LINK FOR AIRCRAFT COMPONENT MOUNTING

A gas turbine engine mount (50) for an aircraft wing including a link body (200) having a first joint (210; 510), a second joint (220; 520) and a linking structure (230; 530) connecting the first joint (210; 510) to the second joint (220; 520). The linking structure (230; 530) includes at least a fl...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
1. Verfasser:	HUSBAND, Jason
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	A gas turbine engine mount (50) for an aircraft wing including a link body (200) having a first joint (210; 510), a second joint (220; 520) and a linking structure (230; 530) connecting the first joint (210; 510) to the second joint (220; 520). The linking structure (230; 530) includes at least a flexing portion (234; 534) and an elastic portion. The flexing portion (234; 534) is configured to flex during a load outside of an expected load window.