AU218618B2 - Improvements in or relating to axial flow compressors - Google Patents

Improvements in or relating to axial flow compressors

Info

Publication number
AU218618B2
AU218618B2 AU23907/56A AU2390756A AU218618B2 AU 218618 B2 AU218618 B2 AU 218618B2 AU 23907/56 A AU23907/56 A AU 23907/56A AU 2390756 A AU2390756 A AU 2390756A AU 218618 B2 AU218618 B2 AU 218618B2
Authority
AU
Australia
Prior art keywords
relating
axial flow
flow compressors
compressors
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
AU23907/56A
Other versions
AU2390756A (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 AU2390756A publication Critical patent/AU2390756A/en
Publication of AU218618B2 publication Critical patent/AU218618B2/en
Expired legal-status Critical Current

Links

AU23907/56A 1956-12-12 Improvements in or relating to axial flow compressors Expired AU218618B2 (en)

Publications (2)

Publication Number Publication Date
AU2390756A AU2390756A (en) 1957-06-13
AU218618B2 true AU218618B2 (en) 1957-06-13

Family

ID=

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