Lock for a turbofan engine thrust reverser
A cascade type thrust reverser for an air duct of a turbofan engine includes a lock mechanism mounted on a track beam (14L) that supports a translating sleeve. A locking portion (42L) of a lock pin (42) of the lock mechanism is engageable with a slideway (48) by which the translating sleeve is suppo...
Gespeichert in:
| Hauptverfasser: | , |
|---|---|
| Format: | Patent |
| Sprache: | eng ; fre ; ger |
| Schlagworte: | |
| Online-Zugang: | Volltext bestellen |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| Zusammenfassung: | A cascade type thrust reverser for an air duct of a turbofan engine includes a lock mechanism mounted on a track beam (14L) that supports a translating sleeve. A locking portion (42L) of a lock pin (42) of the lock mechanism is engageable with a slideway (48) by which the translating sleeve is supported by the track beam to lock the translating sleeve in the forward, closed position. The lock pin is recieved adjacent and rearward of the rearward end of the sleeve. |
|---|