Patent · US Active

Method for assembling an aircraft pylon and aircraft pylon obtained by this method

US12054271B2 · kind B2 · utility

0Cited by
2References
12Claims
0Family size

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Key dates

Filing dateAug 2, 2021
Grant dateAug 6, 2024
Priority date
Expiry dateFeb 13, 2042

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64F5/10
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A method for assembling an aircraft pylon including a primary structure and at least one internal system positioned at least partially within the primary structure, wherein the assembly method includes a first step of assembling a part of the primary structure so that the interior of the primary structure remains accessible, a step of mounting an internal systems module including at least one support and at least one internal system connected to the support, a second step of assembling the internal systems module and the partially assembled primary structure, a third step of assembling any element of the primary structure not assembled in the first assembly step, and an aircraft pylon assembled by such a method.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.