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(19)

(11)

2 495 788

(13)

(51)

IPC

B64C3/36(2006-01-01)

B64C1/38(2006-01-01)

B64G1/58(2006-01-01)

B64C23/00(2006-01-01)

(21) (22)

Application

2012100799/11, 2012-01-11

(24)

Start date

2012-01-11

(22)

Actual filing date

2012-01-11

(45)

Published

2013-10-20

(72)

Inventor

Kernozhitskij Vladimir AndreevichAtamasov Vladimir Dmitrievich

(73)

Holder

Federal'Noe Gosudarstvennoe Bjudzhetnoe Obrazovatel'Noe Uchrezhdenie Vysshego Professional'Nogo Obrazovanija Baltijskij Gosudarstvennyj Tekhnicheskij Universitet Im. D.F. Ustinova

HYPERSONIC AIRCRAFT WING IN AERODYNAMIC HEATING CONDITIONS Russian patent published in 2013 - IPC B64C3/36 B64C1/38 B64G1/58 B64C23/00

Abstract RU 2495788 C2

FIELD: transport.

SUBSTANCE: invention relates to aircraft and aerospace engineering, particularly, to hypersonic craft thermal protection. Hypersonic craft wing comprises heat emission layer 2 arranged at its surface connected via onboard electric power using circuit 7 with electrically conducting element 3. Electrically conducting element 3 is thermally connected via insulating layer 4 with channels 6 communicated with onboard thermal control system cooling line. Aforesaid heat emission layer 2 is arranged at wing outer surface nearby leading edge. Electric conductor 3 is arranged at insulating layer 6 nearby wing trailing edge.

EFFECT: reduced temperature of heating, higher reliability and lower drag.

2 cl, 1 dwg

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RU 2 495 788 C2

Authors

Kernozhitskij Vladimir Andreevich

Atamasov Vladimir Dmitrievich

Dates

2013-10-20—Published

2012-01-11—Filed