Method for integrating a backing-structure assembly in a structure of an aircraft or spacecraft
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United States of America Patent
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Nov 26, 2019
Grant Date -
Dec 14, 2017
app pub date -
Jun 5, 2017
filing date -
Jun 8, 2016
priority date (Note) -
In Force
status (Latency Note)
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Abstract
A method for integrating a backing-structure assembly in a structure of an aircraft or spacecraft is described. In this case, a plurality of individual elements is joined to form the backing-structure assembly. The individual elements for the backing-structure assembly and a skin portion for the structure are provided. The elements are arranged on a pre-assembly device which comprises retaining devices, which are each configured to hold one of the elements so as to be adjustable with respect to the position and/or location thereof. Some or all of the elements are connected to the skin portion. In the method, by adjusting the retaining devices for tolerance compensation, gaps between joint regions of the elements and the skin portion are eliminated or adjusted.
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International Classification(s)
- B29C:SHAPING OR JOINING OF PLASTICS; SHAPING OF SUBSTAN....
- B64F:GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS
- B29K:INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, ....
- B64C:AEROPLANES; HELICOPTERS
- B29L:INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RE....
- B32B:LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA....
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