Method for assembling a primary structure of an aircraft pylon
US10800549B2 · kind B2 · utility
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1References
7Claims
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Key dates
| Filing date | Oct 2, 2018 |
| Grant date | Oct 13, 2020 |
| Priority date | — |
| Expiry date | Oct 13, 2038 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64F5/00
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A method for assembling a primary structure of an aircraft pylon, includes a step of fixing an angle bracket to each of the first and second lateral panels such as to obtain an L form for each of the first and second lateral panels prior to a placement of said L forms each placed against two sides of each transverse frame. This assembly technique makes it possible to reduce the mounting clearances such that it is unnecessary to fit shims, resulting in a reduction of mounting time and manufacturing costs.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.