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The concepts listed below are shown in Figure 5
/ B0 X5 D$ r3 i4 k6 P. G# T- varying topdeck thickness9 V) x- l1 I: t( J
- varying liner thickness
5 S9 r5 @4 z% F n1 A- horizontal trussbar are integrated to the topdeck) |" R* I/ E4 g7 j; B/ v1 T8 x3 E
- vertical trussbars act as oil return and blow-by passages% V! \( }# Q: \9 O* }4 L9 d3 A
- thread bosses for the cylinder head are integrated to the water jacket deck
- N% O" u8 h! O: E. u- reduced thread depth
9 t' a& c$ n2 {' q' K7 s* {) G. o& F+ D-- decreased water jacket height
2 D: l6 L2 t8 @: l8 M1 O- wide crankcase venting holes: D# h' i P, Q( _- C; y: q M
- hollow main bearing walls
! t @( L7 b4 W9 e5 q! z- u. K# H- reduced oil pan flange thickness: L+ J: @2 z. g8 z0 q
- bearing cap designed as U-profile, H1 _4 V% B: R" d- N
9 ^9 y2 D" K! O7 |
红色的字翻译不准,我做的是才柴油机机体设计 先谢谢了 |
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