公开(公告)号：US20240124149A1

公开(公告)日：2024-04-18

申请号：US18351022

申请日：2023-07-12

Applicant: Safran Nacelles

Inventor： Jean-Baptiste DELARUE ,  Laurent Georges VALLEROY ,  Vianney HUS ,  Hugo BOISTELLE

IPC: B64D29/08 ,  B64D29/02

CPC classification number: B64D29/08 ,  B64D29/02

Abstract: An assembly includes a nacelle panel of an aircraft engine, the nacelle panel including an outer skin, an inner skin and a central layer interposed between the outer and inner skins. The central layer has a housing, the outer skin has an opening which opens into the housing, and a linking member extends in the opening and in the housing, the linking member to be connected to an actuator.

公开(公告)号：US20240125283A1

公开(公告)日：2024-04-18

申请号：US18350885

申请日：2023-07-12

Applicant: Safran Nacelles

Inventor： Jean-Baptiste DELARUE ,  Bertrand Léon Marie DESJOYEAUX ,  Moncef M'HASNI

IPC: F02K1/32 ,  B64D29/06

CPC classification number: F02K1/32 ,  B64D29/06 ,  F05D2230/60

Abstract: An assembly including a nacelle panel of an aircraft engine, the nacelle panel including an outer skin, an inner skin and a central layer interposed between the outer skin and the inner skin, and the nacelle panel having a free inner enclosure contiguous with the outer skin, and a member forming a link including one or more degrees of freedom, the member being attached to the nacelle panel solely by one or both of the outer skin and the inner skin, and the member extending facing the free inner enclosure.