SU422296A1 - TWO-CONTROL GAS TURBINE ENGINE - Google Patents

TWO-CONTROL GAS TURBINE ENGINE

Info

Publication number
SU422296A1
SU422296A1 SU1685147/06A SU1685147A SU422296A1 SU 422296 A1 SU422296 A1 SU 422296A1 SU 1685147/06 A SU1685147/06 A SU 1685147/06A SU 1685147 A SU1685147 A SU 1685147A SU 422296 A1 SU422296 A1 SU 422296A1
Authority
SU
USSR - Soviet Union
Prior art keywords
gas turbine
circuit
turbine engine
control gas
heat exchanger
Prior art date
Application number
SU1685147/06A
Other languages
Russian (ru)
Inventor
А.А. Михайлов
Г.М. Горелов
А.Е. Трянов
А.М. Керенский
В.А. Чистяков
А.А. Чулошников
A.A. Mikhajlov
G.M. Gorelov
A.E. Trjanov
A.M. Kerenskij
V.A. Chistjakov
A.A. Chuloshnikov
Original Assignee
А.А. Михайлов
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 А.А. Михайлов filed Critical А.А. Михайлов
Priority to SU1685147/06A priority Critical patent/SU422296A1/en
Application granted granted Critical
Publication of SU422296A1 publication Critical patent/SU422296A1/en

Links

Landscapes

  • Turbine Rotor Nozzle Sealing (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)

Abstract

Двухконтурный газотурбинный двигатель, содержащий расположенный во втором контуре теплообменник, входное устройство тракта охлаждаемой среды которого подключено к внутреннему газотурбинному контуру, а выходное - к распределительной полости системы охлаждения турбины, отличающийся тем, что, с целью повышения эффективности охлаждения элементов турбины, теплообменник выполнен в виде равномерно установленных по окружности радиальных секций, образованных расположенными одна над другой U-образными трубами, а входное и выходное устройства - в виде полых радиальных пилонов, из которых входной соединен с каналом вторичного воздуха камеры сгорания.A dual-circuit gas turbine engine containing a heat exchanger located in the second circuit, the input device of the cooled medium path is connected to the internal gas turbine circuit, and the output is connected to the distribution cavity of the turbine cooling system, characterized in that the heat exchanger radial sections of uniformly circumferential sections formed by U-tubes arranged one above the other, and the input and output devices and - in the form of hollow radial pylons, of which the inlet is connected to the channel of the secondary air of the combustion chamber.

SU1685147/06A 1971-07-30 1971-07-30 TWO-CONTROL GAS TURBINE ENGINE SU422296A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU1685147/06A SU422296A1 (en) 1971-07-30 1971-07-30 TWO-CONTROL GAS TURBINE ENGINE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU1685147/06A SU422296A1 (en) 1971-07-30 1971-07-30 TWO-CONTROL GAS TURBINE ENGINE

Publications (1)

Publication Number Publication Date
SU422296A1 true SU422296A1 (en) 2005-11-27

Family

ID=60520479

Family Applications (1)

Application Number Title Priority Date Filing Date
SU1685147/06A SU422296A1 (en) 1971-07-30 1971-07-30 TWO-CONTROL GAS TURBINE ENGINE

Country Status (1)

Country Link
SU (1) SU422296A1 (en)

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