THRUST REVERSER WITH BLOCKER DOOR FOLDING LINKAGE

An assembly for an aircraft propulsion system (20) includes a fixed structure (60), a translating structure (62) and a thrust reverser (36). The thrust reverser (36) includes a blocker door (58), a door link (102) and a structure link (100). The blocker door (58) is pivotally coupled to the translat...

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Bibliographische Detailangaben
1. Verfasser:	GORMLEY, Timothy
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
Online-Zugang:	Volltext bestellen
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Beschreibung
Zusammenfassung:	An assembly for an aircraft propulsion system (20) includes a fixed structure (60), a translating structure (62) and a thrust reverser (36). The thrust reverser (36) includes a blocker door (58), a door link (102) and a structure link (100). The blocker door (58) is pivotally coupled to the translating structure (62). The door link (102) includes a first door link arm (124A), a second door link arm (124B) and a door link mount (126) connected to the first door link arm (124A) and the second door link arm (124B). The first door link arm (124A) and the second door link arm (124B) are each pivotally coupled to the blocker door (58). The first door link arm (124A) and the second door link arm (124B) laterally converge towards one another as the first door link arm (124A) and the second door link arm (124B) extend longitudinally towards the door link mount (126). The structure link (100) extends longitudinally between and is pivotally coupled to the door link mount (126) and the fixed structure (60).