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2 099 248

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IPC

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Application

95121375/28, 1995-12-19

(22)

Actual filing date

1995-12-19

(45)

Published

1997-12-20

(72)

Inventor

Shengardt A.S.Pukhov A.A.Avtomanov A.I.Malyshev V.V.Solozobov V.I.Gal'Perin S.B.

(73)

Holder

Aktsionernoe Obshchestvo Nauchno-Tekhnicheskij Kompleks Im.A.N.Tupoleva"

AIRCRAFT Russian patent published in 1997 - IPC

Abstract RU 2099248 C1

FIELD: aeronautical engineering; flying vehicles using standard fuel - kerosene and cryogenic propellant. SUBSTANCE: aircraft includes fuselage, main and canard wings connected by means of nacelles located on either side of fuselage, as well as engines and cryogenic propellant tanks located in nacelles. Kerosene tanks are located in wings. Spans of wings are related by relationship of 1.5-3; ratio of distance between leading edges of wings and chord of main wing ranges from 1.5 to 3. Wings are mounted at equal angles of attack and have chords of similar length. EFFECT: enhanced reliability. 3 cl, 2 dwg

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RU 2 099 248 C1

Authors

Shengardt A.S.

Pukhov A.A.

Avtomanov A.I.

Malyshev V.V.

Solozobov V.I.

Gal'Perin S.B.

Dates

1997-12-20—Published

1995-12-19—Filed

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