachi.nF; flanges shall be joined to pipes and pipes shall ,joined torether to fom mnifolds, when required, by continuous welds made as specified in 3.28.6. assemblies
17、 shall be capable of withstmdjn(- corrosive effects and exhaust g,as temperatures throu*out the period of operation specified in 3.6.2 vithout Any nodel havinfi only two cylinders may be equipyed. with Fxhaust Fipe and manifold 7 - . . Provided by IHSNot for ResaleNo reproduction or networking permi
18、tted without license from IHS-,-,-leakage, cracking, scrioirs erosion of any surface, or distortion to such extent as to make removal or installation difficult. single manifold would produce excessive linear thermal expansion, it will be permissible to construct it of two riKifi sections joined by a
19、 suitahle, gastight clamp or other connecting device that will have the scame durability as the manifold section, will not unduly interfere with cooling 8.i circulation alonp the manifold, arid will relieve the stress of linear expansion on cylinders and on manifold sections. difficulty in disassemb
20、ly due to corrosion, seizure, or other forms of deterioration. Each exhust oipe and manifo1.d shall extend outside the cylinder cooling shroud a short distance to permit connection of an exhaust gas collector systerr. -fitting met81 jacket of such desian as to allow a continuous flow of cooling .ir
21、around the pipe or manifold fromthe enqine cooling fan to a point outside the cooling air shroud, provided that the length of such pipe or manifold within the shroud exceeds 6 inches. Exhaust manifold cooling air jackets shall be designed to p.ern5.t easy removal without disassembly of major portion
22、s of the cooling shrouds or removal of other major engine parts. shall. be constructed of corrosion-resistant naterials or their surfaces shn11 be treated to resist corrosim at the temperature attained in full load and rated speed operation throuph the period specified in 3.6.2. 3.13 Lubricatjornry$
23、gm. A force feed lubrication system shall be employed. The oil shall be stayed in, drawn from, and returned by gravity to a wet-tpe sump. engine passages by a positive displacenent pump with a.d.enuRt,e capacity to supply all pressure lubricnted arts under a11 onerating conditions syecified herein.
24、prevent the entrance of dangerously laxge particles. The intake shall be lower than the minimum safe oil level at my 8.ny;le of tilt specified in 3.6.3. An oil filter, as specified in 3.13.3, shall be -laced bettTeen the oil pump and all lubricated points in the enrine. One or more nressure relief v
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- AIRFORCEMILE26248A1972ENGINESGASOLINEGROUNDUSEPACKETTEGENERALSPECIFICATIONFOR 袋装 地面 使用 汽油 发动机 一般 规格 PDF

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