CA734764A - Gas turbine nozzle vane and like articles - Google Patents

Gas turbine nozzle vane and like articles

Info

Publication number
CA734764A
CA734764A CA734764A CA734764DA CA734764A CA 734764 A CA734764 A CA 734764A CA 734764 A CA734764 A CA 734764A CA 734764D A CA734764D A CA 734764DA CA 734764 A CA734764 A CA 734764A
Authority
CA
Canada
Prior art keywords
articles
gas turbine
turbine nozzle
nozzle vane
vane
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
CA734764A
Inventor
G. Chisholm Charles
A. Fritzlen Glenn
M. Leach Edward
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.)
Union Carbide Corp
Original Assignee
Union Carbide Corp
Publication date
Application granted granted Critical
Publication of CA734764A publication Critical patent/CA734764A/en
Expired legal-status Critical Current

Links

CA734764A Gas turbine nozzle vane and like articles Expired CA734764A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA734764T

Publications (1)

Publication Number Publication Date
CA734764A true CA734764A (en) 1966-05-24

Family

ID=36132922

Family Applications (1)

Application Number Title Priority Date Filing Date
CA734764A Expired CA734764A (en) Gas turbine nozzle vane and like articles

Country Status (1)

Country Link
CA (1) CA734764A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3055352A1 (en) * 2016-08-29 2018-03-02 Safran Aircraft Engines DUST FOR TURBOMACHINE WITH A STRUCTURE REDUCING THE RISK OF CREAM APPEARANCE

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3055352A1 (en) * 2016-08-29 2018-03-02 Safran Aircraft Engines DUST FOR TURBOMACHINE WITH A STRUCTURE REDUCING THE RISK OF CREAM APPEARANCE

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