BOUNDARY LAYER SHIELDING SYSTEM USING UPSTREAM PLASMA (VERSIONS), AND OPERATING METHOD OF SYSTEM Russian patent published in 2012 - IPC F01D5/18 

Abstract RU 2458227 C2

FIELD: machine building.

SUBSTANCE: boundary layer shielding system using upstream plasma includes film cooling holes formed through wall and plasma generator. Film cooling holes are located at an angle in the direction of outlet from cold surface of wall to external hot surface of wall. Plasma generator is upstream located relative to film cooling holes for formation of plasma passing above film cooling holes. Operating method of boundary layer shielding system using upstream plasma consists in the fact that energy is supplied to plasma generator to form the plasma passing in the direction of outlet above film cooling holes formed through the wall and along external hot surface of the wall.

EFFECT: providing the shielding effect of film cooling holes without physical intrusion to keep aerodynamic efficiency.

10 cl, 7 dwg

Similar patents RU2458227C2

Title Year Author Number
SYSTEM OF PLASMA SCREENING OF BOUNDARY LAYER DOWNSTREAM AND METHOD OF ITS OPERATION 2007
  • Li Chin-Pan
  • Vadija Aspi Rustom
  • Cherri Dehvid Glenn
  • Khan' Tsze-Chin
RU2455495C2
SYSTEM FOR REDUCTION OF SWIRLS ON REAR EDGE OF AERODYNAMIC SECTION OF GAS TURBINE ENGINE, AND ITS OPERATING METHOD 2007
  • Li Chin-Pan
  • Vadija Aspi Rustom
  • Cherri Dehvid Glenn
  • Khan' Tsze-Chin
RU2461716C2
REDUCTION SYSTEM OF VORTEX FORMATION ON END WALL (VERSIONS), AND SYSTEM OPERATING METHOD 2007
  • Li Chin-Pan
  • Vadija Aspi Rustom
  • Cherri Dehvid Glen
  • Khan' Tsze-Chin
RU2471996C2
SYSTEM FOR LIFTING BOUNDARY LAYER USING PLASMA FOR BLADE OF GAS-TURBINE ENGINE (VERSIONS), AND GAS-TURBINE ENGINE APPLICATION METHOD 2007
  • Li Chin-Pan
  • Vadija Aspi Rustom
  • Cherri Dehvid Glenn
  • Khan' Tsze-Chin
RU2466279C2
ENGINE WITH COMPOUND TURBINE COOLING 2007
  • Li Chin-Pan
  • Moniz Tomas Ori
  • Orlando Robert Dzhozef
RU2447302C2
GAS TURBINE ENGINE AND METHOD OF COOLING NOZZLE VANES 2007
  • Li Chin-Pan
  • Moniz Tomas Ori
  • Orlando Robert Dzhozef
RU2453710C2
GAS TURBINE ENGINE FAST EXPANSION PLASMA-ENRICHED TRANSITION DUCT 2007
  • Li Chin-Pan
  • Vadija Aspi Rustom
  • Cherri Dehvid Glenn
  • Karson Skott Majkl
RU2463459C2
TURBINE SYSTEM AND GAS TURBINE ENGINE 2011
  • Batt Stefen
  • Magglstoun Dzhonatan
RU2576754C2
METHOD AND SYSTEM OF AERO/HYDRODYNAMIC CONTROL OF NEWTONIAN FLUID FLOW IN RADIAL TURBOMACHINE 2013
  • Irlend Piter
  • Irlend Entoni
RU2642203C2
TURBINE BLADE 2014
  • Li Chin-Pan
RU2665092C2

RU 2 458 227 C2

Authors

Li Chin-Pan

Vadija Aspi Rustom

Cherri Dehvid Glenn

Khan' Tsze-Chin

Dates

2012-08-10Published

2007-11-29Filed