Flame tube structure of turbojet engine
The utility model relates to a flame tube structure of a turbojet engine. The flame tube structure comprises an inner tube, an outer tube, a tube top and an air inlet group, wherein the inner cylinder and the outer cylinder are of cylindrical structures, and the inner cylinder and the outer cylinder...
Gespeichert in:
| Hauptverfasser: | , , , , , , , |
|---|---|
| Format: | Patent |
| Sprache: | chi ; eng |
| Schlagworte: | |
| Online-Zugang: | Volltext bestellen |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | |
|---|---|
| container_issue | |
| container_start_page | |
| container_title | |
| container_volume | |
| creator | REN QUANLONG CAO HAOBO LI SHIJIE DU ZHUO YANG XIAOJIE SHI HONGHAO YANG JINHU ZHANG WEI |
| description | The utility model relates to a flame tube structure of a turbojet engine. The flame tube structure comprises an inner tube, an outer tube, a tube top and an air inlet group, wherein the inner cylinder and the outer cylinder are of cylindrical structures, and the inner cylinder and the outer cylinder are provided with first ends and second ends; the inner cylinder is sleeved with the outer cylinder, the outer cylinder coincides with the central axis of the inner cylinder, a combustion area is formed between the outer cylinder and the inner cylinder, the first end of the outer cylinder is aligned with the first end of the inner cylinder, and the second end of the inner cylinder extends out of the outer cylinder; the cylinder top is of an annular structure, the periphery of the cylinder top is connected with the outer cylinder, the inner periphery is connected with the inner cylinder, and a gap between the inner cylinder and the first end of the outer cylinder is sealed through the annular structure. The air inl |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN219414871UU</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN219414871UU</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN219414871UU3</originalsourceid><addsrcrecordid>eNrjZFB3y0nMTVUoKU1KVSguKSpNLiktSlXITwOKFCXlZ6WWKKTmpWfmpfIwsKYl5hSn8kJpbgYlN9cQZw_d1IL8-NTigsTk1LzUknhnPyNDSxNDEwtzw9BQY6IUAQD2hijM</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Flame tube structure of turbojet engine</title><source>esp@cenet</source><creator>REN QUANLONG ; CAO HAOBO ; LI SHIJIE ; DU ZHUO ; YANG XIAOJIE ; SHI HONGHAO ; YANG JINHU ; ZHANG WEI</creator><creatorcontrib>REN QUANLONG ; CAO HAOBO ; LI SHIJIE ; DU ZHUO ; YANG XIAOJIE ; SHI HONGHAO ; YANG JINHU ; ZHANG WEI</creatorcontrib><description>The utility model relates to a flame tube structure of a turbojet engine. The flame tube structure comprises an inner tube, an outer tube, a tube top and an air inlet group, wherein the inner cylinder and the outer cylinder are of cylindrical structures, and the inner cylinder and the outer cylinder are provided with first ends and second ends; the inner cylinder is sleeved with the outer cylinder, the outer cylinder coincides with the central axis of the inner cylinder, a combustion area is formed between the outer cylinder and the inner cylinder, the first end of the outer cylinder is aligned with the first end of the inner cylinder, and the second end of the inner cylinder extends out of the outer cylinder; the cylinder top is of an annular structure, the periphery of the cylinder top is connected with the outer cylinder, the inner periphery is connected with the inner cylinder, and a gap between the inner cylinder and the first end of the outer cylinder is sealed through the annular structure. The air inl</description><language>chi ; eng</language><subject>BLASTING ; COMBUSTION APPARATUS ; COMBUSTION PROCESSES ; GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS ; HEATING ; LIGHTING ; MECHANICAL ENGINEERING ; WEAPONS</subject><creationdate>2023</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=20230725&DB=EPODOC&CC=CN&NR=219414871U$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20230725&DB=EPODOC&CC=CN&NR=219414871U$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>REN QUANLONG</creatorcontrib><creatorcontrib>CAO HAOBO</creatorcontrib><creatorcontrib>LI SHIJIE</creatorcontrib><creatorcontrib>DU ZHUO</creatorcontrib><creatorcontrib>YANG XIAOJIE</creatorcontrib><creatorcontrib>SHI HONGHAO</creatorcontrib><creatorcontrib>YANG JINHU</creatorcontrib><creatorcontrib>ZHANG WEI</creatorcontrib><title>Flame tube structure of turbojet engine</title><description>The utility