Aircraft component
A method of manufacturing an aircraft component such as a wing rib. The method comprises: providing a body with two or more connectors (19, 20) arranged in a line on the body, each connector having an arm (35, 41) extending from the body, a first flange (23a) positioned on a first side of the line,...
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Patent |
| Sprache: | chi ; eng |
| Schlagworte: | |
| Online-Zugang: | Volltext bestellen |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| Zusammenfassung: | A method of manufacturing an aircraft component such as a wing rib. The method comprises: providing a body with two or more connectors (19, 20) arranged in a line on the body, each connector having an arm (35, 41) extending from the body, a first flange (23a) positioned on a first side of the line, and a second flange (23b) positioned on a second side of the line; and attaching a separate (30) connector to the body, the separate connector having an arm (35) extending from the body, a first flange positioned on a first side of the line and a second flange positioned on a second side of the line. |
|---|