CA630112A - Rotors for multi stage axial flow compressors or turbines - Google Patents

Rotors for multi stage axial flow compressors or turbines

Info

Publication number
CA630112A
CA630112A CA630112A CA630112DA CA630112A CA 630112 A CA630112 A CA 630112A CA 630112 A CA630112 A CA 630112A CA 630112D A CA630112D A CA 630112DA CA 630112 A CA630112 A CA 630112A
Authority
CA
Canada
Prior art keywords
rotors
turbines
axial flow
multi stage
stage 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
CA630112A
Inventor
E. J. Buckingham David
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.)
Napier Turbochargers Ltd
Original Assignee
D Napier and Son Ltd
Publication date
Application granted granted Critical
Publication of CA630112A publication Critical patent/CA630112A/en
Expired legal-status Critical Current

Links

CA630112A Rotors for multi stage axial flow compressors or turbines Expired CA630112A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA630112T

Publications (1)

Publication Number Publication Date
CA630112A true CA630112A (en) 1961-10-31

Family

ID=35886249

Family Applications (1)

Application Number Title Priority Date Filing Date
CA630112A Expired CA630112A (en) Rotors for multi stage axial flow compressors or turbines

Country Status (1)

Country Link
CA (1) CA630112A (en)

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