HIGH AREA RATIO AUTOSUCTION INTERTURBINE DUCT ASSEMBLY FOR GAS TURBINE ENGINE (VERSIONS), SYSTEM AND METHOD OF OPTIMISING EFFICIENCY OF GAS TURBINE ENGINE INCORPORATING SUCHDUCT Russian patent published in 2008 - IPC F01D9/02 

Abstract RU 2331776 C2

FIELD: engines and pumps.

SUBSTANCE: interturbine duct assembly to be used in a gas turbine engine or the like unit includes a duct to receive the flow from the turbine with an inlet and outlet, inner and outer surfaces and to form a main fluid medium flow passage. An opening is provided on the duct outer surface. The aforesaid assembly comprises also a nozzle communicating with the duct and a channel with its inlet communicating with the said opening and outlet arranged in the nozzle. The said channel makes a fluid medium flow bypass passage between the duct and the nozzle. Various versions of the given invention propose certain means to increase the gas turbine engine efficiency by controlling the fluid medium flow in the said interturbine duct. The invention allows increasing the low-pressure turbine stage diameter relative to that of the high-pressure stage and/or decreasing the number of the low-pressure turbine nozzles as compared to known similar versions.

EFFECT: lower weight and higher efficiency of gas turbine engine.

48 cl, 3 dwg

Similar patents RU2331776C2

Title Year Author Number
PIPE ASSEMBLY FOR GAS TURBINE ENGINE, BYPASS PIPE AND GAS TURBINE ENGINE 2005
  • Gratsiozi Paolo
  • Kertli Kevin Richard
RU2379525C2
GAS TURBINE ENGINE FAST EXPANSION PLASMA-ENRICHED TRANSITION DUCT 2007
  • Li Chin-Pan
  • Vadija Aspi Rustom
  • Cherri Dehvid Glenn
  • Karson Skott Majkl
RU2463459C2
TAIL CONE FOR ROTARY GAS TURBINE ENGINE WITH MICRO-JETS 2012
  • Kont Per
  • Vjuillmen Aleksandr Alfred Gaston
  • Kenig Maksim
  • Dzhordan Piter
  • Zherve Iv
RU2605869C2
GAS TURBINE ENGINE (VARIANTS) 2017
  • Sheridan, William G.
  • Hasel, Karl L.
RU2676150C1
GAS TURBINE ENGINE (VERSIONS) AND METHOD FOR INCREASING GAS TURBINE ENGINE PERFORMANCE 2014
  • Sheridan Uilyam G.
  • Khejzel Karl L.
RU2635181C2
GAS TURBINE ENGINE AND METHOD OF COOLING NOZZLE VANES 2007
  • Li Chin-Pan
  • Moniz Tomas Ori
  • Orlando Robert Dzhozef
RU2453710C2
TURBOFAN GAS TURBINE ENGINE WITH ADJUSTABLE FAN OUTLET GUIDE VANES (VERSIONS) 2006
  • Vud Piter Dzhon
  • Zenon Rubi Lasandra
  • Lachapelle Donald Dzhordzh
  • Milke Mark Dzhozef
  • Grant Karl
RU2435057C2
METHOD OF GAS TURBINE ENGINE COOLING (VERSIONS), METHOD OF CONTROLLING GAS TURBINE ENGINE, GAS TURBINE ENGINE AND ITS ROTOR 2005
  • Tompson Ml. Robert S.
  • Uil'Jams Greg
RU2477379C2
GAS TURBINE ENGINE 2013
  • Batt Stefen
  • Blak Richard
  • Batler Devid
RU2616743C2
GAS TURBINE ENGINE (VERSIONS) 2012
  • Marshall, Richard M.
RU2527815C2

RU 2 331 776 C2

Authors

Kertli Kevin

Gratsiozi Paolo

Dates

2008-08-20Published

2003-10-23Filed