The present invention provides a hatch locking device (100) for an aircraft or spacecraft hatch (10), in particular for a cargo door, comprising: an actuation lever (101) for actuating the hatch locking device (100), wherein the actuation lever (101) is rotatable about a pivot axis (A101) and comprises a protruding section (102); a latch element (103), which is hinged rotatable about a hinge axis (A103) at a hatch frame (11) of the aircraft or spacecraft hatch (10) and configured to be engageable with a corresponding latch counter part (3) of a fuselage frame (2) [such that the hatch locking device 100 is positively locked]; and a connection element (104), which mechanically connects the protruding section (102) and the latch element (103) such that a rotation of the actuation lever (101) causes a rotation of the latch element (103). Further the present invention provides an aircraft or spacecraft hatch (10) comprising such hatch locking device (100) as well as an aircraft (1) comprising such an aircraft or spacecraft hatch (10).
HATCH LOCKING DEVICE, AIRCRAFT OR SPACECRAFT HATCH AND AIRCRAFT OR SPACECRAFT
LUKENVERRIEGELUNGSVORRICHTUNG, LUFT- ODER RAUMFAHRZEUGLUKE UND LUFT- ODER RAUMFAHRZEUG
DISPOSITIF DE VERROUILLAGE DE TRAPPE, TRAPPE D'AÉRONEF OU DE VÉHICULE SPATIAL ET AÉRONEF OU VÉHICULE SPATIAL
2025-04-30
Patent
Electronic Resource
English
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