SU1471661A1 - Уплотнение радиального зазора турбомашины - Google Patents

Уплотнение радиального зазора турбомашины

Info

Publication number
SU1471661A1
SU1471661A1 SU4234097/06A SU4234097A SU1471661A1 SU 1471661 A1 SU1471661 A1 SU 1471661A1 SU 4234097/06 A SU4234097/06 A SU 4234097/06A SU 4234097 A SU4234097 A SU 4234097A SU 1471661 A1 SU1471661 A1 SU 1471661A1
Authority
SU
USSR - Soviet Union
Prior art keywords
ring
packing
turbomachine
radial clearance
vibrator
Prior art date
Application number
SU4234097/06A
Other languages
English (en)
Inventor
Е.Н. Иванов
Original Assignee
Московский авиационный институт им.Серго Орджоникидзе
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 Московский авиационный институт им.Серго Орджоникидзе filed Critical Московский авиационный институт им.Серго Орджоникидзе
Priority to SU4234097/06A priority Critical patent/SU1471661A1/ru
Application granted granted Critical
Publication of SU1471661A1 publication Critical patent/SU1471661A1/ru

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
    • F01D11/20—Actively adjusting tip-clearance
    • F01D11/22—Actively adjusting tip-clearance by mechanically actuating the stator or rotor components, e.g. moving shroud sections relative to the rotor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/04—Antivibration arrangements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/40—Transmission of power
    • F05D2260/407—Transmission of power through piezoelectric conversion
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/96—Preventing, counteracting or reducing vibration or noise
    • F05D2260/962—Preventing, counteracting or reducing vibration or noise by means of "anti-noise"
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/10—Purpose of the control system to cope with, or avoid, compressor flow instabilities
    • F05D2270/101—Compressor surge or stall
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/60—Control system actuates means
    • F05D2270/62—Electrical actuators

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

Изобретение позволяет повысить эффективность работы турбомашины. В корпусе 1 установлено кольцо 2. На обращенной к лопаткам 3 поверхности 4 кольца 2 выполнены кольцевые канавки 5. Уплотнение снабжено охватывающим кольцо 2 вибратором. Вибратор выполнен в виде пьезокерамического цилиндра 6 с нанесенными на его внутренней и наружной поверхностях электродами 7, 8 и закреплен по внутренней поверхности на кольце 2, а по торцам 9, 10 на корпусе 1. Уплотнение позволяет уменьшить концевые перетечки за счет радиальных колебаний цилиндра 6 и кольца 2, которые возникают при подаче напряжения на электроды 7 и 8. 2 ил.
SU4234097/06A 1987-04-22 1987-04-22 Уплотнение радиального зазора турбомашины SU1471661A1 (ru)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU4234097/06A SU1471661A1 (ru) 1987-04-22 1987-04-22 Уплотнение радиального зазора турбомашины

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU4234097/06A SU1471661A1 (ru) 1987-04-22 1987-04-22 Уплотнение радиального зазора турбомашины

Publications (1)

Publication Number Publication Date
SU1471661A1 true SU1471661A1 (ru) 1996-11-20

Family

ID=60534731

Family Applications (1)

Application Number Title Priority Date Filing Date
SU4234097/06A SU1471661A1 (ru) 1987-04-22 1987-04-22 Уплотнение радиального зазора турбомашины

Country Status (1)

Country Link
SU (1) SU1471661A1 (ru)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2537100C2 (ru) * 2009-09-08 2014-12-27 Снекма Регулирование зазоров на вершине лопаток турбомашины
RU2710458C2 (ru) * 2014-10-10 2019-12-26 Сафран Аэро Бустерс Са Внешний корпус компрессора осевой турбомашины с уплотнением

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2537100C2 (ru) * 2009-09-08 2014-12-27 Снекма Регулирование зазоров на вершине лопаток турбомашины
RU2710458C2 (ru) * 2014-10-10 2019-12-26 Сафран Аэро Бустерс Са Внешний корпус компрессора осевой турбомашины с уплотнением
EP3006679B1 (fr) * 2014-10-10 2023-09-06 Safran Aero Boosters SA Carter externe de turbomachine axiale et procédé de commande d'un dispositif d'étanchéité de carter externe de turbomachine axiale

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