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The concepts listed below are shown in Figure 5 % M. {# T; d. C8 N" U w
- varying topdeck thickness
5 N. o3 d6 z4 U2 e E- varying liner thickness1 O F# P/ K7 S7 G1 y( h
- horizontal trussbar are integrated to the topdeck
# p7 {& L% P. B2 G& t- vertical trussbars act as oil return and blow-by passages
N$ {8 ?6 v8 {* G% ?6 a! C- thread bosses for the cylinder head are integrated to the water jacket deck
& @& h( H% H6 d- reduced thread depth. ?/ j2 b$ b/ X0 Z
-- decreased water jacket height
- N9 i% x, H# |9 L- C- d, W0 p- wide crankcase venting holes! g3 q' X3 d' y& Y& Q
- hollow main bearing walls
. I& Z3 q) ^1 z; `- reduced oil pan flange thickness
' x. y* S( ~# q- bearing cap designed as U-profile0 T; R- ^/ ?. s; U$ `& i) g
, ~* O! f$ \6 S$ J4 V, t; |
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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