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FR1157855A - Axial flow turbine or compressor - Google Patents

Axial flow turbine or compressor

Info

Publication number
FR1157855A
FR1157855A FR1157855DA FR1157855A FR 1157855 A FR1157855 A FR 1157855A FR 1157855D A FR1157855D A FR 1157855DA FR 1157855 A FR1157855 A FR 1157855A
Authority
FR
France
Prior art keywords
compressor
axial flow
flow turbine
turbine
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
French (fr)
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
General Motors 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 General Motors Corp filed Critical General Motors Corp
Application granted granted Critical
Publication of FR1157855A publication Critical patent/FR1157855A/en
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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Chemically Coating (AREA)
FR1157855D 1955-08-17 1956-08-17 Axial flow turbine or compressor Expired FR1157855A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US345353XA 1955-08-17 1955-08-17

Publications (1)

Publication Number Publication Date
FR1157855A true FR1157855A (en) 1958-06-04

Family

ID=21877015

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1157855D Expired FR1157855A (en) 1955-08-17 1956-08-17 Axial flow turbine or compressor

Country Status (3)

Country Link
CH (1) CH345353A (en)
FR (1) FR1157855A (en)
GB (1) GB794947A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1169958B (en) * 1961-06-13 1964-05-14 Gasturbinenbau Und Energiemasc Sealing ring for the radial gap between a rotor blade ring and the housing of a hot steam or hot gas turbine

Also Published As

Publication number Publication date
CH345353A (en) 1960-03-31
GB794947A (en) 1958-05-14

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