ENGINE THRUST REVERSER LOCK

An aircraft engine thrust reverser lock system (100) includes a pin- capturing member (102). The pin-capturing member includes a body that is rotatable about an axis defined by a pivot (104) extending through the body. The body includes an interior surface that defines a slot (150). The slot has an...

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Bibliographische Detailangaben
Hauptverfasser:	CONWAY, GEORGE, STIEG, MICHAEL ALAN, KOPECEK, JOSEPH THOMAS, OZANICH, BRENT MICHAEL, MEARS, JOHN STEPHEN, WILLETT, KENNETH, ANAYA, JESUS
Format:	Patent
Sprache:	eng ; fre
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 aircraft engine thrust reverser lock system (100) includes a pin- capturing member (102). The pin-capturing member includes a body that is rotatable about an axis defined by a pivot (104) extending through the body. The body includes an interior surface that defines a slot (150). The slot has an opening that is sized to receive a pin (110) into the slot. One side of the slot includes a protruded sidewall surface that protrudes into the slot toward an another sidewall surface of the slot. The protruded sidewall surface defines an apex (206) between the open and closed ends of the slot. Between the apex and the closed end of the slot, the protruded sidewall surface faces the rotational axis.