CN107091159A - 基于柔性中心体的轴对称可调超声速进气道的设计方法 - Google Patents
基于柔性中心体的轴对称可调超声速进气道的设计方法 Download PDFInfo
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- CN107091159A CN107091159A CN201710461647.8A CN201710461647A CN107091159A CN 107091159 A CN107091159 A CN 107091159A CN 201710461647 A CN201710461647 A CN 201710461647A CN 107091159 A CN107091159 A CN 107091159A
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/042—Air intakes for gas-turbine plants or jet-propulsion plants having variable geometry
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/057—Control or regulation
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F30/00—Computer-aided design [CAD]
- G06F30/10—Geometric CAD
- G06F30/17—Mechanical parametric or variational design
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
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- Combustion & Propulsion (AREA)
- Chemical & Material Sciences (AREA)
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- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Physics & Mathematics (AREA)
- Theoretical Computer Science (AREA)
- Mathematical Analysis (AREA)
- Evolutionary Computation (AREA)
- Computer Hardware Design (AREA)
- Pure & Applied Mathematics (AREA)
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- Rigid Pipes And Flexible Pipes (AREA)
Abstract
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Priority Applications (1)
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CN201710461647.8A CN107091159B (zh) | 2017-06-16 | 2017-06-16 | 基于柔性中心体的轴对称可调超声速进气道的设计方法 |
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CN201710461647.8A CN107091159B (zh) | 2017-06-16 | 2017-06-16 | 基于柔性中心体的轴对称可调超声速进气道的设计方法 |
Publications (2)
Publication Number | Publication Date |
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CN107091159A true CN107091159A (zh) | 2017-08-25 |
CN107091159B CN107091159B (zh) | 2018-07-31 |
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CN201710461647.8A Active CN107091159B (zh) | 2017-06-16 | 2017-06-16 | 基于柔性中心体的轴对称可调超声速进气道的设计方法 |
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Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107701314A (zh) * | 2017-11-24 | 2018-02-16 | 厦门大学 | 一种利用柔性壁面提升进气道起动性能的流动控制方法 |
CN108999704A (zh) * | 2018-08-17 | 2018-12-14 | 中国人民解放军国防科技大学 | 高超声速进气道起动方法及起动装置 |
CN110159434A (zh) * | 2018-11-15 | 2019-08-23 | 北京机电工程研究所 | 一种进气道可调装置和方法 |
CN110780685A (zh) * | 2019-08-20 | 2020-02-11 | 南京理工大学 | 用于直连式实验台来流流量调节装置 |
CN111648865A (zh) * | 2020-04-30 | 2020-09-11 | 南京航空航天大学 | 一种可变粒子分离器多气室鼓包中心体结构及其设计方法 |
CN113700560A (zh) * | 2021-09-24 | 2021-11-26 | 西安航天动力研究所 | 一种半膜翻转超声速可调进气道 |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20090092482A1 (en) * | 2007-10-09 | 2009-04-09 | United Technologies Corp. | Systems and Methods for Altering Inlet Airflow of Gas Turbine Engines |
CN101956631A (zh) * | 2010-09-30 | 2011-01-26 | 西北工业大学 | 一种吸气式脉冲爆震发动机进气道 |
CN105134383A (zh) * | 2015-08-26 | 2015-12-09 | 南京航空航天大学 | 基于流线偏折的高超声速内转式进气道唇罩设计方法 |
CN205277643U (zh) * | 2015-11-26 | 2016-06-01 | 重庆凯特动力科技有限公司 | 增压发动机进气道 |
-
2017
- 2017-06-16 CN CN201710461647.8A patent/CN107091159B/zh active Active
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20090092482A1 (en) * | 2007-10-09 | 2009-04-09 | United Technologies Corp. | Systems and Methods for Altering Inlet Airflow of Gas Turbine Engines |
CN101956631A (zh) * | 2010-09-30 | 2011-01-26 | 西北工业大学 | 一种吸气式脉冲爆震发动机进气道 |
CN105134383A (zh) * | 2015-08-26 | 2015-12-09 | 南京航空航天大学 | 基于流线偏折的高超声速内转式进气道唇罩设计方法 |
CN205277643U (zh) * | 2015-11-26 | 2016-06-01 | 重庆凯特动力科技有限公司 | 增压发动机进气道 |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107701314A (zh) * | 2017-11-24 | 2018-02-16 | 厦门大学 | 一种利用柔性壁面提升进气道起动性能的流动控制方法 |
CN108999704A (zh) * | 2018-08-17 | 2018-12-14 | 中国人民解放军国防科技大学 | 高超声速进气道起动方法及起动装置 |
CN110159434A (zh) * | 2018-11-15 | 2019-08-23 | 北京机电工程研究所 | 一种进气道可调装置和方法 |
CN110780685A (zh) * | 2019-08-20 | 2020-02-11 | 南京理工大学 | 用于直连式实验台来流流量调节装置 |
CN110780685B (zh) * | 2019-08-20 | 2023-01-13 | 南京理工大学 | 用于直连式实验台来流流量调节装置 |
CN111648865A (zh) * | 2020-04-30 | 2020-09-11 | 南京航空航天大学 | 一种可变粒子分离器多气室鼓包中心体结构及其设计方法 |
CN111648865B (zh) * | 2020-04-30 | 2022-02-08 | 南京航空航天大学 | 一种可变粒子分离器多气室鼓包中心体结构及其设计方法 |
CN113700560A (zh) * | 2021-09-24 | 2021-11-26 | 西安航天动力研究所 | 一种半膜翻转超声速可调进气道 |
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CN107091159B (zh) | 2018-07-31 |
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Inventor after: Zhang Yue Inventor after: Liu Yazhou Inventor after: Sheng Fajia Inventor after: Tan Huijun Inventor after: Li Bo Inventor after: Wang Ziyun Inventor before: Zhang Yue Inventor before: Tan Huijun Inventor before: Li Bo Inventor before: Wang Ziyun Inventor before: Liu Yazhou Inventor before: Sheng Fajia |
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