公开(公告)号：US09611030B2

公开(公告)日：2017-04-04

申请号：US14655135

申请日：2013-12-16

Applicant: EUROPEAN AERONAUTIC DEFENCE AND SPACE COMPANY EADS FRANCE

Inventor： Caroline Petiot ,  Michel Bermudez ,  Didier Mesnage

IPC: B64C1/00 ,  B64C7/00 ,  B64C1/06 ,  B64C3/20 ,  B64C11/26 ,  F01D21/04 ,  B64C11/20

CPC classification number: B64C7/00 ,  B64C1/062 ,  B64C3/20 ,  B64C11/205 ,  B64C11/26 ,  B64C2001/0072 ,  F01D21/045 ,  Y02T50/43 ,  Y02T50/672

Abstract: A device for absorbing kinetic energy for an aircraft structural element undergoing a dynamic impact. The device includes an outer enclosure made from a braided composite material configured to preserve its integrity after an impact, a foam core, contained in the outer enclosure and to at least partially fill the outer enclosure. The foam core is configured to at least partially absorb the kinetic energy generated by the impact. Reinforcing elements are integrated at least partially into the foam core to dissipate, combined with the form core, the kinetic energy generated by the impact. The reinforcing elements includes discontinuous threads inserted into the foam core by stitching, and each discontinuous thread includes an L- or T-shaped head, folded down outside the outer enclosure.

公开(公告)号：US10029441B2

公开(公告)日：2018-07-24

申请号：US14655303

申请日：2013-12-16

Applicant: EUROPEAN AERONAUTIC DEFENCE AND SPACE COMPANY EADS FRANCE

Inventor： Caroline Petiot ,  Michel Bermudez ,  Didier Mesnage

IPC: B32B5/24 ,  B23P15/00 ,  B64C3/28 ,  B64C11/20 ,  B64C27/473 ,  F41H5/04 ,  F42D5/045 ,  B32B1/00

Abstract: A device for absorbing kinetic energy for an aircraft structural element undergoing a dynamic impact. The device includes an outer enclosure made from a braided composite material configured to preserve its integrity after an impact, and a foam core contained in the outer enclosure and to at least partially fill the outer enclosure. The foam core configured to at least partially absorb the kinetic energy generated by the impact. Reinforcing elements include at least one dry composite fiber preform integrated into the foam core to dissipate, in combination with the foam core, the kinetic energy generated by the impact. A method for integrating the device for absorbing kinetic energy.

公开(公告)号：US20140290977A1

公开(公告)日：2014-10-02

申请号：US14117054

申请日：2012-05-15

Applicant: EUROPEAN AERONAUTIC DEFENCE AND SPACE COMPANY EADS FRANCE

Inventor： Jesus Aspas Puertolas ,  Nicolas Maisonnave ,  Mathieu Sauzedde ,  Michel Bermudez

IPC: H01B7/02 ,  H01B13/06

CPC classification number: H01B7/02 ,  H01B7/0838 ,  H01B13/06 ,  H01B13/103 ,  Y10T29/49117

Abstract: A strip of a semi-finished product (101, 102), suitable for being deposited by lay-up, for the constitution of a laminated composite material, includes, according to a cross-section and over all its length: a first conductive layer (105, 106), made of an electric conductive material; two electric insulating layers (121, 122), made of a dielectric material completely surrounding the conductive layer (105, 106), the cross sectional width of which is greater than the width of the conductive layer; and two bonding layers (111, 112), extending in thickness on either side of the insulating layers (121, 122), on the exterior of the strip (101, 102). A method for the continuous production of such a strip is also described.

Abstract translation: 根据横截面并且其全部长度，适于通过层叠沉积的半成品条（101,102）用于层压复合材料的构造包括：第一导电层 （105,106），由导电材料制成; 两个电绝缘层（121,122）由完全包围导电层（105,106）的电介质材料制成，其横截面宽度大于导电层的宽度; 以及在所述条带（101,102）的外部上在所述绝缘层（121,122）的任一侧上厚度延伸的两个接合层（111,112）。 还描述了连续生产这种条带的方法。