公开(公告)号：US09169022B2

公开(公告)日：2015-10-27

申请号：US14331152

申请日：2014-07-14

Applicant: EADS SOGERMA

Inventor： Lionel Bacquey ,  Remy Barre ,  Laurent Cecinas ,  Julien Normandin

IPC: B60R21/00 ,  B64D11/06 ,  B64C1/18 ,  B60N2/50

CPC classification number: B64D11/0696 ,  B60N2/502 ,  B60N2/509 ,  B64C1/18 ,  B64D11/06 ,  B64D11/0619 ,  B64D11/064 ,  B64D11/0689

Abstract: A seat-floor assembly for a vehicle comprises a floor element and at least one monobeam seat fixed to the floor element by a beam. A seat cushion and a seat backrest fixed to the beam. The floor element comprises a stiffened panel structure, one face of which forms a top sole of at least one floor crossmember. The floor element further comprises a housing receptacle open on the top sole and fixed to the top sole and/or to the at least one floor crossmember. At least one monobeam seat is fixed to the beam. An aircraft fuselage comprises a floor with such seat-floor assemblies and reinforced by the structure of the floor elements.

Abstract translation: 用于车辆的座椅地板组件包括地板元件和通过梁固定到地板元件的至少一个单体座椅座椅。 固定在梁上的座垫和座椅靠背。 地板元件包括加强板结构，其一面形成至少一个地板横梁的顶部鞋底。 地板元件还包括在顶部鞋底上敞开并固定到顶部鞋底和/或至少一个地板横梁上的壳体容器。 至少一个monobeam座椅固定在梁上。 飞机机身包括具有这种座椅地板组件的地板，并通过地板元件的结构加固。

公开(公告)号：US09604725B2

公开(公告)日：2017-03-28

申请号：US13911271

申请日：2013-06-06

Applicant: EADS SOGERMA

Inventor： Laurent Cecinas ,  Julien Normandin ,  Remy Barre ,  Lionel Bacquey

IPC: B60N2/42 ,  B60R21/00 ,  B64D11/06 ,  B60N2/427 ,  B64D25/04 ,  B60N2/20 ,  B60N2/30 ,  B60N2/16

CPC classification number: B64D11/0696 ,  B60N2/16 ,  B60N2/20 ,  B60N2/3031 ,  B60N2/3065 ,  B60N2/309 ,  B60N2/4242 ,  B60N2/427 ,  B60N2/42709 ,  B64D11/06 ,  B64D11/0619 ,  B64D11/064 ,  B64D11/0649 ,  B64D11/0689 ,  B64D25/04 ,  Y02T50/46

Abstract: An aircraft seat includes a seat bucket that is integral by its seatback with a single beam oriented along an axis that is approximately perpendicular to the aircraft floor, which beam is integral with fastening points located on at least two separate lines on the aircraft floor.

公开(公告)号：US09421886B2

公开(公告)日：2016-08-23

申请号：US14553938

申请日：2014-11-25

Applicant: EADS SOGERMA

Inventor： Laurent Cecinas ,  Christian Morais

IPC: B60N2/42 ,  B60N2/16 ,  B64D11/06 ,  B60N2/10 ,  B60N2/427 ,  B60N2/68 ,  B64D25/04 ,  B63B29/04

CPC classification number: B60N2/16 ,  B60N2/10 ,  B60N2/42709 ,  B60N2/42718 ,  B60N2/42736 ,  B60N2/68 ,  B63B2029/043 ,  B64D11/0619 ,  B64D11/064 ,  B64D11/0689 ,  B64D25/04

Abstract: A seat having a bucket and a supporting structure on which the bucket is fixed. The height of the bucket on the supporting structure is adjustable. A lower sub-assembly of the supporting structure forms a seat subframe and of which at least one bucket support is mounted movable in height following at least one lower guide rail. An upper sub-assembly of the supporting structure is assembled movable in rotation relative to the lower sub-assembly around a pivot axis which is situated close to a lower end of the lower guide rails and situated close to a lower end of the upper sub-assembly. The bucket is fixed to the bucket support in an articulated manner at the seat base and has at least one guide element fixed to the backrest and sliding in an upper guide rail of the upper sub-assembly situated above the lower guide rails.

Abstract translation: 具有铲斗和支撑结构的座椅，其上固定有铲斗。 支撑结构上的铲斗的高度是可调节的。 支撑结构的下部子组件形成座椅子框架，并且其中至少一个铲斗支撑件安装成可沿着至少一个下部导轨移动高度。 支撑结构的上部子组件组装成可相对于下部子组件旋转地围绕枢转轴线移动，所述枢转轴线位于靠近下部导轨的下端并且靠近上部子组件的下端， 部件。 铲斗在座椅基座处以铰接的方式固定到铲斗支撑件，并且具有固定到靠背并且在位于下导轨上方的上子组件的上导轨中滑动的至少一个引导元件。

公开(公告)号：US09399518B2

公开(公告)日：2016-07-26

申请号：US14559137

申请日：2014-12-03

Applicant: EADS SOGERMA

Inventor： Laurent Cecinas ,  Nicolas Taraud

IPC: B64D11/06 ,  F16D55/08 ,  B60N2/427 ,  F16F7/04 ,  B60N2/42

CPC classification number: B64D11/0619 ,  B60N2/4242 ,  B60N2/42736 ,  F16D55/08 ,  F16F7/04

Abstract: An energy absorber (100) to limit an acceleration force experienced by a heavy body, such as an occupant of a seat subjected to the acceleration of an aircraft crash, comprises a winding drum (10) mounted in rotation around a shaft (13), around which a traction line (11) is wound. The shaft is coupled mechanically to a brake (20) that immobilizes the shaft (13) in rotation when a torque applied to the shaft by the traction line is less than the maximum brake torque that can be generated by the brake and that when the shaft (13) is in rotation generates a torque that is approximately constant and equal to the maximum brake torque.A control element (40) acting on the brake (20) makes it possible to modify the value of the maximum brake torque and thus to adapt the energy absorber to the mass of the heavy body to maintain an acceleration experienced at a desired value for different masses.