Hamilton, Brook, Smith & Reynolds, P.C.
Integrated pylon structure for propulsion system
An integrated pylon structure for a propulsion system is suitable for one end to be connected to an aircraft wing and the other end to be connected to an aircraft engine. The pylon structure includes a pylon box section (110) formed from an upper and a lower bean, a frame (100) and a side wall panel. The pylon structure has a thrust reverser hood connection structure, provided on the side wall and connected with a nacelle thrust reverser hood having a front fixed hood (301) and a rear movable hood (302). A guide rail allows the rear movable hood to slide and open relative to the pylon box section. The engine thrust reverser hood is directly connected to the side wall of the pylon box section and a guide rail on the side wall guides the opening of the thrust reverser hood.
Commercial Aircraft Corporation of China, LTD COMMERCIAL AIRCRAFT CORPORATION OF CHINA, LTD SHANGHAI AIRCRAFT DESIGN AND RESEARCH INSTITUTE
F B B B Y Y
F02K B64D B64D B64D Y02T Y02T
inventional inventional additional inventional additional additional
Sen Qifeng Liangdao Haisha Guozheng Honggang Shiwei Haojie Xiaonan Yinyin Kecen Mingpeng Guanghui Hongjie Pengfei Shibiao
Peng Yu Zhou Guo Lin Tang Ma Weng Li Hu Han Yan Wu Zhang Zhang Zhang