A platform for research: civil engineering, architecture and urbanism
A platform for research: civil engineering, architecture and urbanism
HATCH LOCKING DEVICE, AIR- OR SPACECRAFT HATCH AND AIR- OR SPACECRAFT
The present invention provides a hatch locking device (100) for an aircraft or spacecraft hatch (10), comprising: a drivable spindle drive (101) which extends in a longitudinal axis (X) and is fixed in relation to a hatch frame (11) of the aircraft or spacecraft hatch (10) along the longitudinal axis (X); at least one locking bolt (102) which is driven by the drivable spindle drive (101) and is guided along the longitudinal axis (X); and at least one adjustment bush assembly (110) being mounted on a fuselage frame (1) and comprising a first eccentric bush (111) having a bolt receptacle (112) which is oriented centrally along the longitudinal axis (X) for receiving the at least one locking bolt (102) such that the hatch locking device (100) is positive-locking connectable in two axles (Y, Z) both being perpendicular to the longitudinal axis (X). Further the present invention provides an aircraft or spacecraft hatch (10) comprising such hatch locking device (100) as well as an aircraft (A) comprising such aircraft or spacecraft hatch (10).
HATCH LOCKING DEVICE, AIR- OR SPACECRAFT HATCH AND AIR- OR SPACECRAFT
The present invention provides a hatch locking device (100) for an aircraft or spacecraft hatch (10), comprising: a drivable spindle drive (101) which extends in a longitudinal axis (X) and is fixed in relation to a hatch frame (11) of the aircraft or spacecraft hatch (10) along the longitudinal axis (X); at least one locking bolt (102) which is driven by the drivable spindle drive (101) and is guided along the longitudinal axis (X); and at least one adjustment bush assembly (110) being mounted on a fuselage frame (1) and comprising a first eccentric bush (111) having a bolt receptacle (112) which is oriented centrally along the longitudinal axis (X) for receiving the at least one locking bolt (102) such that the hatch locking device (100) is positive-locking connectable in two axles (Y, Z) both being perpendicular to the longitudinal axis (X). Further the present invention provides an aircraft or spacecraft hatch (10) comprising such hatch locking device (100) as well as an aircraft (A) comprising such aircraft or spacecraft hatch (10).
HATCH LOCKING DEVICE, AIR- OR SPACECRAFT HATCH AND AIR- OR SPACECRAFT
KLAPPENVERRIEGELUNGSVORRICHTUNG, LUFT- ODER RAUMFAHRZEUGKLAPPE UND LUFT- ODER RAUMFAHRZEUG
DISPOSITIF DE VERROUILLAGE DE TRAPPE, TRAPPE D'AIR OU D'ENGIN SPATIAL ET ENGIN SPATIAL
OHLE SÖREN (author)
2024-06-26
Patent
Electronic Resource
English
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