BRENNKRAFTMASCHINE MIT BRENNSTOFF- LUFTGEMISCHVORWAERMUNG

A heat pipe (20) runs between the exhaust manifold (16) and the inlet manifold (14) of the engine. It is bent at its heat absorbing end(32) so that a substantial length runs axially along the centreline of the exhaust manifold whilst its central part leaves the manifold radially through the side of...

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Hauptverfasser:	BIRNBREIER,HERMANN, KRAPF,RUDOLF
Format:	Patent
Sprache:	ger
Schlagworte:	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING SUPPLYING COMBUSTION ENGINES IN GENERAL, WITH COMBUSTIBLEMIXTURES OR CONSTITUENTS THEREOF WEAPONS
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creator	BIRNBREIER,HERMANN KRAPF,RUDOLF
description	A heat pipe (20) runs between the exhaust manifold (16) and the inlet manifold (14) of the engine. It is bent at its heat absorbing end(32) so that a substantial length runs axially along the centreline of the exhaust manifold whilst its central part leaves the manifold radially through the side of the manifold. The heat releasing end (24) runs centrally through the inlet manifold before it branches to the several cylinders. This end carries a series of ribs (28) which increase the heat transfer surface. The ribs are perpendicular to the flow of inlet gas for max. turbulence and heat transffer.
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It is bent at its heat absorbing end(32) so that a substantial length runs axially along the centreline of the exhaust manifold whilst its central part leaves the manifold radially through the side of the manifold. The heat releasing end (24) runs centrally through the inlet manifold before it branches to the several cylinders. This end carries a series of ribs (28) which increase the heat transfer surface. The ribs are perpendicular to the flow of inlet gas for max. turbulence and heat transffer.</description><edition>2</edition><language>ger</language><subject>BLASTING ; COMBUSTION ENGINES ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; SUPPLYING COMBUSTION ENGINES IN GENERAL, WITH COMBUSTIBLEMIXTURES OR CONSTITUENTS THEREOF ; WEAPONS</subject><creationdate>1979</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=19790927&DB=EPODOC&CC=DE&NR=2812061A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=19790927&DB=EPODOC&CC=DE&NR=2812061A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>BIRNBREIER,HERMANN</creatorcontrib><creatorcontrib>KRAPF,RUDOLF</creatorcontrib><title>BRENNKRAFTMASCHINE MIT BRENNSTOFF- LUFTGEMISCHVORWAERMUNG</title><description>A heat pipe (20) runs between the exhaust manifold (16) and the inlet manifold (14) of the engine. It is bent at its heat absorbing end(32) so that a substantial length runs axially along the centreline of the exhaust manifold whilst its central part leaves the manifold radially through the side of the manifold. The heat releasing end (24) runs centrally through the inlet manifold before it branches to the several cylinders. This end carries a series of ribs (28) which increase the heat transfer surface. The ribs are perpendicular to the flow of inlet gas for max. turbulence and heat transffer.</description><subject>BLASTING</subject><subject>COMBUSTION ENGINES</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>SUPPLYING COMBUSTION ENGINES IN GENERAL, WITH COMBUSTIBLEMIXTURES OR CONSTITUENTS THEREOF</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>1979</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLB0CnL18_MOcnQL8XUMdvbw9HNV8PUMUQALB4f4u7npKviEuoW4u_p6AqXD_IPCHV2DfEP93HkYWNMSc4pTeaE0N4OCm2uIs4duakF-fGpxQWJyal5qSbyLq5GFoZGBmaGjoTERSgB9dCjT</recordid><startdate>19790927</startdate><enddate>19790927</enddate><creator>BIRNBREIER,HERMANN</creator><creator>KRAPF,RUDOLF</creator><scope>EVB</scope></search><sort><creationdate>19790927</creationdate><title>BRENNKRAFTMASCHINE MIT BRENNSTOFF- LUFTGEMISCHVORWAERMUNG</title><author>BIRNBREIER,HERMANN ; KRAPF,RUDOLF</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_DE2812061A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>ger</language><creationdate>1979</creationdate><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>SUPPLYING COMBUSTION ENGINES IN GENERAL, WITH COMBUSTIBLEMIXTURES OR CONSTITUENTS THEREOF</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>BIRNBREIER,HERMANN</creatorcontrib><creatorcontrib>KRAPF,RUDOLF</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>BIRNBREIER,HERMANN</au><au>KRAPF,RUDOLF</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>BRENNKRAFTMASCHINE MIT BRENNSTOFF- LUFTGEMISCHVORWAERMUNG</title><date>1979-09-27</date><risdate>1979</risdate><abstract>A heat pipe (20) runs between the exhaust manifold (16) and the inlet manifold (14) of the engine. It is bent at its heat absorbing end(32) so that a substantial length runs axially along the centreline of the exhaust manifold whilst its central part leaves the manifold radially through the side of the manifold. The heat releasing end (24) runs centrally through the inlet manifold before it branches to the several cylinders. This end carries a series of ribs (28) which increase the heat transfer surface. The ribs are perpendicular to the flow of inlet gas for max. turbulence and heat transffer.</abstract><edition>2</edition><oa>free_for_read</oa></addata></record>
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subjects	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING SUPPLYING COMBUSTION ENGINES IN GENERAL, WITH COMBUSTIBLEMIXTURES OR CONSTITUENTS THEREOF WEAPONS
title	BRENNKRAFTMASCHINE MIT BRENNSTOFF- LUFTGEMISCHVORWAERMUNG
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