公开(公告)号：US10125721B2

公开(公告)日：2018-11-13

申请号：US14987302

申请日：2016-01-04

Applicant: AIRCELLE

Inventor： Olivier Kerbler ,  Olivier Gilo ,  Patrick Gonidec

IPC: F02K1/12 ,  B64D29/06 ,  B64D33/04 ,  B64C15/02 ,  F02K1/76

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.

公开(公告)号：US09382845B2

公开(公告)日：2016-07-05

申请号：US13922614

申请日：2013-06-20

Applicant: AIRCELLE

Inventor： Herve Hurlin ,  Olivier Kerbler ,  Olivier Gilo

IPC: F02K1/06 ,  F02C7/20 ,  F02K1/08

CPC classification number: F02C7/20 ,  F02K1/085 ,  Y02T50/672

Abstract: An inner structure for a nacelle for an aircraft turbofan includes a plurality of active and passive movable portions. Each active movable portion can drive adjacent passive movable portions such that the inner structure has a nominal first position, a second position and a third position. In the second position, the active movable portions project beyond by the passive movable portions toward the outside of the inner structure after the active mobile portions have driven the passive mobile portions. In the third position, the active movable portions project beyond the passive movable portions toward the inside of the inner structure after the active mobile portions have driven the passive mobile portions. The present disclosure also relates to a nacelle having an outer structure and such an inner structure.

Abstract translation: 用于飞机涡扇风机的机舱的内部结构包括多个主动和可动的可移动部分。 每个有源可移动部分可以驱动相邻的被动可动部分，使得内部结构具有标称的第一位置，第二位置和第三位置。 在第二位置，主动移动部分驱动被动移动部分之后，主动可移动部分在无源可移动部分之外突出到内部结构的外部。 在第三位置，主动移动部分驱动被动移动部分之后，主动可移动部分突出超过被动可移动部分朝向内部结构的内部。 本公开还涉及具有外部结构和这种内部结构的机舱。

公开(公告)号：US20140140830A1

公开(公告)日：2014-05-22

申请号：US13922614

申请日：2013-06-20

Applicant: AIRCELLE

Inventor： Herve Hurlin ,  Olivier Kerbler ,  Olivier Gilo

IPC: F02C7/20

CPC classification number: F02C7/20 ,  F02K1/085 ,  Y02T50/672

Abstract: An inner structure for a nacelle for an aircraft turbofan includes a plurality of active and passive movable portions. Each active movable portion can drive adjacent passive movable portions such that the inner structure has a nominal first position, a second position and a third position. In the second position, the active movable portions project beyond by the passive movable portions toward the outside of the inner structure after the active mobile portions have driven the passive mobile portions. In the third position, the active movable portions project beyond the passive movable portions toward the inside of the inner structure after the active mobile portions have driven the passive mobile portions. The present disclosure also relates to a nacelle having an outer structure and such an inner structure.

Abstract translation: 用于飞机涡扇风机的机舱的内部结构包括多个主动和可动的可移动部分。 每个有源可移动部分可以驱动相邻的被动可动部分，使得内部结构具有标称的第一位置，第二位置和第三位置。 在第二位置，主动移动部分驱动被动移动部分之后，主动可移动部分在无源可移动部分之外突出到内部结构的外部。 在第三位置，主动移动部分驱动被动移动部分之后，主动可移动部分突出超过被动可移动部分朝向内部结构的内部。 本公开还涉及具有外部结构和这种内部结构的机舱。