model relates to a flame tube structure of a turbojet engine. The flame tube structure comprises an inner tube, an outer tube, a tube top and an air inlet group, wherein the inner cylinder and the outer cylinder are of cylindrical structures, and the inner cylinder and the outer cylinder are provided with first ends and second ends; the inner cylinder is sleeved with the outer cylinder, the outer cylinder coincides with the central axis of the inner cylinder, a combustion area is formed between the outer cylinder and the inner cylinder, the first end of the outer cylinder is aligned with the first end of the inner cylinder, and the second end of the inner cylinder extends out of the outer cylinder; the cylinder top is of an annular structure, the periphery of the cylinder top is connected with the outer cylinder, the inner periphery is connected with the inner cylinder, and a gap between the inner cylinder and the first end of the outer cylinder is sealed through the annular structure. The air inl</description><subject>BLASTING</subject><subject>COMBUSTION APPARATUS</subject><subject>COMBUSTION PROCESSES</subject><subject>GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFB3y0nMTVUoKU1KVSguKSpNLiktSlXITwOKFCXlZ6WWKKTmpWfmpfIwsKYl5hSn8kJpbgYlN9cQZw_d1IL8-NTigsTk1LzUknhnPyNDSxNDEwtzw9BQY6IUAQD2hijM</recordid><startdate>20230725</startdate><enddate>20230725</enddate><creator>REN QUANLONG</creator><creator>CAO HAOBO</creator><creator>LI SHIJIE</creator><creator>DU ZHUO</creator><creator>YANG XIAOJIE</creator><creator>SHI HONGHAO</creator><creator>YANG JINHU</creator><creator>ZHANG WEI</creator><scope>EVB</scope></search><sort><creationdate>20230725</creationdate><title>Flame tube structure of turbojet engine</title><author>REN QUANLONG ; CAO HAOBO ; LI SHIJIE ; DU ZHUO ; YANG XIAOJIE ; SHI HONGHAO ; YANG JINHU ; ZHANG WEI</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN219414871UU3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2023</creationdate><topic>BLASTING</topic><topic>COMBUSTION APPARATUS</topic><topic>COMBUSTION PROCESSES</topic><topic>GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>REN QUANLONG</creatorcontrib><creatorcontrib>CAO HAOBO</creatorcontrib><creatorcontrib>LI SHIJIE</creatorcontrib><creatorcontrib>DU ZHUO</creatorcontrib><creatorcontrib>YANG XIAOJIE</creatorcontrib><creatorcontrib>SHI HONGHAO</creatorcontrib><creatorcontrib>YANG JINHU</creatorcontrib><creatorcontrib>ZHANG WEI</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>REN QUANLONG</au><au>CAO HAOBO</au><au>LI SHIJIE</au><au>DU ZHUO</au><au>YANG XIAOJIE</au><au>SHI HONGHAO</au><au>YANG JINHU</au><au>ZHANG WEI</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Flame tube structure of turbojet engine</title><date>2023-07-25</date><risdate>2023</risdate><abstract>The utility model relates to a flame tube structure of a turbojet engine. The flame tube structure comprises an inner tube, an outer tube, a tube top and an air inlet group, wherein the inner cylinder and the outer cylinder are of cylindrical structures, and the inner cylinder and the outer cylinder are provided with first ends and second ends; the inner cylinder is sleeved with the outer cylinder, the outer cylinder coincides with the central axis of the inner cylinder, a combustion area is formed between the outer cylinder and the inner cylinder, the first end of the outer cylinder is aligned with the first end of the inner cylinder, and the second end of the inner cylinder extends out of the outer cylinder; the cylinder top is of an annular structure, the periphery of the cylinder top is connected with the outer cylinder, the inner periphery is connected with the inner cylinder, and a gap between the inner cylinder and the first end of the outer cylinder is sealed through the annular structure. The air inl</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | chi ; eng |
| recordid | cdi_epo_espacenet_CN219414871UU |
| source | esp@cenet |
| subjects | BLASTING COMBUSTION APPARATUS COMBUSTION PROCESSES GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING LIGHTING MECHANICAL ENGINEERING WEAPONS |
| title | Flame tube structure of turbojet engine |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-05T07%3A19%3A15IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=REN%20QUANLONG&rft.date=2023-07-25&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN219414871UU%3C/epo_EVB%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true |