AIRCRAFT Russian patent published in 2019 - IPC B64C1/06 B64C30/00 B64D41/00 H01L35/02 

FIELD: aircrafts.

SUBSTANCE: invention relates to aircrafts. Aircraft contains fuselage; thermal collector is rigidly fixed on the inner surface of the fuselage. External current collector is located on the inner surface of the thermal collector, which is a system of alternating electrically conductive and electrically insulating sections. Two prisms of n- or p-type thermoelectric material are fixed on each electrically conductive area with the help of a hot-commutative commutating solder, and their other bases are bonded to the external surface of the internal current collector, which is a system of alternating electrically conductive and electrically insulating sections, using a cold-junction switching solder. Areas of external and internal current collectors are oriented the way there is an insulating portion of the internal current collector located opposite the electrically conductive portion of the external current collector. Two extreme conductive section of the internal current collector is equipped with terminals. Between the internal current collector and the cooling manifold, equipped with cooling fins, fixed electrical insulating layer.

EFFECT: technical result is to reduce the consumption of fuel consumed.

1 cl, 3 dwg