公开(公告)号：US09701413B2

公开(公告)日：2017-07-11

申请号：US14040978

申请日：2013-09-30

Applicant: AIRCELLE

Inventor： Fabrice Provost ,  Pascal Soulier

IPC: E05C19/10 ,  B64D29/06 ,  E05B41/00 ,  E05B63/14 ,  E05C1/08 ,  E05B53/00

CPC classification number: B64D29/06 ,  E05B41/00 ,  E05B53/003 ,  E05B63/143 ,  Y10S292/04 ,  Y10S292/11 ,  Y10T292/0911

Abstract: A locking device between a first structure and a second structure includes a bolt to lock the first and second structures, an indicator as to whether the bolt has locked/unlocked the structures, and a connecting system. The bolt includes a lock bolt attached to the first structure and able to engage a hook which is attached to the second structure. In particular, the connecting system connects the bolt with the lock bolt to the indicator, and the hook is mounted such that it can move between a first position in which it is engaged with the lock bolt and allows the indicator to be locked, and a second position in which the hook is free of the lock bolt and allows the indicator to be unlocked.

公开(公告)号：US09670874B2

公开(公告)日：2017-06-06

申请号：US15093798

申请日：2016-04-08

Applicant: AIRCELLE

Inventor： Fabrice Provost

IPC: F02K1/72 ,  F02K1/80 ,  F16J15/02 ,  F02K1/56 ,  F01D11/00 ,  F16J15/06

CPC classification number: F02K1/566 ,  F01D11/005 ,  F02K1/72 ,  F02K1/805 ,  F05D2220/323 ,  F05D2240/128 ,  F05D2240/55 ,  F05D2250/182 ,  F05D2260/30 ,  F16J15/027 ,  F16J15/061

Abstract: The present disclosure relates to a seal for an aircraft turbojet engine nacelle thrust reverser, the seal having body having a cross section with respect to a longitudinal axis of the seal that is substantially circular, and a base which is intended to be mounted in a seal support. The seal is notable in that the base of said seal has apertures spaced from each other.

公开(公告)号：US09388769B2

公开(公告)日：2016-07-12

申请号：US14630837

申请日：2015-02-25

Applicant: AIRCELLE

Inventor： Fabrice Provost

IPC: F02K1/80 ,  F01D25/24 ,  F02K1/54

CPC classification number: F02K1/80 ,  F01D25/243 ,  F02K1/54 ,  F05D2240/90 ,  F05D2260/30 ,  F05D2260/37

Abstract: The present disclosure relates to a holding assembly to hold a front frame of a thrust reverser to a turbojet engine casing. The assembly includes at least one connecting flange connecting the front frame to the turbojet engine casing, and also a system for locking the connecting flange. The system includes an actuating handle pivotally mounted on one of two facing ends of the connecting flange, and a connecting rod interposed between the other end of the two facing ends and a portion of the actuating handle. The system locks together the two facing ends, and the actuating handle includes a support provided with a groove and a screw for adjusting a free length of the groove. Furthermore, the connecting rod has, at its one end, an axis pivoting and sliding in the groove.

Abstract translation: 本公开涉及一种用于将推力反向器的前框架保持到涡轮喷气发动机壳体的保持组件。 该组件包括至少一个将前框架连接到涡轮喷气发动机壳体的连接凸缘，以及用于锁定连接凸缘的系统。 该系统包括枢转地安装在连接凸缘的两个相对端的一个上的致动柄，以及插入在两个相对端的另一端和致动手柄的一部分之间的连杆。 系统将两个相对的端部锁定在一起，并且致动手柄包括设置有凹槽的支撑件和用于调节槽的自由长度的螺钉。 此外，连杆在其一端具有在凹槽中枢转和滑动的轴。