|
The concepts listed below are shown in Figure 5
1 B6 r1 `! o- c( e, @, m- varying topdeck thickness8 R: H: r0 w0 Y. Q
- varying liner thickness: x/ L5 o! {3 @: C9 A
- horizontal trussbar are integrated to the topdeck
& z& J5 U* p% \6 \- vertical trussbars act as oil return and blow-by passages
6 W( X' g+ Z2 H3 a) D5 j% b3 c- thread bosses for the cylinder head are integrated to the water jacket deck
: z$ y) k3 t, |; Y- reduced thread depth, F4 K* b \6 s5 g, E3 ?
-- decreased water jacket height# x3 h) F* |% }- S
- wide crankcase venting holes
- V' ?$ w) j2 ]: o4 [/ ]5 R% t- hollow main bearing walls
; X& r+ Z2 {) k7 i; Q4 r' t+ c; v# L- reduced oil pan flange thickness
0 E! q7 A( J! I& Y# f- J1 h0 B+ v- bearing cap designed as U-profile
# T3 K9 | t2 y$ b
6 _' h3 s9 D. x8 d. V$ N$ i0 ]8 X0 n紅色的字翻譯不準,我做的是才柴油機機體設計 先謝謝了 |
本帖子中包含更多資源
您需要 登錄 才可以下載或查看,沒有賬號?注冊會員
×
|