IT8224934A0 - AIR SEAL GASKET FOR STATOR OF A COMPRESSOR. - Google Patents

AIR SEAL GASKET FOR STATOR OF A COMPRESSOR.

Info

Publication number
IT8224934A0
IT8224934A0 IT8224934A IT2493482A IT8224934A0 IT 8224934 A0 IT8224934 A0 IT 8224934A0 IT 8224934 A IT8224934 A IT 8224934A IT 2493482 A IT2493482 A IT 2493482A IT 8224934 A0 IT8224934 A0 IT 8224934A0
Authority
IT
Italy
Prior art keywords
stator
compressor
air seal
seal gasket
gasket
Prior art date
Application number
IT8224934A
Other languages
Italian (it)
Other versions
IT1195967B (en
Inventor
Bruce Joel Johnson
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of IT8224934A0 publication Critical patent/IT8224934A0/en
Application granted granted Critical
Publication of IT1195967B publication Critical patent/IT1195967B/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/08—Sealings
    • F04D29/16—Sealings between pressure and suction sides
    • F04D29/161—Sealings between pressure and suction sides especially adapted for elastic fluid pumps
    • F04D29/164—Sealings between pressure and suction sides especially adapted for elastic fluid pumps of an axial flow wheel
    • 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
    • F01D11/001—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between stator blade and rotor

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Sealing Devices (AREA)
IT24934/82A 1981-12-28 1982-12-23 AIR SEAL GASKET FOR STATOR OF A COMPRESSOR IT1195967B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US33460781A 1981-12-28 1981-12-28

Publications (2)

Publication Number Publication Date
IT8224934A0 true IT8224934A0 (en) 1982-12-23
IT1195967B IT1195967B (en) 1988-11-03

Family

ID=23307975

Family Applications (1)

Application Number Title Priority Date Filing Date
IT24934/82A IT1195967B (en) 1981-12-28 1982-12-23 AIR SEAL GASKET FOR STATOR OF A COMPRESSOR

Country Status (6)

Country Link
JP (1) JPS58119996A (en)
DE (1) DE3244874A1 (en)
FR (1) FR2519096B1 (en)
GB (1) GB2112878B (en)
IT (1) IT1195967B (en)
SE (1) SE458295B (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2553822B1 (en) * 1983-10-24 1987-12-31 Snecma DEVICE FOR FIXING BLADES OF TURBINE DISTRIBUTOR
US6533285B2 (en) * 2001-02-05 2003-03-18 Caterpillar Inc Abradable coating and method of production
US7604455B2 (en) 2006-08-15 2009-10-20 Siemens Energy, Inc. Rotor disc assembly with abrasive insert
DE102010055435B4 (en) 2010-12-21 2018-03-29 Rolls-Royce Deutschland Ltd & Co Kg Innendeckband a gas turbine and method for producing a Innenendeckbandes
DE102013212465B4 (en) * 2013-06-27 2015-03-12 MTU Aero Engines AG Sealing arrangement for a turbomachine, a vane assembly and a turbomachine with such a sealing arrangement

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR998220A (en) * 1949-10-26 1952-01-16 Soc D Const Et D Equipements M Advanced training in the assembly and fixing of fixed blades for turbomachines
GB791568A (en) * 1956-03-26 1958-03-05 Gen Motors Corp Improvements in axial flow compressors
GB780137A (en) * 1955-07-07 1957-07-31 Gen Motors Corp Improvements relating to axial-flow compressors
CH489699A (en) * 1968-03-22 1970-04-30 Sulzer Ag Guide vane ring for turbo machines
US3849023A (en) * 1973-06-28 1974-11-19 Gen Electric Stator assembly
FR2404102A1 (en) * 1977-09-27 1979-04-20 Snecma Labyrinth seal for fixed blades of jet engine compressor - has abradable resin surface in contact with ridges of rotor seal
JPS5550393U (en) * 1978-09-29 1980-04-02
FR2452590A1 (en) * 1979-03-27 1980-10-24 Snecma REMOVABLE SEAL FOR TURBOMACHINE DISPENSER SEGMENT

Also Published As

Publication number Publication date
SE458295B (en) 1989-03-13
FR2519096A1 (en) 1983-07-01
DE3244874A1 (en) 1983-07-07
SE8207315D0 (en) 1982-12-21
DE3244874C2 (en) 1991-03-07
GB2112878A (en) 1983-07-27
IT1195967B (en) 1988-11-03
JPH0319398B2 (en) 1991-03-14
JPS58119996A (en) 1983-07-16
GB2112878B (en) 1985-12-04
SE8207315L (en) 1983-06-29
FR2519096B1 (en) 1988-07-15

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