RU2006126941A - GAS TURBINE ENGINE - Google Patents

GAS TURBINE ENGINE Download PDF

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Publication number
RU2006126941A
RU2006126941A RU2006126941/06A RU2006126941A RU2006126941A RU 2006126941 A RU2006126941 A RU 2006126941A RU 2006126941/06 A RU2006126941/06 A RU 2006126941/06A RU 2006126941 A RU2006126941 A RU 2006126941A RU 2006126941 A RU2006126941 A RU 2006126941A
Authority
RU
Russia
Prior art keywords
turbine engine
gas turbine
turbine
compressor
electric
Prior art date
Application number
RU2006126941/06A
Other languages
Russian (ru)
Other versions
RU2325539C2 (en
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 RU2006126941/06A priority Critical patent/RU2325539C2/en
Publication of RU2006126941A publication Critical patent/RU2006126941A/en
Application granted granted Critical
Publication of RU2325539C2 publication Critical patent/RU2325539C2/en

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  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Motor Or Generator Cooling System (AREA)

Claims (4)

1. Газотурбинный двигатель, содержащий турбокомпрессор с компрессором, камерой сгорания, выход из которой соединен газовым трактом с турбиной, и не менее двух электрических машин, встроенных в турбокомпрессор, отличающий тем, что в компрессор встроен электродвигатель, а в турбину - электрогенератор, причем турбина выполнена свободной, электрогенератор соединен с электродвигателем посредством силового кабеля.1. A gas turbine engine comprising a turbocompressor with a compressor, a combustion chamber, the outlet of which is connected by a gas path to the turbine, and at least two electric machines built into the turbocompressor, characterized in that the electric motor is integrated in the compressor and the generator is in the turbine, moreover, the turbine made free, the electric generator is connected to the electric motor by means of a power cable. 2. Газотурбинный двигатель по п.1, отличающийся тем, что обмотки электродвигателя выполнены на статоре компрессора, а система постоянных магнитов компрессора закреплена на роторе турбины.2. The gas turbine engine according to claim 1, characterized in that the motor windings are made on the compressor stator, and the compressor permanent magnet system is mounted on the turbine rotor. 3. Газотурбинный двигатель по п.1, отличающийся тем, обмотки электрогенератора установлены на статоре турбины, а система постоянных магнитов электрогенератора закреплена на роторе турбины.3. The gas turbine engine according to claim 1, characterized in that the windings of the electric generator are installed on the turbine stator, and the system of permanent magnets of the electric generator is mounted on the turbine rotor. 4. Газотурбинный двигатель по п.1, или 2, или 3, отличающийся тем, что обмотки электродвигателя и электрогенератора заключены в кожуха, к которым подведена система воздушного охлаждения.4. The gas turbine engine according to claim 1, or 2, or 3, characterized in that the windings of the electric motor and electric generator are enclosed in a casing to which an air cooling system is connected.
RU2006126941/06A 2006-07-24 2006-07-24 Gas turbine engine RU2325539C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2006126941/06A RU2325539C2 (en) 2006-07-24 2006-07-24 Gas turbine engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2006126941/06A RU2325539C2 (en) 2006-07-24 2006-07-24 Gas turbine engine

Publications (2)

Publication Number Publication Date
RU2006126941A true RU2006126941A (en) 2008-01-27
RU2325539C2 RU2325539C2 (en) 2008-05-27

Family

ID=39109794

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2006126941/06A RU2325539C2 (en) 2006-07-24 2006-07-24 Gas turbine engine

Country Status (1)

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RU (1) RU2325539C2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20130231893A1 (en) * 2012-03-01 2013-09-05 General Electric Company Apparatus and related monitoring system

Also Published As

Publication number Publication date
RU2325539C2 (en) 2008-05-27

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