Patenton — panteon of patents

(19)

RU

(11)

2 184 876

(13)

C1

(51)

IPC

(21) (22)

Application

2001101854/06, 2001-01-19

(24)

Start date

2001-01-19

(22)

Actual filing date

2001-01-19

(45)

Published

2002-07-10

(72)

Inventor

Magafurov Sh.M.Bikbulatov A.M.Kultygin A.A.Shajkhutdinov D.Kh.

(73)

Holder

Ufimskij Gosudarstvennyj Aviatsionnyj Tekhnicheskij Universitet

EXHAUST PLANT Russian patent published in 2002 - IPC

Abstract RU 2184876 C1

FIELD: power engineering. SUBSTANCE: invention relates to turbocompressor sets to provide vacuum of higher degree by means of two-stage controllable supersonic back-up gas ejector at compressor inlet. Proposed exhaust plant has compressor installed on one shaft with free power turbine provided with inlet and outlet, and drive made in form of aircraft gas turbine engine whose outlet is connected with inlet of free power turbine. EFFECT: provision of vacuum of higher level owing to installation of two-stage controllable supersonic back-up gas ejector at compressor. 1 dwg

Similar patents RU2184876C1

Title Year Author Number
TURBINE COMPRESSOR PLANT 1998
  • Magafurov Sh.M.
  • Bikbulatov A.M.
  • Kultygin A.A.
 RU2147084C1
METHOD OF OPERATION AND DESIGN OF COMBINATION GAS TURBINE PLANT OF GAS DISTRIBUTING SYSTEM 2000
  • Bakirov F.G.
  • Poleshchuk I.Z.
  • Salikhov A.A.
 RU2199020C2
DEVICE AND METHOD (VERSIONS) TO STABILISE FLAME IN TURBOJET ENGINE AFTERBURNER CHAMBER 2009
  • Kishalov Aleksandr Evgen'Evich
 RU2403422C1
METHOD OF OPERATION OF INTERNAL COMBUSTION ENGINE AND POWER PLANT FOR IMPLEMETING THE METHOD 2001
  • Enikeev R.D.
  • Khamitova A.F.
 RU2209322C2
POWER PLANT AUTOMATIC CONTROL SYSTEM 2001
  • Il'Jasov B.G.
  • Denisova E.V.
  • Denisov V.V.
  • Klimenko D.V.
 RU2204044C2
DEVICE MEASURING TEMPERATURE OF GAS-OF GAS-TURBINE ENGINE 1990
  • Urazbakhtina L.B.
  • Sigacheva T.N.
  • Opshin Eh.G.
 RU2066854C1
POWER DRIVE BASED ON OF AIRCRAFT GAS TURBINE PLANT (AGTP) 2019
  • Sejfi Aleksandr Fatykhovich
  • Limanskij Adolf Stepanovich
 RU2727213C1
METHOD AND DEVICE TO DETERMINE CHARACTERISTICS AND BORDER OF STABLE COMPRESSOR OPERATION WITHIN GAS TURBINE ENGINE 2011
  • Krivosheev Igor' Aleksandrovich
  • Akhmedzjanov Dmitrij Al'Bertovich
  • Kishalov Aleksandr Evgen'Evich
 RU2488086C2
METHOD AND DEVICE FOR STARTING GAS-TURBINE POWER PLANT AND FEEDING IT WITH GAS 1999
  • Shelud'Ko L.P.
  • Denisov I.N.
  • Krasheninnikov A.V.
 RU2182247C2
TURBO-JET ENGINE AND CONTROL METHOD THEREOF 2016
  • Pismennyj Vladimir Leonidovich
 RU2645373C1

RU 2 184 876 C1

Authors

Magafurov Sh.M.

Bikbulatov A.M.

Kultygin A.A.

Shajkhutdinov D.Kh.

Dates

2002-07-10—Published

2001-01-19—Filed

read Similar patents