公开(公告)号：US09643713B2

公开(公告)日：2017-05-09

申请号：US14426955

申请日：2013-09-09

Applicant: AIRBUS GROUP SAS

Inventor： Michel Bermudez ,  Didier Mesnage ,  Hichem Smaoui ,  Benoit Fleury

IPC: H01G9/155 ,  B64C7/00 ,  B64D41/00 ,  B64C1/12 ,  B64C1/40 ,  H01G11/58 ,  H01G11/78 ,  B64C1/00

CPC classification number: B64C7/00 ,  B64C1/12 ,  B64C1/40 ,  B64C2001/0072 ,  B64D41/00 ,  H01G11/58 ,  H01G11/78 ,  Y02T50/43 ,  Y10T29/435 ,  Y10T29/49622

Abstract: A method of manufacturing a stiffened panel having a skin and at least one substantially elongate stiffener having a longitudinal groove forming a cavity. At least one storage device for storing and releasing electrical energy. The longitudinal groove is filled with at least one storage device for storing and releasing electrical energy. The storage device is covered with a skin which forms the cavity together with the longitudinal groove of the stiffener. A stiffened ring can be derived from the method.

公开(公告)号：US10410759B2

公开(公告)日：2019-09-10

申请号：US15527900

申请日：2015-11-19

Applicant: AIRBUS GROUP SAS ,  Gerard Guilbert

Inventor： Didier Mesnage ,  Thierry Pelegrin

IPC: B29C70/88 ,  B32B15/088 ,  B32B15/20 ,  H01B7/00 ,  H01B7/02 ,  H01B7/04 ,  B64C1/06 ,  B29K105/24 ,  B29K77/00 ,  B29K309/08 ,  B29L31/30 ,  B64C1/00

Abstract: A conductive device to form electrical connections on the surface of a structure made of composite material. The device includes a thin interface layer having a face via which the device is fixed to the surface of the structure made of composite material. A conductive metal element is placed on the face of the interface layer opposite the face making contact with the surface of the structure. The conductive element is configured to be able to undergo tensile and compressive stresses without damage. A protective layer is configured to protect the conductive element from attack from the environment surrounding the structure. These various elements are arranged relative to one another such that the length of the conductive element can vary as a function of temperature variations independently of the amplitude of the variations undergone by the structure on which the device is mounted.

公开(公告)号：US20150225073A1

公开(公告)日：2015-08-13

申请号：US14426955

申请日：2013-09-09

Applicant: AIRBUS GROUP SAS

Inventor： Michel Bermudez ,  Didier Mesnage ,  Hichem Smaoui ,  Benoit Fleury

IPC: B64C7/00 ,  B64D41/00 ,  B64C1/40 ,  H01G11/58 ,  H01G11/78

CPC classification number: B64C7/00 ,  B64C1/12 ,  B64C1/40 ,  B64C2001/0072 ,  B64D41/00 ,  H01G11/58 ,  H01G11/78 ,  Y02T50/43 ,  Y10T29/435 ,  Y10T29/49622

Abstract: A method of manufacturing a stiffened panel having a skin and at least one substantially elongate stiffener having a longitudinal groove forming a cavity. At least one storage device for storing and releasing electrical energy. The longitudinal groove is filled with at least one storage device for storing and releasing electrical energy. The storage device is covered with a skin which forms the cavity together with the longitudinal groove of the stiffener. A stiffened ring can be derived from the method.

Abstract translation: 一种制造具有皮肤的加强板的方法和具有形成空腔的纵向槽的至少一个基本上细长的加强件。 用于存储和释放电能的至少一个存储装置。 纵向凹槽填充有用于存储和释放电能的至少一个存储装置。 存储装置被覆盖有与加强件的纵向槽一起形成空腔的皮肤。 可以从该方法得到加强环。