Secondary-flow pintle rocket engine with pushing force controllable function
The invention discloses a secondary-flow pintle rocket engine with a pushing force controllable function, relates to a pintle rocket engine, and belongs to the field of variable-pushing-force rocket engines in pneumatic and mechanical hybrid control. The secondary-flow pintle rocket engine mainly co...
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creator | YAN DONGFENG WEI ZHIJUN WANG NINGFEI GUO CHANGCHAO XIE KAN |
description | The invention discloses a secondary-flow pintle rocket engine with a pushing force controllable function, relates to a pintle rocket engine, and belongs to the field of variable-pushing-force rocket engines in pneumatic and mechanical hybrid control. The secondary-flow pintle rocket engine mainly consists of pintle rocket engine basic devices such as a housing, a motor, a guide wheel, a combustion chamber, a pintle and a spray tube. The inner part of the pintle is hollowed out, a secondary-flow gas source is arranged in the hollowed-out part, and a secondary-flow jet hole is formed in the top of the pintle. During working, high-pressure secondary flow generated by the secondary-flow gas source is sprayed at the secondary-flow jet hole, and the jetted high-pressure secondary flow mainly has pushing force control effects as follows: firstly, the formed secondary-flow shearing layer is regulated to regulate the effective area of a throat part by regulating the pressure intensity and the flow rate of secondary fl |
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The secondary-flow pintle rocket engine mainly consists of pintle rocket engine basic devices such as a housing, a motor, a guide wheel, a combustion chamber, a pintle and a spray tube. The inner part of the pintle is hollowed out, a secondary-flow gas source is arranged in the hollowed-out part, and a secondary-flow jet hole is formed in the top of the pintle. During working, high-pressure secondary flow generated by the secondary-flow gas source is sprayed at the secondary-flow jet hole, and the jetted high-pressure secondary flow mainly has pushing force control effects as follows: firstly, the formed secondary-flow shearing layer is regulated to regulate the effective area of a throat part by regulating the pressure intensity and the flow rate of secondary fl</description><language>chi ; eng</language><subject>BLASTING ; COMBUSTION ENGINES ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; JET-PROPULSION PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; WEAPONS</subject><creationdate>2017</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=20170808&DB=EPODOC&CC=CN&NR=107023420A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20170808&DB=EPODOC&CC=CN&NR=107023420A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>YAN DONGFENG</creatorcontrib><creatorcontrib>WEI ZHIJUN</creatorcontrib><creatorcontrib>WANG NINGFEI</creatorcontrib><creatorcontrib>GUO CHANGCHAO</creatorcontrib><creatorcontrib>XIE KAN</creatorcontrib><title>Secondary-flow pintle rocket engine with pushing force controllable function</title><description>The invention discloses a secondary-flow pintle rocket engine with a pushing force controllable function, relates to a pintle rocket engine, and belongs to the field of variable-pushing-force rocket engines in pneumatic and mechanical hybrid control. The secondary-flow pintle rocket engine mainly consists of pintle rocket engine basic devices such as a housing, a motor, a guide wheel, a combustion chamber, a pintle and a spray tube. The inner part of the pintle is hollowed out, a secondary-flow gas source is arranged in the hollowed-out part, and a secondary-flow jet hole is formed in the top of the pintle. During working, high-pressure secondary flow generated by the secondary-flow gas source is sprayed at the secondary-flow jet hole, and the jetted high-pressure secondary flow mainly has pushing force control effects as follows: firstly, the formed secondary-flow shearing layer is regulated to regulate the effective area of a throat part by regulating the pressure intensity and the flow rate of secondary fl</description><subject>BLASTING</subject><subject>COMBUSTION ENGINES</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>JET-PROPULSION PLANTS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2017</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNy7EKwjAQgOEsDqK-w_kAhdgKzlIUB3HRvcR4aQ_DXUiuFN_eDj6A0798_9Jc7-iFXy5_qhBlgkSsESGLf6MCck-MMJEOkMYyEPcQJHuEedIsMbrnrMPIXkl4bRbBxYKbX1dmez492kuFSTosyXlk1K697ezB1s2-tsfmH_MF6JY2YA</recordid><startdate>20170808</startdate><enddate>20170808</enddate><creator>YAN DONGFENG</creator><creator>WEI ZHIJUN</creator><creator>WANG NINGFEI</creator><creator>GUO CHANGCHAO</creator><creator>XIE KAN</creator><scope>EVB</scope></search><sort><creationdate>20170808</creationdate><title>Secondary-flow pintle rocket engine with pushing force controllable function</title><author>YAN DONGFENG ; WEI ZHIJUN ; WANG NINGFEI ; GUO CHANGCHAO ; XIE KAN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN107023420A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2017</creationdate><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>JET-PROPULSION PLANTS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>YAN DONGFENG</creatorcontrib><creatorcontrib>WEI ZHIJUN</creatorcontrib><creatorcontrib>WANG NINGFEI</creatorcontrib><creatorcontrib>GUO CHANGCHAO</creatorcontrib><creatorcontrib>XIE KAN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>YAN DONGFENG</au><au>WEI ZHIJUN</au><au>WANG NINGFEI</au><au>GUO CHANGCHAO</au><au>XIE KAN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Secondary-flow pintle rocket engine with pushing force controllable function</title><date>2017-08-08</date><risdate>2017</risdate><abstract>The invention discloses a secondary-flow pintle rocket engine with a pushing force controllable function, relates to a pintle rocket engine, and belongs to the field of variable-pushing-force rocket engines in pneumatic and mechanical hybrid control. The secondary-flow pintle rocket engine mainly consists of pintle rocket engine basic devices such as a housing, a motor, a guide wheel, a combustion chamber, a pintle and a spray tube. The inner part of the pintle is hollowed out, a secondary-flow gas source is arranged in the hollowed-out part, and a secondary-flow jet hole is formed in the top of the pintle. During working, high-pressure secondary flow generated by the secondary-flow gas source is sprayed at the secondary-flow jet hole, and the jetted high-pressure secondary flow mainly has pushing force control effects as follows: firstly, the formed secondary-flow shearing layer is regulated to regulate the effective area of a throat part by regulating the pressure intensity and the flow rate of secondary fl</abstract><oa>free_for_read</oa></addata></record> |
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language | chi ; eng |
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subjects | BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS |
title | Secondary-flow pintle rocket engine with pushing force controllable function |
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