FR1506794A - Compresseur à flux axial - Google Patents

Compresseur à flux axial

Info

Publication number
FR1506794A
FR1506794A FR88914A FR88914A FR1506794A FR 1506794 A FR1506794 A FR 1506794A FR 88914 A FR88914 A FR 88914A FR 88914 A FR88914 A FR 88914A FR 1506794 A FR1506794 A FR 1506794A
Authority
FR
France
Prior art keywords
axial flow
flow compressor
compressor
axial
flow
Prior art date
Legal status (The legal status 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 status listed.)
Expired
Application number
FR88914A
Other languages
English (en)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Motors Liquidation Co
Original Assignee
Motors Liquidation Co
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 Motors Liquidation Co filed Critical Motors Liquidation Co
Application granted granted Critical
Publication of FR1506794A publication Critical patent/FR1506794A/fr
Expired legal-status Critical Current

Links

Classifications

    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08G—MACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
    • C08G59/00—Polycondensates containing more than one epoxy group per molecule; Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups
    • C08G59/18—Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing
    • C08G59/20—Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing characterised by the epoxy compounds used
    • C08G59/22—Di-epoxy compounds
    • C08G59/226—Mixtures of di-epoxy compounds
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08G—MACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
    • C08G59/00—Polycondensates containing more than one epoxy group per molecule; Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups
    • C08G59/18—Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing
    • C08G59/20—Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing characterised by the epoxy compounds used
    • C08G59/22—Di-epoxy compounds
    • 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
    • F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
    • F01D11/122—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part with erodable or abradable material
    • 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
    • F05D2250/00—Geometry
    • F05D2250/20—Three-dimensional
    • F05D2250/29—Three-dimensional machined; miscellaneous
    • F05D2250/293—Three-dimensional machined; miscellaneous lathed, e.g. rotation symmetrical

Landscapes

  • Chemical & Material Sciences (AREA)
  • Medicinal Chemistry (AREA)
  • Health & Medical Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Engineering & Computer Science (AREA)
  • Polymers & Plastics (AREA)
  • Organic Chemistry (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Paints Or Removers (AREA)
  • Epoxy Resins (AREA)
  • Compositions Of Macromolecular Compounds (AREA)
FR88914A 1966-04-01 1966-12-27 Compresseur à flux axial Expired FR1506794A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US539383A US3346175A (en) 1966-04-01 1966-04-01 Plastic coating for compressors

Publications (1)

Publication Number Publication Date
FR1506794A true FR1506794A (fr) 1967-12-22

Family

ID=24150977

Family Applications (1)

Application Number Title Priority Date Filing Date
FR88914A Expired FR1506794A (fr) 1966-04-01 1966-12-27 Compresseur à flux axial

Country Status (4)

Country Link
US (1) US3346175A (fr)
DE (1) DE1628262A1 (fr)
FR (1) FR1506794A (fr)
GB (1) GB1102049A (fr)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3487519A (en) * 1967-08-31 1970-01-06 Hudson Eng Co Method of making axial flow fans
US3799128A (en) * 1973-03-08 1974-03-26 Gen Motors Corp Engine cooling system radiator and fan shroud
US4152094A (en) * 1975-10-31 1979-05-01 Hitachi, Ltd. Axial fan
US4257735A (en) * 1978-12-15 1981-03-24 General Electric Company Gas turbine engine seal and method for making same
GB2195920A (en) * 1986-08-29 1988-04-20 Corrocoat Limited Coating internal surfaces of pumps
US5544484A (en) * 1993-02-03 1996-08-13 Nartron Corporation Engine induction air driven alternator
US5388959A (en) * 1993-08-23 1995-02-14 General Electric Company Seal including a non-metallic abradable material
US5472315A (en) * 1993-11-09 1995-12-05 Sundstrand Corporation Abradable coating in a gas turbine engine
US6220234B1 (en) 1999-03-04 2001-04-24 Cummins Engine Company Coated compressor diffuser
GB0015207D0 (en) * 2000-06-21 2000-08-09 Neyrfor Weir Ltd A turbine
GB2397342A (en) * 2002-12-19 2004-07-21 Flakt Woods Ltd Fan duct with abradable coating surrounding blade tips
US6916529B2 (en) * 2003-01-09 2005-07-12 General Electric Company High temperature, oxidation-resistant abradable coatings containing microballoons and method for applying same
GB0400752D0 (en) 2004-01-13 2004-02-18 Rolls Royce Plc Cantilevered stator stage
ITMI20041780A1 (it) * 2004-09-17 2004-12-17 Nuovo Pignone Spa Dispositivo di protezione per uno statore di una turbina
US7712311B2 (en) * 2007-03-14 2010-05-11 Gm Global Technology Operations, Inc. Turbocharger assembly with catalyst coating
US7726286B2 (en) * 2007-05-21 2010-06-01 Gm Global Technology Operations, Inc. Housing for a supercharger assembly
EP2576999B1 (fr) * 2010-05-31 2014-09-03 Craig Rookstool Doublage de carter de compresseur
FR3037511B1 (fr) 2015-06-18 2017-06-02 Snecma Dispositif de revetement d'un carter annulaire de turbomachine
US10077782B2 (en) * 2015-09-30 2018-09-18 Siemens Aktiengesellschaft Adaptive blade tip seal assembly
US10082152B2 (en) * 2015-09-30 2018-09-25 Siemens Aktiengsellschaft Gas turbine compressor with adaptive blade tip seal assembly
FR3049978B1 (fr) * 2016-04-12 2018-04-27 Safran Aircraft Engines Aube et procede de rechargement d'une couche d'abradable

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA637191A (en) * 1962-02-27 K. Eder Virgil Abradable protective coating for compressor casings
US2962809A (en) * 1953-02-26 1960-12-06 Gen Motors Corp Method of making a compressor seal
US3010843A (en) * 1958-04-28 1961-11-28 Gen Motors Corp Abradable protective coating for compressor casings
GB852273A (en) * 1958-04-28 1960-10-26 Gen Motors Corp Improvements relating to axial-flow compressors
GB851267A (en) * 1958-04-28 1960-10-12 Gen Motors Corp Improvements relating to axial-flow compressors

Also Published As

Publication number Publication date
GB1102049A (en) 1968-02-07
US3346175A (en) 1967-10-10
DE1628262A1 (de) 1972-01-27

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