Fusion bonded thermoplastic leading edge for aircraft aerodynami

Adhesive bonding and miscellaneous chemical manufacture – Methods – Surface bonding and/or assembly therefor

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156212, 156242, 156245, 156297, 156298, 1563798, 264241, 264247, 264248, 264251, 264258, 264259, 264263, 2642711, 264277, 264DIG64, B29C 6900, B32B 3104, B32B 3120

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053623479

ABSTRACT:
An aircraft wing, a fusion bonded thermoplastic fixed leading edge structure for aircraft aerodynamic surfaces and a method of manufacture are provided. The fixed leading edge structure comprises a leading edge skin (28), one or more aerodynamic profile defining stiffening members (17, 18) spaced spanwise therewithin and a sub-spar. Each of the components are of low modulus consolidated composite material and the leading edge skin (28) is attached to the stiffening members (17, 18) and to the sub-spar by a fusion-bonding thermoplastic process.

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Navy Technical Disclosure Bulletin, vol. 9, No. 2, Dec. 1983, Arlington US pp. 93-98, W. J. Wallace `Composite Air Foil, Navy Tech. Cat. No. 0164, Navy Case No. 66779`.

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