The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.
The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.
Patent No.:
Date of Patent:
Jan. 02, 2018
Filed:
Dec. 12, 2013
Commercial Aircraft Corporation of China, Ltd, Shanghai, CN;
Commercial Aircraft Corporation of China, Ltd Shanghai Aircraft Design and Research Institute, Shanghai, CN;
Guanghui Wu, Shanghai, CN;
Kecen Han, Shanghai, CN;
Liangdao Zhou, Shanghai, CN;
Qifeng Yu, Shanghai, CN;
Guozheng Lin, Shanghai, CN;
Hongjie Zhang, Shanghai, CN;
Shibiao Zhang, Shanghai, CN;
Haojie Weng, Shanghai, CN;
Haisha Guo, Shanghai, CN;
Pengfei Zhang, Shanghai, CN;
Xiaonan Li, Shanghai, CN;
Shiwei Ma, Shanghai, CN;
Yinyin Hu, Shanghai, CN;
Sen Peng, Shanghai, CN;
Honggang Tang, Shanghai, CN;
Mingpeng Yan, Shanghai, CN;
Abstract
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 () formed from an upper and a lower bean, a frame () 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 () and a rear movable hood (). 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.