Unitary seat support with integrated electronics

Details Unitary seat support with integrated electronics Unitary seat support with integrated electronics

B - Operations, Transporting

64

D

B64D 11/06 (2006.01) B60N 2/44 (2006.01) H05K 7/14 (2006.01) H05K 7/20 (2006.01)

Patent

CA 2156520

An aircraft seat frame (1) includes n plurality of upright seat supports (21, 21' 21") each formed in one piece of heat- conductive material. Heat-generating electronics (20, 20') are thermally coupled to one of the supports (21, 21', 21"). Such support (21, 21', 21") acts as a heat sink to conduct and dissipate heat away from the electronics (20, 20').

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