Eine Plattform für die Wissenschaft: Bauingenieurwesen, Architektur und Urbanistik
Eine Plattform für die Wissenschaft: Bauingenieurwesen, Architektur und Urbanistik
HINGE ASSEMBLY, AS WELL AS STORAGE COMPARTMENT OR MONUMENT FOR INSTALLATION IN AN AIRCRAFT OR SPACECRAFT CABIN
The invention relates to a hinge assembly (1; 1') for pivotably coupling two components in an aircraft or spacecraft cabin, in particular for pivotably attaching a door (107) of an overhead storage compartment (102). The hinge assembly comprises a first hinge part (2) and a second hinge part (3) arranged and coupled so as to be pivotable relative to each other about a hinge axis (A), an elastic element (5) capable of providing an elastic torque about the hinge axis (A), and a torque-adjustment piece (6; 6', 6a', 6b'). The elastic element is coupled to each of the first hinge part and the torque-adjustment piece in a torque-transmitting manner. The hinge assembly includes a positive engagement device (7; 7') configured to be kept positively engaged by elastic action so as to prevent a rotation of the torque-adjustment piece at least in a first direction of rotation (R1), and capable of being disengaged against the elastic action so as to enable a rotation of the torque-adjustment piece in a second direction of rotation (R2) opposite to the first direction of rotation (R1) against a torque provided by the elastic element in order to apply a torsional pre-load to the elastic element.
HINGE ASSEMBLY, AS WELL AS STORAGE COMPARTMENT OR MONUMENT FOR INSTALLATION IN AN AIRCRAFT OR SPACECRAFT CABIN
The invention relates to a hinge assembly (1; 1') for pivotably coupling two components in an aircraft or spacecraft cabin, in particular for pivotably attaching a door (107) of an overhead storage compartment (102). The hinge assembly comprises a first hinge part (2) and a second hinge part (3) arranged and coupled so as to be pivotable relative to each other about a hinge axis (A), an elastic element (5) capable of providing an elastic torque about the hinge axis (A), and a torque-adjustment piece (6; 6', 6a', 6b'). The elastic element is coupled to each of the first hinge part and the torque-adjustment piece in a torque-transmitting manner. The hinge assembly includes a positive engagement device (7; 7') configured to be kept positively engaged by elastic action so as to prevent a rotation of the torque-adjustment piece at least in a first direction of rotation (R1), and capable of being disengaged against the elastic action so as to enable a rotation of the torque-adjustment piece in a second direction of rotation (R2) opposite to the first direction of rotation (R1) against a torque provided by the elastic element in order to apply a torsional pre-load to the elastic element.
HINGE ASSEMBLY, AS WELL AS STORAGE COMPARTMENT OR MONUMENT FOR INSTALLATION IN AN AIRCRAFT OR SPACECRAFT CABIN
SCHARNIERANORDNUNG SOWIE STAUFACH ODER MONUMENT ZUR INSTALLATION IN EINER FLUGZEUG- ODER RAUMFAHRZEUGKABINE
ENSEMBLE CHARNIÈRE, AINSI QUE COMPARTIMENT DE STOCKAGE OU MONUMENT POUR INSTALLATION DANS UNE CABINE D'AÉRONEF OU D'ENGIN SPATIAL
WENG ALEXANDER (Autor:in) / HOGH ROBERT (Autor:in)
28.08.2024
Patent
Elektronische Ressource
Englisch
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