Wing Join

MICHAEL MECHAM

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Wing Join

机译：翼联

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At its Renton factory south of Seattle, Boeing is assembling the first of its 737-900ERs, which incorporate a flat rear pressure bulkhead, optional fuel tanks and additional emergency exit doors to create a 215-seat long-range competitor to the Airbus A321. The 180-215-seat aircraft is set for an Aug. 8 rollout, followed by a five-month flight test/certification program that begins in September. As with all 737s, the fuselage is manufactured by Spirit Aerosystems in Wichita, Kan., and the CFM56-7B powerplants,by CFM International.

机译：波音公司正在其西雅图南部的伦顿工厂组装其首架737-900ER，其中包括平坦的后压力舱壁，可选的燃油箱和附加的紧急出口门，可为空客A321提供215个座位的远程竞争对手。这架180-215座的飞机定于8月8日推出，随后将在9月开始为期5个月的飞行测试/认证计划。与所有737一样，机身由堪萨斯州威奇托的Spirit Aerosystems和CFM International制造的CFM56-7B动力装置制造。

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来源
《Aviation Week & Space Technology》 |2006年第23期|p.39|共1页
作者
MICHAEL MECHAM;
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收录信息美国《工程索引》(EI);
原文格式 PDF
正文语种 eng
中图分类航空;
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机译：主动气动弹性翼技术在联翼传感器飞行器中的应用
2. Wing Joins put 737NG Operators in a Pickle [J] . Airliner World . 2020,第Jana期

机译：Wing Joins使737NG运营商陷入困境
3. Advanced Assembly Solutions for the Airbus RACER Joined-Wing Configuration [J] . Aerospace & Defense Technology . 2020,第Juna期

机译：用于空中客车赛车的高级装配解决方案加入-Wing-Wing配置
4. For Challenges in the Design of Joined Wings Special Session: Comparison of Aeroelastic Stability of Conventional and Joined-Wing Highly Flexible Aircraft [C] . Zahra Sotoudeh AIAA/ASCE/AHS/ASC structures, structural dynamics and materials conference;AIAA SciTech forum . 2015

机译：挑战联合机翼特别会议的设计：常规和联合机翼高柔性飞机的空气弹性稳定性比较
5. Nonlinear Aeroelastic Analysis of Joined-Wing Configurations. [D] . Cavallaro, Rauno. 2014

机译：连接翼构型的非线性气动弹性分析。
6. Narrative of the March of the Right Wing 15th Loodianah Sikhs from Sukkur until They Joined the Regimental Head-Quarters at Kandahar [O] . Surgeon A. E. K. Stephens 1879

机译：第十五届Loodianah Sikhs右翼游行的故事来自Sukkur直到他们加入坎大哈的团长
7. Analisis Numerik Part Spar Pada Sub System Wing To Fuselage Joinner Assembly Pesawat Berkategory Utility Menggunakan Metode Elemen Hingga [O] . Sahril Afandi, Agus Supriatno, Nurhadi Permana, 2021

机译：使用元素方法对副系统翼的数值分析零件翼架对机身翅膀的机身枢纽
8. Structural Design of Wing Twist for Pitch Control of Joined Wing Sensor Craft [R] . Kimler, I. F. 2006

机译：连杆传感器工艺桨距控制翼捻结构设计

Wing Join

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