Metal matrix composite structural panel construction

Details Metal matrix composite structural panel construction Metal matrix composite structural panel construction

1981-06-30

1983-10-25

Hunt, Brooks H.

Metal fusion bonding

Process

Plural joints

52806, 52808, 228157, 228212, 244119, 244123, 428593, B23K 104, B32B 312

Patent

active

044113803

ABSTRACT:
Lightweight capped honeycomb stiffeners 18 for use in fabricating metal or metal/matrix exterior structural panels 14 on aerospace type vehicles 10 and the process for fabricating same are disclosed. The stiffener stringers are formed in sheets (FIG. 6), cut to the desired width and length and brazed in spaced relationship to a skin 16 (FIG. 2) with the honeycomb material serving directly as the required lightweight stiffeners and not requiring separate metal encasement for the exposed honeycomb cells.

REFERENCES:
patent: 3020946 (1962-02-01), Kirk et al.
patent: 3084770 (1963-04-01), Wirsing, Jr.
patent: 3388522 (1968-06-01), Lowes
patent: 3401025 (1968-09-01), Whitney
NASA TP-1573.
NASA TP-1269.

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