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Aviation History
1918
1918 - 0998.PDF
MW**£Z£*r\ SEPTEMBER 5, 1918. CAM DIAGRAMS FOR 300 H P MAYBACH AERO ENGINE 1 • * x c « •0 10 KX 30 , e0 0 - ST t —- o 1— I—fr-fty 5o kJ '—1— 0 i N U1- k •0 ; 1 ij3 2 Ss J 1 1 s0 60 INI FT/ ANCE • 0 fl 1 it ir1- T- K) 3 0 K 0 0 0 1\o 1 o 8 a f w a > 7 6 S 4 3 2 «P A) •oo 90 £ 80 XHAU5T io *** i 90 0 30 VELOCITY --- ?l0 •^ "1 .K CURVE i V 0 / TAN o • h- 6 99 • | 30 «0 * in *** INLET o 0 —J 0 90 lOO I yHV U•0 O AT ANY 0 *° 7 6 5 . 3 * •90 . 17. EXHAUST ACCCLLRATION CURVE UHf,.IM0.(''^f.la: r.«.5« o,-s« INLET fc-tNCt o» VcLOCirrCl/uve TO HM,I0Ni«t »T «»T «3«T t?O HO IOO 3O JO 20 K> O 20 3O 40 JO 6O 70 60 SO 100 "0 (0O I3O 140 190 Fig. 18. 016 •; \ .EAR* MCE ON IN -£T »J0 ffOt'O « 1)0 i« ,« BO . 1* WO TO SO JT 40 JO »K»0»» SO 40 30 M TO no no m MC r*o zso DIAGRAM OF EXHAUST AND INLET PORT OPENING IN RELATION TO PISTON VELOCITY. VR -3-6. Fig. 19. ......•;., -..;.. -. • • .. Fig. 20.—Crankshaft. ~ •-•---::..: ,'••- :-J .•-/'..,?.- '-' :~z~\- ".•-'.•.•"'/•••---^ some natu ,-e, apparently to prevent corrosion. This form of Ka/ve rockers.—The roller bearings carrying the spindles ofgalvanised exterior finish is carried out on several other parts the valve rockers are mounted in short brackets, each of of the engine. which is attached to the cylinder heads by two 8 mm. studsDetails of the valves and valve springs are given in and castellated nuts. The bearing brackets are steel drop Figs. 13, 14 and 15. forgings, and the roller races are, to a certain extent, per- 998
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