FR1150778A - Compresseur axial - Google Patents

Compresseur axial

Info

Publication number
FR1150778A
FR1150778A FR1150778DA FR1150778A FR 1150778 A FR1150778 A FR 1150778A FR 1150778D A FR1150778D A FR 1150778DA FR 1150778 A FR1150778 A FR 1150778A
Authority
FR
France
Prior art keywords
axial compressor
compressor
axial
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
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 FR1150778A publication Critical patent/FR1150778A/fr
Expired legal-status Critical Current

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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Paints Or Removers (AREA)
  • Compositions Of Macromolecular Compounds (AREA)
FR1150778D 1956-03-26 1956-04-11 Compresseur axial Expired FR1150778A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB931856A GB791568A (en) 1956-03-26 1956-03-26 Improvements in axial flow compressors

Publications (1)

Publication Number Publication Date
FR1150778A true FR1150778A (fr) 1958-01-17

Family

ID=9869665

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1150778D Expired FR1150778A (fr) 1956-03-26 1956-04-11 Compresseur axial

Country Status (3)

Country Link
CH (1) CH344168A (fr)
FR (1) FR1150778A (fr)
GB (1) GB791568A (fr)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB851267A (en) * 1958-04-28 1960-10-12 Gen Motors Corp Improvements relating to axial-flow compressors
US3083529A (en) * 1959-03-24 1963-04-02 Charles W F Hemilton Hydraulic jet propulsion apparatus for water-borne craft
US3039737A (en) * 1959-04-13 1962-06-19 Int Harvester Co Device for controlling clearance between rotor and shroud of a turbine
US3053694A (en) * 1961-02-20 1962-09-11 Gen Electric Abradable material
US3173605A (en) * 1963-06-21 1965-03-16 Rotron Mfg Co Fan housing
GB2112878B (en) * 1981-12-28 1985-12-04 United Technologies Corp Air seal for compressor stator
DE3316535A1 (de) * 1983-05-06 1984-11-08 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Turboverdichter mit einlaufbelag
CA2166852A1 (fr) * 1995-01-17 1996-07-18 Donnie Ray Juen Compositions d'organosiloxane donnant des elastomeres usinables resistant a l'erosion
GB0705696D0 (en) * 2007-03-24 2007-05-02 Rolls Royce Plc A method of repairing a damaged abradable coating
EP2202264B1 (fr) * 2008-12-24 2018-04-18 Safran Aero Boosters SA Procédé de fabrication par moulage d'un élément structurel de machine avec une surface abradable
GB2496887A (en) * 2011-11-25 2013-05-29 Rolls Royce Plc Gas turbine engine abradable liner

Also Published As

Publication number Publication date
GB791568A (en) 1958-03-05
CH344168A (de) 1960-01-31

Similar Documents

Publication Publication Date Title
FR1150778A (fr) Compresseur axial
FR1177716A (fr) Projectile empenné
CH362270A (de) Axialkompressor
FR1192696A (fr) Turbomachine axiale
CH350066A (de) Axialkompressor
CH340943A (de) Turbokompressor
FR1180760A (fr) Projectile empenné
FR1199567A (fr) Compresseur axial
FR1140265A (fr) Compresseur portatif
CH326478A (fr) Wassingue
FR1192360A (fr) Stator de compresseur du type axial
FR1191087A (fr) Compresseur
CH341939A (de) Turboverdichter
FR1153272A (fr) Compresseur
FR1183889A (fr) Compresseur axial poly-étagé
AT194419B (de) Kühltruhe
FR1192161A (fr) Compresseurs rotatifs
FR70939E (fr) Compresseur axial
CH356301A (de) Heuwerbemaschine
AT194047B (de) Kolbenkompressor
FI28582A (fi) Nopeakäyntinen kompressori
FR1145502A (fr) Projectile
FI31157A (fi) Jäähdytysainekompressori
ES55661Y (es) Nueva Camisa-chaqueta
ES55120Y (es) Nueva llave-mordaza