CA555925A - Blade ring assemblies for axial flow compressors or turbines - Google Patents

Blade ring assemblies for axial flow compressors or turbines

Info

Publication number
CA555925A
CA555925A CA555925A CA555925DA CA555925A CA 555925 A CA555925 A CA 555925A CA 555925 A CA555925 A CA 555925A CA 555925D A CA555925D A CA 555925DA CA 555925 A CA555925 A CA 555925A
Authority
CA
Canada
Prior art keywords
turbines
axial flow
blade ring
ring assemblies
flow compressors
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
CA555925A
Other languages
French (fr)
Inventor
B. Halford Frank
F. Clarke George
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.)
Bristol Siddeley Engines Ltd
Original Assignee
De Havilland Engine Co Ltd
Publication date
Application granted granted Critical
Publication of CA555925A publication Critical patent/CA555925A/en
Expired legal-status Critical Current

Links

CA555925A Blade ring assemblies for axial flow compressors or turbines Expired CA555925A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA555925T

Publications (1)

Publication Number Publication Date
CA555925A true CA555925A (en) 1958-04-15

Family

ID=35717344

Family Applications (1)

Application Number Title Priority Date Filing Date
CA555925A Expired CA555925A (en) Blade ring assemblies for axial flow compressors or turbines

Country Status (1)

Country Link
CA (1) CA555925A (en)

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