Study on Manufacturing Technology of Ω Type Stiffened Panel of Civil Aviation

MA Gang; TANG Wenfeng

doi:10.16080/j.issn1671-833x.2017.12.074

您当前的位置：

首页 >

文章列表页 >

Study on Manufacturing Technology of Ω Type Stiffened Panel of Civil Aviation

更新时间：2026-04-17

- Study on Manufacturing Technology of Ω Type Stiffened Panel of Civil Aviation
- Aeronautical Manufacturing Technology Vol. 60, Issue 12, Pages: 74-77(2017)
- 作者机构：
  
  航空工业沈阳飞机工业（集团）有限公司,沈阳,110850
- 作者简介：
- 基金信息：
- DOI：10.16080/j.issn1671-833x.2017.12.074
  CLC：
- Published：2017
- 稿件说明：
移动端阅览
马　刚，唐文峰. 民用航空含Ω 型长桁复合材料加筋壁板制造技术研究[J]. 航空制造技术, 2017, 60(12): 74-77.

MA Gang, TANG Wenfeng. Study on Manufacturing Technology of Ω Type Stiffened Panel of Civil Aviation. Aeronautical Manufacturing Technology, 2017, 60(12): 74-77.
马　刚，唐文峰. 民用航空含Ω 型长桁复合材料加筋壁板制造技术研究[J]. 航空制造技术, 2017, 60(12): 74-77. DOI： 10.16080/j.issn1671-833x.2017.12.074.

MA Gang, TANG Wenfeng. Study on Manufacturing Technology of Ω Type Stiffened Panel of Civil Aviation. Aeronautical Manufacturing Technology, 2017, 60(12): 74-77. DOI： 10.16080/j.issn1671-833x.2017.12.074.

摘要

含Ω 型长桁的复合材料加筋壁板由于其结构上的优势，在民用大飞机上被越来越多地采用。然而，此种类型的加筋壁板在共固化成型过程中存在Ω 型长桁如何加压的问题，特别是在有严格的适航符合性审查要求的民用航空产品制造领域，进一步提高了制造难度。经过多次试验，最终采用薄壁橡胶气囊成型法制造出符合设计要求和适航要求的含Ω 型长桁加筋壁板。

Abstract

Ω type composites stiffened panel has been widely used in large civil aircraft due to its structural advantage. But some difficulties exist in how to pressurize these Ω type stiffened panels during the co-curing process. Especially there are strict airworthiness compliance review requirements in the field of civil aviation products manufacturing

thereby further increasing the manufacturing difficulty. After a number of tests

the group decided to adopt thin-walled rubber balloon forming method to manufacture the Ω type stiffened panel in order to meet design requirements and airworthiness requirements finally.

关键词

Keywords

references

Views

800

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Design and Verification of the Hot-Press Scheme for Composite Double-Curved Omega Stringer

Deformation Prediction of Composite Bolted Joints Considering Multi-Source Variables

Circuit Design and Analysis for Passenger Oxygen System of Civil Aircraft

Experimental Study on Penetration Characteristics of Domestic Automated Placement Dry Fibers

Research Progress on Structure Design and Properties of MXene-Based Electromagnetic Shielding Composites

Related Author

LIU Juntian

YAN Chao

QIU Chunliang

CHEN Ping

LU Xin

YU Wencai

LIU Yuming

LIN Qingyuan

Related Institution

COMAC Shanghai Aircraft Manufacturing Co., Ltd.

Changzhou Newtry Aviation Technology Co., Ltd.

Shanghai Key Laboratory of Digital Manufacture for Thin-Walled Structures, Shanghai Jiao Tong University

Shanghai Aircraft Design and Research Institute

College of Textiles, Donghua University

The platform construction and operation are provided by Beijing Founder electronics co., LTD 京ICP备09064830号-19 京公网安备11010802024621
It is recommended to read the content of this site in Chrome&IE9+. Please switch to extreme mode in browser 360.
Cookies We use cookies to help provide and enhance our service and tailor content. By continuing, you agree to the use of cookies.
Total Visits：34726 Visits Today：204

⁰