CN113074060A - 一种二元适量喷管矢量偏转控制方法 - Google Patents
一种二元适量喷管矢量偏转控制方法 Download PDFInfo
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- CN113074060A CN113074060A CN202110307735.9A CN202110307735A CN113074060A CN 113074060 A CN113074060 A CN 113074060A CN 202110307735 A CN202110307735 A CN 202110307735A CN 113074060 A CN113074060 A CN 113074060A
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/06—Varying effective area of jet pipe or nozzle
- F02K1/15—Control or regulation
- F02K1/18—Control or regulation automatic
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CN113074060A true CN113074060A (zh) | 2021-07-06 |
CN113074060B CN113074060B (zh) | 2022-04-01 |
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Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113638820A (zh) * | 2021-10-13 | 2021-11-12 | 中国航发四川燃气涡轮研究院 | 一种扩张段调节板不过中线的二元矢量喷管矢量实现方法 |
CN114542323A (zh) * | 2021-12-29 | 2022-05-27 | 中国航空工业集团公司沈阳飞机设计研究所 | 一种矢量喷管的控制方法及装置 |
CN117087865A (zh) * | 2023-10-20 | 2023-11-21 | 中国空气动力研究与发展中心计算空气动力研究所 | 一种飞翼气动飞行器及控制方法 |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1030122A (zh) * | 1987-06-25 | 1989-01-04 | 联合工艺公司 | 用于二维排气喷管的发散调节片驱动*** |
CN104033279A (zh) * | 2014-06-06 | 2014-09-10 | 中国航空工业集团公司沈阳发动机设计研究所 | 一种新型二元矢量喷管 |
CN104033280A (zh) * | 2014-06-06 | 2014-09-10 | 中国航空工业集团公司沈阳发动机设计研究所 | 一种可实现s弯遮挡功能的二元矢量喷管 |
CN104033281A (zh) * | 2014-06-09 | 2014-09-10 | 中国航空工业集团公司沈阳发动机设计研究所 | 一种具有单边膨胀功能的二元矢量喷管 |
CN112502852A (zh) * | 2020-12-01 | 2021-03-16 | 中国航发沈阳发动机研究所 | 一种可实现滚转功能的二元矢量喷管 |
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2021
- 2021-03-23 CN CN202110307735.9A patent/CN113074060B/zh active Active
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1030122A (zh) * | 1987-06-25 | 1989-01-04 | 联合工艺公司 | 用于二维排气喷管的发散调节片驱动*** |
CN104033279A (zh) * | 2014-06-06 | 2014-09-10 | 中国航空工业集团公司沈阳发动机设计研究所 | 一种新型二元矢量喷管 |
CN104033280A (zh) * | 2014-06-06 | 2014-09-10 | 中国航空工业集团公司沈阳发动机设计研究所 | 一种可实现s弯遮挡功能的二元矢量喷管 |
CN104033281A (zh) * | 2014-06-09 | 2014-09-10 | 中国航空工业集团公司沈阳发动机设计研究所 | 一种具有单边膨胀功能的二元矢量喷管 |
CN112502852A (zh) * | 2020-12-01 | 2021-03-16 | 中国航发沈阳发动机研究所 | 一种可实现滚转功能的二元矢量喷管 |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113638820A (zh) * | 2021-10-13 | 2021-11-12 | 中国航发四川燃气涡轮研究院 | 一种扩张段调节板不过中线的二元矢量喷管矢量实现方法 |
CN114542323A (zh) * | 2021-12-29 | 2022-05-27 | 中国航空工业集团公司沈阳飞机设计研究所 | 一种矢量喷管的控制方法及装置 |
CN114542323B (zh) * | 2021-12-29 | 2023-11-28 | 中国航空工业集团公司沈阳飞机设计研究所 | 一种矢量喷管的控制方法及装置 |
CN117087865A (zh) * | 2023-10-20 | 2023-11-21 | 中国空气动力研究与发展中心计算空气动力研究所 | 一种飞翼气动飞行器及控制方法 |
CN117087865B (zh) * | 2023-10-20 | 2024-01-26 | 中国空气动力研究与发展中心计算空气动力研究所 | 一种飞翼气动飞行器及控制方法 |
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