A hatch locking device (100) for an aircraft or spacecraft hatch (10) including: a drivable spindle drive (101) with a longitudinal axis (X) and fixed relative to a hatch frame (11, 10) along the longitudinal axis (X); a locking bolt (102) driven by the drivable spindle drive (101) and guided along the longitudinal axis (X); and an adjustment bush assembly (110) mounted on a fuselage frame (1) and including a first eccentric bush (111) having a bolt receptacle (112) oriented centrally along the longitudinal axis (X) to receive the locking bolt (102). The hatch locking device (100) is positive-locking connectable in two axles (Y, Z) both perpendicular to the longitudinal axis (X).
HATCH LOCKING DEVICE, AIR- OR SPACECRAFT HATCH AND AIR- OR SPACECRAFT
2024-06-20
Patent
Elektronische Ressource
Englisch
HATCH LOCKING DEVICE, AIR- OR SPACECRAFT HATCH AND AIR- OR SPACECRAFT
Europäisches Patentamt | 2024
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Worldwide Spacecraft Crew Hatch History
NTIS | 2009
|Worldwide Spacecraft Crew Hatch History
NTRS | 2009
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