Releasable fastening of a component in an aircraft
AssigneeAirbus Operations GmbH
InventorsHartwig Jaeger, Gerd Rohlfs
Life of this patent
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Abstract
A device for the releasable fastening of a component in an aircraft includes a component carrier with a base plane, wherein the component carrier comprises an installation state in which the base plane of the component carrier comprises an angle relative to the horizontal base plane of the aircraft, and wherein the component carrier is equipped to accommodate a component in a releasably affixed manner.
Claims18
A device for the releasable fastening of a component in an aircraft, the device comprising:
- a component carrier with a base plane;
- wherein the component carrier comprises an installed state in which the base plane of the component carrier comprises an angle relative to a horizontal base plane of the aircraft;
- and
- wherein the component carrier is equipped to accommodate a component in a releasably fastened manner,
- wherein the component carrier further comprises a second state, in which the base plane of the component carrier is arranged so as to be substantially parallel relative to the horizontal base plane of the aircraft;
- and
- wherein the component carrier is arranged so as to be displaceable between the installed state and the second state by a continuous tilt movement.
A system for the releasable fastening of a component in an aircraft, the system comprising:
- a device comprising a component carrier with a base plane;
- wherein the component carrier comprises an installed state in which the base plane of the component carrier comprises an angle relative to a horizontal base plane of the aircraft;
- and
- wherein the component carrier is equipped to accommodate a component in a releasably fastened manner;
- wherein the component carrier further comprises a second state, in which the base plane of the component carrier is arranged so as to be substantially parallel relative to the horizontal base plane of the aircraft;
- and
- wherein the component carrier is arranged so as to be displaceable between the installed state and the second state by a continuous tilt movement, and
- a component;
- wherein the component is placeable in the component carrier;
- wherein the component is affixable to the component carrier in a releasably fixed manner;
- and
- wherein the component carrier, with the placed component is displaceable between the installed state and the second state.
An aircraft comprising a device for the releasable fastening of a component in an aircraft, the device comprising:
- a component carrier with a base plane;
- wherein the component carrier comprises an installed state in which the base plane of the component carrier comprises an angle relative to a horizontal base plane of the aircraft;
- and
- wherein the component carrier is equipped to accommodate a component in a releasably fastened manner;
- wherein the component carrier further comprises a second state, in which the base plane of the component carrier is arranged so as to be substantially parallel relative to the horizontal base plane of the aircraft;
- and
- wherein the component carrier is arranged so as to be displaceable between the installed state and the second state by a continuous tilt movement.
A method for the releasable fastening of a component in an aircraft, comprising:
- inserting a component in a component carrier;
- fixing the component to the component carrier;
- and
- wherein the base plane of the component carrier in its installed state is arranged at an angle relative to a horizontal base plane of the aircraft, wherein the component carrier further comprises a second state, in which the base plane of the component carrier is arranged so as to be substantially parallel relative to the horizontal plane of the aircraft;
- and
- wherein the component carrier is arranged so as to be displaceable between the installed state and the second state by a continuous tilt movement.
Dependencies are inferred from the claim text.