CN203512023U - 位于飞机机身尾部的俯仰控制舵面 - Google Patents
位于飞机机身尾部的俯仰控制舵面 Download PDFInfo
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- CN203512023U CN203512023U CN201320663457.1U CN201320663457U CN203512023U CN 203512023 U CN203512023 U CN 203512023U CN 201320663457 U CN201320663457 U CN 201320663457U CN 203512023 U CN203512023 U CN 203512023U
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- rudder face
- airplane
- control subsystem
- pitch control
- airframe
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CN201320663457.1U CN203512023U (zh) | 2013-10-27 | 2013-10-27 | 位于飞机机身尾部的俯仰控制舵面 |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110775296A (zh) * | 2019-11-12 | 2020-02-11 | 中国空气动力研究与发展中心计算空气动力研究所 | 一种可重复使用空天飞行器压心后移的设计方法 |
CN113911313A (zh) * | 2021-09-14 | 2022-01-11 | 中国航空工业集团公司沈阳飞机设计研究所 | 一种飞机后机身结构 |
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- 2013-10-27 CN CN201320663457.1U patent/CN203512023U/zh not_active Expired - Fee Related
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110775296A (zh) * | 2019-11-12 | 2020-02-11 | 中国空气动力研究与发展中心计算空气动力研究所 | 一种可重复使用空天飞行器压心后移的设计方法 |
CN113911313A (zh) * | 2021-09-14 | 2022-01-11 | 中国航空工业集团公司沈阳飞机设计研究所 | 一种飞机后机身结构 |
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Legal Events
Date | Code | Title | Description |
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C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
C53 | Correction of patent for invention or patent application | ||
CB03 | Change of inventor or designer information |
Inventor after: Jiang Zeng* Inventor after: Yang Lei Inventor after: Liu Tiezhong Inventor after: Yan Dongqi Inventor after: Li Chunpeng Inventor before: Jiang Zeng Inventor before: Yang Lei Inventor before: Liu Tiezhong Inventor before: Yan Dongqi Inventor before: Li Chunpeng |
|
COR | Change of bibliographic data |
Free format text: CORRECT: INVENTOR; FROM: JIANG ZENG YANG LEI LIU TIEZHONG YAN DONGQI LI CHUNPENG TO: JIANG ZENG * YANG LEI LIU TIEZHONG YAN DONGQI LI CHUNPENG |
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CF01 | Termination of patent right due to non-payment of annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20140402 Termination date: 20171027 |