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MECHANISM FOR INDICATING POSITION OF A LATCH MECHANISM FOR AN AIRCRAFT NACELLE
An aircraft nacelle (10) is disclosed and includes a first fan cowl (20A) and a second fan cowl (20B). An opening (94) is defined in an exterior surface of the first fan cowl (20A). The aircraft nacelle (10) also includes a blade (64), a latch mechanism (50), an arm (110), and a linkage assembly (142) operably connecting the arm (110) to the blade (64). The blade (64) is moveable along between a stowed position and a deployed position. The latch mechanism (50) is moveable between a latched position an unlatched position where a portion of the latch mechanism (50) obstructs a path of movement of the blade (64). The arm (110) is unable to move from an extended position where a portion of the arm (110) extends through the opening (94) in the exterior surface (8) of the aircraft nacelle (10) into a retracted position within an interior volume of the aircraft nacelle (10) when the blade (64) is in the deployed position and the latch mechanism (50) is in the unlatched position.
MECHANISM FOR INDICATING POSITION OF A LATCH MECHANISM FOR AN AIRCRAFT NACELLE
An aircraft nacelle (10) is disclosed and includes a first fan cowl (20A) and a second fan cowl (20B). An opening (94) is defined in an exterior surface of the first fan cowl (20A). The aircraft nacelle (10) also includes a blade (64), a latch mechanism (50), an arm (110), and a linkage assembly (142) operably connecting the arm (110) to the blade (64). The blade (64) is moveable along between a stowed position and a deployed position. The latch mechanism (50) is moveable between a latched position an unlatched position where a portion of the latch mechanism (50) obstructs a path of movement of the blade (64). The arm (110) is unable to move from an extended position where a portion of the arm (110) extends through the opening (94) in the exterior surface (8) of the aircraft nacelle (10) into a retracted position within an interior volume of the aircraft nacelle (10) when the blade (64) is in the deployed position and the latch mechanism (50) is in the unlatched position.
MECHANISM FOR INDICATING POSITION OF A LATCH MECHANISM FOR AN AIRCRAFT NACELLE
MECHANISMUS ZUR ANZEIGE DER POSITION EINES VERRIEGELUNGSMECHANISMUS FÜR EINE FLUGZEUGGONDEL
MÉCANISME D'INDICATION DE POSITION D'UN MÉCANISME DE VERROUILLAGE POUR UNE NACELLE D'AÉRONEF
THOMAS KYLE A (author) / TOLIVER RHODA REBECCA (author) / ROETHLE MICHAEL (author) / SENESAC MATTHEW (author) / WOERLY MATTHEW JOSEPH (author) / SACHDEVA KUSHY (author)
2021-10-27
Patent
Electronic Resource
English
IPC:
B64D
Ausrüstung für Flugzeuge
,
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
/
B64C
AEROPLANES
,
Flugzeuge
/
E05B
LOCKS
,
Schlösser
/
E05C
Riegel oder Feststellvorrichtungen für Flügel, insbesondere für Türen oder Fenster
,
BOLTS OR FASTENING DEVICES FOR WINGS, SPECIALLY FOR DOORS OR WINDOWS
/
F01D
Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen
,
NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
Mechanism for indicating position of a latch mechanism for an aircraft nacelle
| European Patent Office | 2021
MECHANISM FOR INDICATING POSITION OF A LATCH MECHANISM FOR AN AIRCRAFT NACELLE
| European Patent Office | 2020