公开(公告)号：US20170259899A1

公开(公告)日：2017-09-14

申请号：US15444498

申请日：2017-02-28

Applicant: Airbus Operations, S.L.

Inventor： Felipe Abellán Alzallu ,  Alberto Ramos Guerrero ,  Adolfo Ávila Gutierrez ,  Juan Carlos Monje Martin

IPC: B64C1/06

CPC classification number: B64C1/068 ,  B64C1/061 ,  B64C1/065 ,  B64C1/26 ,  B64C5/02

Abstract: A harness routing electrically connects a rear fuselage section of an aircraft and a trimmable Horizontal Tail Plane (HTP) installed at this rear section. The aircraft rear section includes a first clipping point wherein the harness is attached to a fuselage frame located in front of the torsion box front spar, and a second clipping point wherein the harness is attached to a front spar of the HTP torsion box. The second clipping point is located downstream the first clipping point from the fuselage towards the torsion box interior, and the harness passes through the front spar towards the interior of the torsion box downstream the second clipping point. The harness installation and routing is optimized, in order to reduce harness length and weight, but at the same time assuring that any damage to the harness cables are prevented during the entire aircraft operative life.

公开(公告)号：US10549836B2

公开(公告)日：2020-02-04

申请号：US15444498

申请日：2017-02-28

Applicant: Airbus Operations, S.L.

Inventor： Felipe Abellán Alzallu ,  Alberto Ramos Guerrero ,  Adolfo Ávila Gutierrez ,  Juan Carlos Monje Martin

IPC: B64C1/06

Abstract: A harness routing electrically connects a rear fuselage section of an aircraft and a trimmable Horizontal Tail Plane (HTP) installed at this rear section. The aircraft rear section includes a first clipping point wherein the harness is attached to a fuselage frame located in front of the torsion box front spar, and a second clipping point wherein the harness is attached to a front spar of the HTP torsion box. The second clipping point is located downstream from the first clipping point from the fuselage towards the torsion box interior, and the harness passes through the front spar towards the interior of the torsion box downstream the second clipping point.