THE STRENGTHENING OF AERO-TRANSPORT WITH LARGE OPENING |
| |
Authors: | SU Yanfei TAN Shengang XUE Yingju HUI Hongjun |
| |
Institution: | The First Aircraft Institute of the Aviation Industry Corporation of China, Xi'an 710089, China |
| |
Abstract: | The concept of stiffness ratio is defined to study the strengthening of a fuselage with large opening, in order to meet the design requirements of stiffness and deformation. The relationships among the opening angle, the fuselage radius, the skin thickness, the beam area and the stiffness ratio are formulated through a theoretical analysis. The principle and the method to strengthen the fuselage with large opening are successfully applied on the aircraft in the preliminary design stage and can be used to guide the structure design. |
| |
Keywords: | large opening|fuselage|the ratio of stiffness |
|
| 点击此处可从《力学与实践》浏览原始摘要信息 |
| 点击此处可从《力学与实践》下载免费的PDF全文 |
|