Enclosed multi-layer curved surface cavity integrated exhaust manifold turbine box
The invention discloses a closed multi-layer curved surface cavity integrated exhaust manifold turbine box which comprises a turbine box body. The turbine box comprises an inner wall layer and an outer wall layer which are distributed at intervals inside and outside; a waste gas exhaust cavity chann...
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creator | PANG SHAOBO ZHANG BIN WANG QI WANG HUI YANG JIANWEN YAN JIANFEI |
description | The invention discloses a closed multi-layer curved surface cavity integrated exhaust manifold turbine box which comprises a turbine box body. The turbine box comprises an inner wall layer and an outer wall layer which are distributed at intervals inside and outside; a waste gas exhaust cavity channel is formed in the inner wall layer; a cooling water cavity channel is formed between the inner wall layer and the outer wall layer; the cooling water cavity channel is arranged on the outer side of the waste gas exhaust cavity channel in a surrounding manner; a plurality of waste gas inlets distributed at intervals are formed in the right side of the turbine box; a cooling water inlet is formed in the lower end of the right side of the turbine box; the cooling water inlet is communicated with the cooling water cavity channel; the waste gas inlet is communicated with the waste gas exhaust cavity channel; a cooling water outlet is formed in the upper end of the rear side of the turbine box; the cooling water outlet |
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The turbine box comprises an inner wall layer and an outer wall layer which are distributed at intervals inside and outside; a waste gas exhaust cavity channel is formed in the inner wall layer; a cooling water cavity channel is formed between the inner wall layer and the outer wall layer; the cooling water cavity channel is arranged on the outer side of the waste gas exhaust cavity channel in a surrounding manner; a plurality of waste gas inlets distributed at intervals are formed in the right side of the turbine box; a cooling water inlet is formed in the lower end of the right side of the turbine box; the cooling water inlet is communicated with the cooling water cavity channel; the waste gas inlet is communicated with the waste gas exhaust cavity channel; a cooling water outlet is formed in the upper end of the rear side of the turbine box; the cooling water outlet</description><language>chi ; eng</language><subject>BLASTING ; ENGINE PLANTS IN GENERAL ; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNALCOMBUSTION ENGINES ; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES ORENGINES IN GENERAL ; HEATING ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; STEAM ENGINES ; WEAPONS</subject><creationdate>2024</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20240308&DB=EPODOC&CC=CN&NR=117662261A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20240308&DB=EPODOC&CC=CN&NR=117662261A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>PANG SHAOBO</creatorcontrib><creatorcontrib>ZHANG BIN</creatorcontrib><creatorcontrib>WANG QI</creatorcontrib><creatorcontrib>WANG HUI</creatorcontrib><creatorcontrib>YANG JIANWEN</creatorcontrib><creatorcontrib>YAN JIANFEI</creatorcontrib><title>Enclosed multi-layer curved surface cavity integrated exhaust manifold turbine box</title><description>The invention discloses a closed multi-layer curved surface cavity integrated exhaust manifold turbine box which comprises a turbine box body. 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The turbine box comprises an inner wall layer and an outer wall layer which are distributed at intervals inside and outside; a waste gas exhaust cavity channel is formed in the inner wall layer; a cooling water cavity channel is formed between the inner wall layer and the outer wall layer; the cooling water cavity channel is arranged on the outer side of the waste gas exhaust cavity channel in a surrounding manner; a plurality of waste gas inlets distributed at intervals are formed in the right side of the turbine box; a cooling water inlet is formed in the lower end of the right side of the turbine box; the cooling water inlet is communicated with the cooling water cavity channel; the waste gas inlet is communicated with the waste gas exhaust cavity channel; a cooling water outlet is formed in the upper end of the rear side of the turbine box; the cooling water outlet</abstract><oa>free_for_read</oa></addata></record> |
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language | chi ; eng |
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subjects | BLASTING ENGINE PLANTS IN GENERAL GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNALCOMBUSTION ENGINES GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES ORENGINES IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS |
title | Enclosed multi-layer curved surface cavity integrated exhaust manifold turbine box |
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