公开(公告)号：US20150360791A1

公开(公告)日：2015-12-17

申请号：US14763859

申请日：2014-02-04

Applicant: AIRBUS DEFENCE AND SPACE SAS

Inventor： Samuel CHEVROLLIER ,  Robert ABADIE-LAHAILLE ,  Pascal MEZIERES ,  Benjamin FAURE ,  Jérôme BERTRAND ,  Yohann CORABOEUF ,  Angélique SANTERRE

IPC: B64D37/04 ,  B64G1/40 ,  B64D37/30 ,  B64D37/06

CPC classification number: B64D37/04 ,  B64D37/06 ,  B64D37/30 ,  B64G1/402 ,  F16C11/0695 ,  F17C2205/0192 ,  F17C2221/08 ,  F17C2270/0197

Abstract: The invention concerns a tank retainer for retaining a tank in the fuselage of an aircraft which includes, between the tank and a frame rigidly connected to the fuselage of the aircraft, a hinged retaining means and a fastening rod on which said hinged retaining means is mounted. Advantageously, the hinged retaining means is intended to be connected to a rear end of the tank and the fastening rod is suitable for being mounted on the frame rigidly connected to the fuselage of the aircraft and, preferably, the hinged retaining means comprises a ball joint.

Abstract translation: 本发明涉及一种用于将坦克保持在飞行器的机身中的坦克保持器，其包括在坦克和刚性地连接到飞行器的机身的框架之间，铰接的保持装置和紧固杆，所述铰接的保持装置安装在该紧固杆上 。 有利地，铰接的保持装置旨在连接到罐的后端，并且紧固杆适于安装在刚性地连接到飞行器的机身的框架上，并且优选地，铰接的保持装置包括球形接头 。