GB794947A - Improvements relating to turbines and compressors - Google Patents

Improvements relating to turbines and compressors

Info

Publication number
GB794947A
GB794947A GB23926/56A GB2392656A GB794947A GB 794947 A GB794947 A GB 794947A GB 23926/56 A GB23926/56 A GB 23926/56A GB 2392656 A GB2392656 A GB 2392656A GB 794947 A GB794947 A GB 794947A
Authority
GB
United Kingdom
Prior art keywords
nickel
powder
phosphide
casing
layer
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
GB23926/56A
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
Publication of GB794947A publication Critical patent/GB794947A/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)
  • Chemically Coating (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
GB23926/56A 1955-08-17 1956-08-02 Improvements relating to turbines and compressors Expired GB794947A (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
GB794947A true GB794947A (en) 1958-05-14

Family

ID=21877015

Family Applications (1)

Application Number Title Priority Date Filing Date
GB23926/56A Expired GB794947A (en) 1955-08-17 1956-08-02 Improvements relating to turbines and compressors

Country Status (3)

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

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1169958B (de) * 1961-06-13 1964-05-14 Gasturbinenbau Und Energiemasc Dichtungsring fuer den Radialspalt zwischen einem Laufschaufelkranz und dem Gehaeuseeiner Heissdampf- oder Heissgasturbine

Also Published As

Publication number Publication date
FR1157855A (fr) 1958-06-04
CH345353A (de) 1960-03-31

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