SU1228559A1 - Gas-turbine moving blade - Google Patents

Gas-turbine moving blade

Info

Publication number
SU1228559A1
SU1228559A1 SU3354999/06A SU3354999A SU1228559A1 SU 1228559 A1 SU1228559 A1 SU 1228559A1 SU 3354999/06 A SU3354999/06 A SU 3354999/06A SU 3354999 A SU3354999 A SU 3354999A SU 1228559 A1 SU1228559 A1 SU 1228559A1
Authority
SU
USSR - Soviet Union
Prior art keywords
moving blade
cavity
interrib
gas
feather
Prior art date
Application number
SU3354999/06A
Other languages
Russian (ru)
Inventor
Г.П. Нагога
М.В. Рукин
К.С. Нетесов
Original Assignee
Г.П. Нагога
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 Г.П. Нагога filed Critical Г.П. Нагога
Priority to SU3354999/06A priority Critical patent/SU1228559A1/en
Application granted granted Critical
Publication of SU1228559A1 publication Critical patent/SU1228559A1/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/18Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/187Convection cooling

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

FIELD: gas turbines. SUBSTANCE: moving blade has feather with upper cavity and front and rear cavities separated by longitudinal partitions; side walls of the latter have parallel ribs inclined to feather axis on back and trough sides in opposite directions contacting through their ends at intersection points and forming interrib channels communicating with upper cavity; novelty is that part of interrib channels of front cavity near longitudinal partition communicates directly with rear cavity. EFFECT: improved economic efficiency of cooling.
SU3354999/06A 1981-11-13 1981-11-13 Gas-turbine moving blade SU1228559A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU3354999/06A SU1228559A1 (en) 1981-11-13 1981-11-13 Gas-turbine moving blade

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU3354999/06A SU1228559A1 (en) 1981-11-13 1981-11-13 Gas-turbine moving blade

Publications (1)

Publication Number Publication Date
SU1228559A1 true SU1228559A1 (en) 1996-10-10

Family

ID=60539509

Family Applications (1)

Application Number Title Priority Date Filing Date
SU3354999/06A SU1228559A1 (en) 1981-11-13 1981-11-13 Gas-turbine moving blade

Country Status (1)

Country Link
SU (1) SU1228559A1 (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6382907B1 (en) 1998-05-25 2002-05-07 Abb Ab Component for a gas turbine
US7674092B2 (en) 2004-02-27 2010-03-09 Siemens Aktiengesellschaft Blade or vane for a turbomachine
EP2378073A1 (en) * 2010-04-14 2011-10-19 Siemens Aktiengesellschaft Blade or vane for a turbomachine
RU2554397C2 (en) * 2009-12-31 2015-06-27 Снекма Blade with inner ventilation
RU2559102C2 (en) * 2012-07-02 2015-08-10 Альстом Текнолоджи Лтд Cooled blade for gas turbine

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6382907B1 (en) 1998-05-25 2002-05-07 Abb Ab Component for a gas turbine
US7674092B2 (en) 2004-02-27 2010-03-09 Siemens Aktiengesellschaft Blade or vane for a turbomachine
RU2554397C2 (en) * 2009-12-31 2015-06-27 Снекма Blade with inner ventilation
EP2378073A1 (en) * 2010-04-14 2011-10-19 Siemens Aktiengesellschaft Blade or vane for a turbomachine
WO2011128404A1 (en) * 2010-04-14 2011-10-20 Siemens Aktiengesellschaft Blade or vane for a turbomachine
RU2573087C2 (en) * 2010-04-14 2016-01-20 Сименс Акциенгезелльшафт Blade, particularly, turbomachine blade
RU2559102C2 (en) * 2012-07-02 2015-08-10 Альстом Текнолоджи Лтд Cooled blade for gas turbine

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