RU2007139537A - Flying apparatus "Flying Saucer" - Google Patents

Flying apparatus "Flying Saucer" Download PDF

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Publication number
RU2007139537A
RU2007139537A RU2007139537/11A RU2007139537A RU2007139537A RU 2007139537 A RU2007139537 A RU 2007139537A RU 2007139537/11 A RU2007139537/11 A RU 2007139537/11A RU 2007139537 A RU2007139537 A RU 2007139537A RU 2007139537 A RU2007139537 A RU 2007139537A
Authority
RU
Russia
Prior art keywords
flying
aircraft
gas turbine
turbine engine
saucer
Prior art date
Application number
RU2007139537/11A
Other languages
Russian (ru)
Inventor
Николай Борисович Болотин (RU)
Николай Борисович Болотин
Original Assignee
Николай Борисович Болотин (RU)
Николай Борисович Болотин
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Николай Борисович Болотин (RU), Николай Борисович Болотин filed Critical Николай Борисович Болотин (RU)
Priority to RU2007139537/11A priority Critical patent/RU2007139537A/en
Publication of RU2007139537A publication Critical patent/RU2007139537A/en

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  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

Летательный аппарат, содержащий корпус осесимметричной формы, нижняя часть которого выполнена с возможностью вращения вокруг вертикальной оси, топливный бак и приборный отсек, газотурбинный двигатель, содержащий, в свою очередь, компрессор, камеру сгорания, турбину и реактивное сопло, отличающийся тем, что газотурбинный двигатель выполнен биротативным, при этом его статор соединен с нижней частью корпуса летательного аппарата.An aircraft comprising an axisymmetric housing, the lower part of which is rotatable about a vertical axis, a fuel tank and an instrument compartment, a gas turbine engine, which in turn contains a compressor, a combustion chamber, a turbine and a jet nozzle, characterized in that the gas turbine engine made birotative, while its stator is connected to the lower part of the hull of the aircraft.

Claims (1)

Летательный аппарат, содержащий корпус осесимметричной формы, нижняя часть которого выполнена с возможностью вращения вокруг вертикальной оси, топливный бак и приборный отсек, газотурбинный двигатель, содержащий, в свою очередь, компрессор, камеру сгорания, турбину и реактивное сопло, отличающийся тем, что газотурбинный двигатель выполнен биротативным, при этом его статор соединен с нижней частью корпуса летательного аппарата.An aircraft comprising an axisymmetric housing, the lower part of which is rotatable about a vertical axis, a fuel tank and an instrument compartment, a gas turbine engine, which in turn contains a compressor, a combustion chamber, a turbine and a jet nozzle, characterized in that the gas turbine engine made birotative, while its stator is connected to the lower part of the hull of the aircraft.
RU2007139537/11A 2007-10-24 2007-10-24 Flying apparatus "Flying Saucer" RU2007139537A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2007139537/11A RU2007139537A (en) 2007-10-24 2007-10-24 Flying apparatus "Flying Saucer"

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2007139537/11A RU2007139537A (en) 2007-10-24 2007-10-24 Flying apparatus "Flying Saucer"

Publications (1)

Publication Number Publication Date
RU2007139537A true RU2007139537A (en) 2009-04-27

Family

ID=41018641

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2007139537/11A RU2007139537A (en) 2007-10-24 2007-10-24 Flying apparatus "Flying Saucer"

Country Status (1)

Country Link
RU (1) RU2007139537A (en)

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Legal Events

Date Code Title Description
FA92 Acknowledgement of application withdrawn (lack of supplementary materials submitted)

Effective date: 20090616