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AU160496B2 - Improvements in or relating to rotors for axial flow compressors or turbines - Google Patents

Improvements in or relating to rotors for axial flow compressors or turbines

Info

Publication number
AU160496B2
AU160496B2 AU9360/52A AU936052A AU160496B2 AU 160496 B2 AU160496 B2 AU 160496B2 AU 9360/52 A AU9360/52 A AU 9360/52A AU 936052 A AU936052 A AU 936052A AU 160496 B2 AU160496 B2 AU 160496B2
Authority
AU
Australia
Prior art keywords
rotors
turbines
relating
axial flow
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
AU9360/52A
Other versions
AU936052A (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.)
Bristol Aeroplane Co Ltd
Original Assignee
Bristol Aeroplane Co Ltd
Filing date
Publication date
Application filed by Bristol Aeroplane Co Ltd filed Critical Bristol Aeroplane Co Ltd
Application granted granted Critical
Publication of AU936052A publication Critical patent/AU936052A/en
Publication of AU160496B2 publication Critical patent/AU160496B2/en
Expired legal-status Critical Current

Links

AU9360/52A 1952-04-17 Improvements in or relating to rotors for axial flow compressors or turbines Expired AU160496B2 (en)

Publications (2)

Publication Number Publication Date
AU936052A AU936052A (en) 1952-06-19
AU160496B2 true AU160496B2 (en) 1952-06-19

Family

ID=

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