Aircraft Component Assembly System
1 Assignment
0 Petitions
Accused Products
Abstract
An aircraft component assembly system (10; 10′; 10″) for the assembly of an interior component, a pipe and/or an electric line in an aircraft comprises at least one arc-shaped frame element (12; 12′; 12″), a connection element (32) that extends between a first and a second end of the frame element (12; 12′; 12″), a fastening apparatus for fastening the interior component, the pipe and/or the electric line to the frame element (12; 12′; 12″) and/or the connection element (32), and a first guide device (46) that is provided on the frame element (12; 12′; 12″) and/or the connection element (32) and is devised to interact with a second guide device (52), which is complementary to the first guide device (46) and provided on an aircraft structure (40), in such a way that the aircraft component assembly system (10; 10; 10″) is connectable to the aircraft structure (40) in a manner displaceable relative to the aircraft structure (40).
42 Citations
30 Claims
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1-15. -15. (canceled)
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16. Aircraft component assembly system for use in the assembly of an interior component, a pipe and/or an electric line in an aircraft, comprising:
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at least one arc-shaped frame element, which comprises a plurality of longitudinal struts that are disposed at least in sections substantially parallel to one another, a connection element that extends between a first and a second end of the frame element and is devised, in the assembled state of the aircraft component assembly system in an aircraft, to form an element of a floor of a cabin of the aircraft, a fastening apparatus for fastening the interior component, the pipe and/or the electric line to the frame element and/or the connection element, and a first guide device that is provided on the frame element and/or the connection element and is devised to interact with a second guide device, which is complementary to the first guide device and provided on an aircraft structure, in such a way that the aircraft component assembly system is connectable to the aircraft structure in a manner displaceable relative to the aircraft structure. - View Dependent Claims (17, 18, 19, 20, 21, 22, 23, 24, 25, 26, 27, 28, 29, 30)
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Specification