THRUST REVERSER WITH BLOCKER DOOR OPENING CONTROL DEVICE(S)

An assembly is provided for an aircraft propulsion system (20). This assembly includes a fixed structure (60), a translating structure (62) and a thrust reverser (36). The translating structure (62) is configured to translate between a stowed position and a deployed position. The thrust reverser (36...

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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 is provided for an aircraft propulsion system (20). This assembly includes a fixed structure (60), a translating structure (62) and a thrust reverser (36). The translating structure (62) is configured to translate between a stowed position and a deployed position. The thrust reverser (36) includes a blocker door (58), an actuation linkage (86) and a spring cartridge (176). The blocker door (58) is pivotally coupled to the translating structure (62). The actuation linkage (86) operatively couples the blocker door (58) to the fixed structure (60). The spring cartridge (176) is coupled to the blocker door (58) and the translating structure (62). The spring cartridge (176) is configured to bias the blocker door (58) closed.