<p>A modular exhaust carrier (134) for an engine (104) is provided. The modular exhaust carrier (134) includes a first concave shell member (202) and a second concave shell member (204). The first concave shell member (202) is configured to define one half of an exhaust air passage. Moreover, the first concave shell member (202) either includes a solid wall configuration or a dust ejector opening (302) configuration. The second concave shell member (204) is configured to define a second half of an exhaust air passage. The second concave shell member (204) includes a solid wall configuration or a sensor housing configuration.</p>
申请公布号
WO2013095916(A1)
申请公布日期
2013.06.27
申请号
WO2012US67820
申请日期
2012.12.05
申请人
CATERPILLAR INC.
发明人
GRZESIAK, REBECCA, M.;BRAUN, MICHAEL, J.;VINCENT, REGINALD, R.