Force infeed element for laminar panel assembly

Details Force infeed element for laminar panel assembly Force infeed element for laminar panel assembly

1979-09-17

1981-06-16

Epstein, Henry F.

Stock material or miscellaneous articles

Structurally defined web or sheet

Honeycomb-like

52787, 136292, B32B 312

Patent

active

042738180

ABSTRACT:
A laminar panel assembly which is particularly useful in space vehicles for contact with solar cells includes a first and a second cover layer, a supporting core structure interposed between the cover layers and at least one force infeed element disposed within the core structure between the cover layers. The force infeed element includes at least one solid central piece for punctiform load infeed, and shear webs extending from the central piece radially outwardly in a branched formation such that the number of shear webs increases with increasing radial distance from the central piece.

REFERENCES:
patent: 2952579 (1960-09-01), Merriman
patent: 3137887 (1964-06-01), Mannino et al.
patent: 3138506 (1964-06-01), Ross
patent: 3166149 (1965-01-01), Hulse et al.
patent: 3170471 (1965-02-01), Schnitzer
patent: 3256649 (1966-06-01), Webb
patent: 3282533 (1966-11-01), Spain
patent: 3341050 (1967-09-01), Forman et al.
patent: 3890749 (1975-06-01), Gunther
patent: 4014147 (1977-03-01), Wesch

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