公开(公告)号：US09108721B2

公开(公告)日：2015-08-18

申请号：US13775471

申请日：2013-02-25

Applicant: Airbus Operations, S.L.

Inventor： Yolanda De Gregorio Hurtado ,  Alberto Balsa Gonzalez

IPC: B64C3/28 ,  B64C5/00 ,  B64C3/20 ,  B64C3/14

CPC classification number: B64C3/28 ,  B64C3/20 ,  B64C5/00 ,  B64C2003/147

Abstract: The invention discloses a trailing edge (2) of an aircraft aerodynamic surface, which comprises an upper skin (6) and a lower skin (7), being the upper and lower skins (6, 7) made of composite material. In the trailing edge (2) a lightweight part (1) is assembled at an end section (13) of the upper and lower skins (6, 7). The lightweight part (1) is covered by a metallic sheet (8), and has a “V”-shaped cross section with arms and peak, where the peak of the “V”-shaped cross section has a rounded shape and is located opposite the end section (13) of the upper and lower skins (6, 7).

Abstract translation: 本发明公开了一种飞机空气动力学表面的后缘（2），其包括由复合材料制成的上皮和下皮（6,7）的上皮（6）和下皮（7）。 在后缘（2）中，将轻质部件（1）组装在上皮和下皮（6,7）的端部（13）处。 轻质部件（1）由金属板（8）覆盖，并具有“V”形横截面，具有臂和峰，其中“V”形横截面的峰值具有圆形并位于 与上皮和下皮（6,7）的端部（13）相对。

公开(公告)号：US20140017445A1

公开(公告)日：2014-01-16

申请号：US13928047

申请日：2013-06-26

Applicant: Airbus Operations, S.L.

Inventor： Alberto Balsa Gonzalez ,  Jose Javier Almendros Gomez ,  Narciso Rodriguez Garcia ,  Maria Rocio Fernando Magarzo

IPC: B23P6/00 ,  F16B5/04

CPC classification number: B23P6/00 ,  B29C73/04 ,  B29C2073/268 ,  F16B5/04 ,  Y10T29/49732 ,  Y10T29/49739 ,  Y10T428/24322

Abstract: The present invention relates to a repair part and to a repair method. The repair part is an elongated part made of a composite material comprising two attached portions forming an angle and holes in each portion arranged in the direction of the line joining both portions. The repair method includes: providing a fragment of a repair part, being long enough to cover the damaged area of the part to be repaired, maintaining a border for fixing the fragment of the repair part; making holes in both portions of the part to be repaired, such that the distance between the centers of consecutive repair holes is the same as the distance between the centers of the consecutive holes; and attaching the fragment of the repair part to the part to be repaired.

Abstract translation: 本发明涉及修理部件和修理方法。 修复部分是由复合材料制成的细长部件，该复合材料包括形成角度的两个附接部分和沿连接两个部分的线的方向布置的每个部分中的孔。 修复方法包括：提供修复部分的片段，其长度足以覆盖待修复部件的损坏区域，保持用于固定修复部分的片段的边界; 在要修复的部件的两个部分中形成孔，使得连续修复孔的中心之间的距离与连续孔的中心之间的距离相同; 并将修理部分的片段附着到要修复的部件上。