METHOD OF CONSTRUCTING COMPOSITE ASSEMBLIES

A composite assembly has an outer spar component (120) having an outer spar component inner profile (142), an inner spar component (166) having an inner spar component outer profile (168) substantially complementary to the outer spar component inner profile (142), and an adhesive disposed between the outer spar component (120) and the inner spar component (166).


» Number: EP3330063A1 (A1)

» Publication Date: 06/06/2018

» Applicant: BELL HELICOPTER TEXTRON INC?[US]

» Inventor: MEASOM RONALD J?[US]; RAINS MITCHELL ELVIN?[US]

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This project has received funding from the European Union's Horizon 2020 research and innovation programme under grant agreement Nº 768737


                   




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