公开(公告)号：US20150152811A1

公开(公告)日：2015-06-04

申请号：US14597352

申请日：2015-01-15

Applicant: AIRCELLE

Inventor： Olivier KERBLER ,  Olivier GILO ,  Pierre CARUEL

IPC: F02K1/76 ,  F02K1/12 ,  B64D33/04

CPC classification number: F02K1/763 ,  B64D33/04 ,  F02K1/12 ,  F02K1/1207 ,  F02K1/70 ,  F02K1/76 ,  F05D2260/50

Abstract: A device is provided to drive flaps for an adaptive nozzle of a nacelle, and the adaptive nozzle includes at least one flap moveable in rotation and adapted to pivot toward a position causing a variation of a nozzle section. In particular, the device includes a control ring and a connecting rod driving the flaps. The control ring rotates along a circumference of the nacelle during a driving rod drives the control ring, and the connecting rod is connected to the control ring and one of the flaps so that the driving rod causes a displacement in translation of the connecting rod. The driving rod is connected to an assembly forming a lever, and the assembly is secured to the control ring.

Abstract translation: 提供了一种用于驱动用于机舱的自适应喷嘴的​​翼片的装置，并且所述自适应喷嘴包括至少一个可旋转运动的翼片，并且适于朝向引起喷嘴部分变化的位置枢转。 特别地，该装置包括控制环和驱动翼片的连杆。 在驱动杆驱动控制环时，控制环沿着机舱的圆周旋转，并且连杆连接到控制环和其中一个翼片，使得驱动杆引起连杆平移的位移。 驱动杆连接到形成杠杆的组件上，组件固定在控制环上。

公开(公告)号：US20160115902A1

公开(公告)日：2016-04-28

申请号：US14987302

申请日：2016-01-04

Applicant: AIRCELLE

Inventor： Olivier KERBLER ,  Olivier GILO ,  Patrick GONIDEC

IPC: F02K1/12

CPC classification number: F02K1/1261 ,  B64C15/02 ,  B64D29/06 ,  B64D33/04 ,  F02K1/12 ,  F02K1/1207 ,  F02K1/1253 ,  F02K1/763

Abstract: The present disclosure provides a turbojet engine nacelle having a downstream section including a cowl which is ended with a hinged flap constituting a nozzle. In particular, the hinged flap is hingedly and translatably hinged to the cowl.

Abstract translation: 本公开提供了一种涡轮喷气发动机机舱，其具有包括整流罩的下游部分，该整流罩以构成喷嘴的铰接折片结束。 特别地，铰链翼片铰接并可平移地铰接到整流罩。

公开(公告)号：US20150083823A1

公开(公告)日：2015-03-26

申请号：US14558833

申请日：2014-12-03

Applicant: AIRCELLE

Inventor： Hervé HURLIN ,  Olivier GILO ,  Olivier KERBLER

IPC: F02K1/76 ,  F16D11/14

CPC classification number: F02K1/763 ,  F02K1/766 ,  F05D2250/41 ,  F05D2260/4031 ,  F16D11/10 ,  F16D11/14 ,  F16D2011/006

Abstract: A mechanism for coupling and uncoupling a motor inlet shaft and an outlet shaft, in particular, the inlet shaft is mounted in rotation on a front frame, and the outlet shaft is mounted in rotation on a rear frame. The outlet shaft rotates an outlet pinion, and the rear frame is slidably mounted to translate between a forward compact position and a backward deployed position. The mechanism includes a coupler, and first and second lockers to couple or uncouple the inlet and outlet shafts according to the translation of the rear frame between the forward compact position and the backward deployed position. The first locker locks in rotation the inlet shaft on the front frame, the second locker locks the outlet shaft on the rear frame. In particular, the second locker automatically locks the inlet and outlet shafts in rotation respectively, according to the displacement of the rear frame.

Abstract translation: 用于将电动机入口轴和出口轴，特别是入口轴联接和分离的机构旋转安装在前框架上，并且出口轴旋转安装在后框架上。 出口轴使出口小齿轮旋转，并且后框架可滑动地安装以在前部紧凑位置和向后展开位置之间平移。 该机构包括联接器，以及第一和第二储物柜，用于根据在前紧凑位置和向后展开位置之间的后框架的平移来连接或分离入口和出口轴。 第一个储物柜锁定前框架上的入口轴，第二个储物柜将出口轴锁定在后框架上。 特别地，第二储物柜根据后框架的位移自动将入口和出口轴锁定在旋转中。