THRUST REVERSER WITH BLOCKER DOOR SYSTEM

THRUST REVERSER WITH BLOCKER DOOR SYSTEM

An assembly is provided for an aircraft propulsion system (10). This assembly includes a fixed structure (48), a translating structure (50), a blocker door (46) and a rigid linkage (74). The translating structure (50) is configured to translate relative to the fixed structure (48). The blocker door...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: SANZ MARTINEZ, Pablo T, AZIZ, Peter W
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
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Beschreibung
Zusammenfassung:An assembly is provided for an aircraft propulsion system (10). This assembly includes a fixed structure (48), a translating structure (50), a blocker door (46) and a rigid linkage (74). The translating structure (50) is configured to translate relative to the fixed structure (48). The blocker door (46) extends between a blocker door first end (82) and a blocker door second end (86). The translating structure (50) is pivotally attached to the blocker door (46) at the blocker door first end (82). The rigid linkage (74) includes a first pivot attachment, a second pivot attachment and a third pivot attachment. The first pivot attachment is coupled to the fixed structure (48). The second pivot attachment is coupled to the translating structure (50). The third pivot attachment is coupled to the blocker door (46) at the blocker door second end (86).