Honeycomb core assembly including a sacrificial core portion

Details Honeycomb core assembly including a sacrificial core portion Honeycomb core assembly including a sacrificial core portion

1980-09-29

1982-08-24

Epstein, Henry F.

Stock material or miscellaneous articles

Structurally defined web or sheet

Honeycomb-like

156154, 156267, B32B 312

Patent

active

043461344

ABSTRACT:
A sandwich assembly, e.g. an aluminum honeycomb sandwich assembly such as an inboard slat trailing edge for use in an aircraft wherein the spar cap spacing accuracy is retained through break-away tooling, e.g. a strip of low density core machined to the leading edge contour of the honeycomb core during core manufacture.

REFERENCES:
patent: 3060561 (1962-10-01), Watter
patent: 3064345 (1962-11-01), Herman et al.
patent: 3407110 (1968-10-01), Axelson et al.
patent: 3413708 (1968-12-01), Norville et al.
patent: 3566493 (1971-03-01), Poucher et al.
patent: 3740301 (1973-06-01), Manning et al.
patent: 4284443 (1981-08-01), Hilton

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