Method of maufacturing a leading edge structure for aircraft

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

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60 39093, 156245, 156289, 156292, 244134B, B64D 1504, B32B 3100

Patent

active

058074546

ABSTRACT:
A leading edge structure for an aircraft has an outer wall, an inner wall disposed within the outer wall and including a partition with, the outer wall, the inner wall and the partition jointly defining a hot-air chamber, and a plurality of flow-rectifying fins or disposed in the hot-air chamber and compartmentalizing the hot-air chamber into a plurality of hot-air passages. The outer wall and the flow-rectifying fins are made of a fiber-reinforced synthetic resin and joined to each other by curing. The inner wall and the partition comprise a single component which is made of a fiber-reinforced synthetic resin, and being bonded to the outer wall. Alternatively, the inner wall and the partition are separate from each other and are joined to each other.

REFERENCES:
patent: H648 (1989-07-01), Tran
patent: 4738416 (1988-04-01), Birbragher
patent: 5011098 (1991-04-01), McLaren et al.
patent: 5228643 (1993-07-01), Manda et al.
patent: 5288355 (1994-02-01), Leffel et al.
patent: 5356096 (1994-10-01), Rauckhorst, III et al.

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