Research on the Application of Integrated Design on Micro Turbojet Engine
There are no detailed design criteria and methods for the integrated design of micro turbojet engine.The size and weight design and evaluation method for turbojet engines are used to perform the integrated design of several 9~80 kgf micro turbojet engines and evaluate the engines'data.The integ...
| Main Authors: | , , , , |
|---|---|
| Format: | Article |
| Language: | zho |
| Published: |
Editorial Department of Advances in Aeronautical Science and Engineering
2022-08-01
|
| Series: | Hangkong gongcheng jinzhan |
| Subjects: | |
| Online Access: | http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2021149 |
| _version_ | 1817984445021421568 |
|---|---|
| author | CHEN Minze CHEN Yuchun JIA Linyuan HUANG Xinchun LI Sunyang |
| author_facet | CHEN Minze CHEN Yuchun JIA Linyuan HUANG Xinchun LI Sunyang |
| author_sort | CHEN Minze |
| collection | DOAJ |
| description | There are no detailed design criteria and methods for the integrated design of micro turbojet engine.The size and weight design and evaluation method for turbojet engines are used to perform the integrated design of several 9~80 kgf micro turbojet engines and evaluate the engines'data.The integrated design parameters database of micro turbojet engine is established,and the integrated design criterion of micro turbojet engine is extracted.Using this criterion,the integrated design of 16 kgf micro turbojet engine is completed.The results show that,using the integrated design method for the micro turbojet engine,the obtained design criteria is highly reliable,and can perform the overall scheme design of the micro turbojet engine. |
| first_indexed | 2024-04-13T23:45:35Z |
| format | Article |
| id | doaj.art-b025430592894ce2baeacc8f2278d907 |
| institution | Directory Open Access Journal |
| issn | 1674-8190 |
| language | zho |
| last_indexed | 2024-04-13T23:45:35Z |
| publishDate | 2022-08-01 |
| publisher | Editorial Department of Advances in Aeronautical Science and Engineering |
| record_format | Article |
| series | Hangkong gongcheng jinzhan |
| spelling | doaj.art-b025430592894ce2baeacc8f2278d9072022-12-22T02:24:21ZzhoEditorial Department of Advances in Aeronautical Science and EngineeringHangkong gongcheng jinzhan1674-81902022-08-0113410711610.16615/j.cnki.1674-8190.2022.04.1220220412Research on the Application of Integrated Design on Micro Turbojet EngineCHEN Minze0CHEN Yuchun1JIA Linyuan2HUANG Xinchun3LI Sunyang4School of Power and Energy, Northwestern Polytechnical University, Xi’an 710129, ChinaSchool of Power and Energy, Northwestern Polytechnical University, Xi’an 710129, ChinaSchool of Power and Energy, Northwestern Polytechnical University, Xi’an 710129, ChinaSchool of Power and Energy, Northwestern Polytechnical University, Xi’an 710129, ChinaSchool of Power and Energy, Northwestern Polytechnical University, Xi’an 710129, ChinaThere are no detailed design criteria and methods for the integrated design of micro turbojet engine.The size and weight design and evaluation method for turbojet engines are used to perform the integrated design of several 9~80 kgf micro turbojet engines and evaluate the engines'data.The integrated design parameters database of micro turbojet engine is established,and the integrated design criterion of micro turbojet engine is extracted.Using this criterion,the integrated design of 16 kgf micro turbojet engine is completed.The results show that,using the integrated design method for the micro turbojet engine,the obtained design criteria is highly reliable,and can perform the overall scheme design of the micro turbojet engine.http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2021149micro turbojet enginesizeweightintegrated designdatabasedesign criteria |
| spellingShingle | CHEN Minze CHEN Yuchun JIA Linyuan HUANG Xinchun LI Sunyang Research on the Application of Integrated Design on Micro Turbojet Engine Hangkong gongcheng jinzhan micro turbojet engine size weight integrated design database design criteria |
| title | Research on the Application of Integrated Design on Micro Turbojet Engine |
| title_full | Research on the Application of Integrated Design on Micro Turbojet Engine |
| title_fullStr | Research on the Application of Integrated Design on Micro Turbojet Engine |
| title_full_unstemmed | Research on the Application of Integrated Design on Micro Turbojet Engine |
| title_short | Research on the Application of Integrated Design on Micro Turbojet Engine |
| title_sort | research on the application of integrated design on micro turbojet engine |
| topic | micro turbojet engine size weight integrated design database design criteria |
| url | http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2021149 |
| work_keys_str_mv | AT chenminze researchontheapplicationofintegrateddesignonmicroturbojetengine AT chenyuchun researchontheapplicationofintegrateddesignonmicroturbojetengine AT jialinyuan researchontheapplicationofintegrateddesignonmicroturbojetengine AT huangxinchun researchontheapplicationofintegrateddesignonmicroturbojetengine AT lisunyang researchontheapplicationofintegrateddesignonmicroturbojetengine |