Design method of fluid passage of air exhausting device of combustion gas turbine
The invention discloses a design method of a fluid passage of an air exhausting device of a combustion gas turbine. The design method of the fluid passage of the air exhausting device of the combustion gas turbine is used for reducing the pressure loss of the fluid passage between a circular or a ci...
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| creator | GONG YANAN ZHANG RUIXIA XU LING JIA DONGBING |
| description | The invention discloses a design method of a fluid passage of an air exhausting device of a combustion gas turbine. The design method of the fluid passage of the air exhausting device of the combustion gas turbine is used for reducing the pressure loss of the fluid passage between a circular or a circular ring-shaped air inlet and a rectangular air outlet at the perpendicular state, and comprisesthe steps of uniformly dividing the air inlet into 2n fan-shaped or fan ring-shaped air inlet units, uniformly dividing the air outlet into air outlet units with the same number of the air inlet units, and connecting the air inlet units and the air outlet units so as to form 2n fluid passage units, wherein each fluid passage nut comprises a transition section, a diffusion section and a convergencesection. According to the design method of the fluid passage of the air exhausting device of the combustion gas turbine provided by the invention, the fluid passage is designed to be of a split typestructure, and the 2n fluid |
| format | Patent |
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The design method of the fluid passage of the air exhausting device of the combustion gas turbine is used for reducing the pressure loss of the fluid passage between a circular or a circular ring-shaped air inlet and a rectangular air outlet at the perpendicular state, and comprisesthe steps of uniformly dividing the air inlet into 2n fan-shaped or fan ring-shaped air inlet units, uniformly dividing the air outlet into air outlet units with the same number of the air inlet units, and connecting the air inlet units and the air outlet units so as to form 2n fluid passage units, wherein each fluid passage nut comprises a transition section, a diffusion section and a convergencesection. According to the design method of the fluid passage of the air exhausting device of the combustion gas turbine provided by the invention, the fluid passage is designed to be of a split typestructure, and the 2n fluid</description><language>chi ; eng</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; ENGINE PLANTS IN GENERAL ; GAS-TURBINE PLANTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; STEAM ENGINES ; WEAPONS</subject><creationdate>2019</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=20190222&DB=EPODOC&CC=CN&NR=109372637A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20190222&DB=EPODOC&CC=CN&NR=109372637A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>GONG YANAN</creatorcontrib><creatorcontrib>ZHANG RUIXIA</creatorcontrib><creatorcontrib>XU LING</creatorcontrib><creatorcontrib>JIA DONGBING</creatorcontrib><title>Design method of fluid passage of air exhausting device of combustion gas turbine</title><description>The invention discloses a design method of a fluid passage of an air exhausting device of a combustion gas turbine. The design method of the fluid passage of the air exhausting device of the combustion gas turbine is used for reducing the pressure loss of the fluid passage between a circular or a circular ring-shaped air inlet and a rectangular air outlet at the perpendicular state, and comprisesthe steps of uniformly dividing the air inlet into 2n fan-shaped or fan ring-shaped air inlet units, uniformly dividing the air outlet into air outlet units with the same number of the air inlet units, and connecting the air inlet units and the air outlet units so as to form 2n fluid passage units, wherein each fluid passage nut comprises a transition section, a diffusion section and a convergencesection. 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The design method of the fluid passage of the air exhausting device of the combustion gas turbine is used for reducing the pressure loss of the fluid passage between a circular or a circular ring-shaped air inlet and a rectangular air outlet at the perpendicular state, and comprisesthe steps of uniformly dividing the air inlet into 2n fan-shaped or fan ring-shaped air inlet units, uniformly dividing the air outlet into air outlet units with the same number of the air inlet units, and connecting the air inlet units and the air outlet units so as to form 2n fluid passage units, wherein each fluid passage nut comprises a transition section, a diffusion section and a convergencesection. According to the design method of the fluid passage of the air exhausting device of the combustion gas turbine provided by the invention, the fluid passage is designed to be of a split typestructure, and the 2n fluid</abstract><oa>free_for_read</oa></addata></record> |
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| language | chi ; eng |
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| subjects | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS |
| title | Design method of fluid passage of air exhausting device of combustion gas turbine |
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