METHOD AND DEVICE FOR TANGENTIAL SHIFTING INNER COOLING AT FIXED BLADE OF NOZZLE Russian patent published in 2014 - IPC F01D5/18 

Abstract RU 2518775 C2

FIELD: machine building.

SUBSTANCE: turbine unit consists of the first device (200) of fixed blades, the second device (210) of fixed blades and a deflector (100) formed from a plate-type element. The deflector comprises the first section (101) of a hole with the first hole shape and the second section (102) of a hole with the second hole shape. The first hole section (101) comprises a configuration of inlet holes (104) forming the first hole shape. The second hole section (102) comprises an additional configuration of inlet holes (104) forming the second hole shape. The deflector (100) is spatially mounted on the first device (200) of fixed blades and on the second device (210) of fixed blades so that cooling fluid medium (106) can flow through the inlet holes (104) of the first hole section (101) to the first device (200) of fixed blades and the cooling fluid medium (106) can flow through the inlet holes (104) of the second hole section (102) to the second device (210) of fixed blades. The first shape of the hole differs from the second shape of the hole to reach the specified first flow of the cooling fluid medium (106) mass to the first device (200) of fixed blades and the specified second flow of the cooling fluid medium (106) mass to the second device (210) of fixed blades at the specified installation positions of the first device (200) of fixed blades and the second device (210) of fixed blades.

EFFECT: provision for proper cooling system of a turbine.

13 cl, 4 dwg

Similar patents RU2518775C2

Title Year Author Number
GUIDE VANES DEVICE FOR TURBINE AND METHOD OF ITS MANUFACTURING 2011
  • Dzhounz Richard
  • Pejsi Endi
RU2576600C2
INTEGRATED SUPPLY IN PROCESS AT DRILLING SITE 2015
  • Lukharuka Radzhesh
  • Fam Khau Ngujen-Pkhuk
  • Khyui Uillyam
  • Morrison Nikki
  • Shen Kristofer
  • Ramesh Avinash
  • Bindiganavale Garud
  • Kokijo Loran Iv Klod
RU2692297C2
CIRCULAR FIXED ELEMENT FOR USE WITH STEAM TURBINE AND STEAM TURBINE 2009
  • Bauehn Mark Kevin
  • Suon Stefan Rodzher
  • Montgomeri Majkl Ehrl
RU2511914C2
SYSTEM OF FLOW CONTROL, GENERATING SYSTEM AND METHOD FOR TURBINE ENGINE RECOVERY IN SUCH SYSTEM 2013
  • Dutta Sandip
  • Maldonado Jaime Javier
RU2618133C2
COOLED DESIGN OF A BLADE OR BLADES OF A GAS TURBINE AND METHOD OF ITS ASSEMBLY 2018
  • Mugglestone, Jonathan
RU2740048C1
GAS TURBINE SYSTEM, WHICH REDUCES STRESS 2012
  • Blak Richard
  • Khyuz Martin
RU2626913C2
TRANSITION DUCT OF GAS TURBINE ENGINE AND METHOD OF ITS MANUFACTURING, AND ALSO GAS TURBINE ENGINE 2010
  • Khedlehnd Pol
  • Ternbull Majkl
RU2531094C2
SYSTEM AND METHOD OF WORK FLUID EXTRACTION FROM INTERNAL VOLUME OF TURBINE MACHINE, AND TURBINE MACHINE WITH SUCH SYSTEM 2012
  • Tvell Filip
RU2567524C2
TURBINE SYSTEM AND METHOD FOR ADJUSTING GAPS IN THE TURBINE 2013
  • Chillar Rakhul Dzh.
  • Ansari Adil
  • Pena Ezio
  • Antuan Nikolya
  • Vignolo Zhan-Lui
RU2648196C2
REDUCTION METHOD OF THE TORSIONAL VIBRATION IN THE BOREHOLE AND CORRESPONDING DEVICE 2013
  • Gadzhdzhi Bkhargav
  • Gaikvad Rakhul Ramchandra
  • Agarval Puneet
RU2625682C1

RU 2 518 775 C2

Authors

Batler Dehvid

Dates

2014-06-10Published

2009-09-04Filed